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0.857358 0.003240 + 0.871239 0.003171 + 0.885123 0.003045 + 0.899010 0.002855 + 0.912897 0.002596 + 0.926785 0.002269 + 0.940673 0.001866 + 0.954562 0.001387 + 0.968423 0.000836 + 0.982034 0.000226 + 0.994050 -0.000374 + 1.000000 -0.000680 + +The AG2x airfoils are intended to be used on composite versions of the +Bubble Dancer and the Allegro-Lite. diff --git a/airfoil/data/ag26.dat b/airfoil/data/ag26.dat new file mode 100644 index 0000000..30faf03 --- /dev/null +++ b/airfoil/data/ag26.dat @@ -0,0 +1,164 @@ +AG26 Bubble Dancer DLG by Mark Drela + 1.000000 0.000283 + 0.994061 0.000999 + 0.982066 0.002505 + 0.968526 0.004228 + 0.954693 0.006008 + 0.940816 0.007759 + 0.926936 0.009469 + 0.913054 0.011174 + 0.899169 0.012856 + 0.885285 0.014530 + 0.871402 0.016190 + 0.857523 0.017832 + 0.843640 0.019461 + 0.829761 0.021064 + 0.815882 0.022652 + 0.801998 0.024219 + 0.788119 0.025763 + 0.774238 0.027291 + 0.760352 0.028789 + 0.746468 0.030268 + 0.732578 0.031719 + 0.718685 0.033151 + 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index 0000000..61e48da --- /dev/null +++ b/airfoil/data/ag27.dat @@ -0,0 +1,165 @@ +AG27 Bubble Dancer DLG by Mark Drela + 1.000000 0.000283 + 0.994180 0.000967 + 0.982337 0.002388 + 0.968812 0.004026 + 0.955011 0.005695 + 0.941189 0.007338 + 0.927350 0.008957 + 0.913497 0.010556 + 0.899632 0.012140 + 0.885755 0.013711 + 0.871872 0.015274 + 0.857989 0.016826 + 0.844111 0.018368 + 0.830237 0.019895 + 0.816368 0.021406 + 0.802503 0.022898 + 0.788640 0.024370 + 0.774777 0.025821 + 0.760916 0.027248 + 0.747055 0.028652 + 0.733192 0.030032 + 0.719329 0.031386 + 0.705466 0.032715 + 0.691601 0.034018 + 0.677736 0.035294 + 0.663871 0.036542 + 0.650005 0.037761 + 0.636140 0.038952 + 0.622275 0.040111 + 0.608411 0.041238 + 0.594548 0.042333 + 0.580687 0.043392 + 0.566827 0.044415 + 0.552967 0.045401 + 0.539110 0.046347 + 0.525254 0.047252 + 0.511400 0.048115 + 0.497547 0.048934 + 0.483698 0.049707 + 0.469849 0.050432 + 0.456003 0.051109 + 0.442161 0.051733 + 0.428321 0.052305 + 0.414484 0.052821 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b/airfoil/data/aquilasm.dat new file mode 100644 index 0000000..7ba1657 --- /dev/null +++ b/airfoil/data/aquilasm.dat @@ -0,0 +1,70 @@ + AQUILA 9.3% smoothed + 1.00000 0.0 + 0.99667 0.00057 + 0.99333 0.00114 + 0.99000 0.00171 + 0.98667 0.00228 + 0.98000 0.00340 + 0.92667 0.01240 + 0.87333 0.02150 + 0.82000 0.03065 + 0.76000 0.04077 + 0.70667 0.04945 + 0.65333 0.05768 + 0.60000 0.06530 + 0.54667 0.07214 + 0.49333 0.07799 + 0.44000 0.08263 + 0.39333 0.08551 + 0.34667 0.08710 + 0.31333 0.08735 + 0.27333 0.08655 + 0.23333 0.08438 + 0.19333 0.08055 + 0.16000 0.07577 + 0.12667 0.06914 + 0.09333 0.06012 + 0.06000 0.04786 + 0.04667 0.04171 + 0.03333 0.03454 + 0.02667 0.03045 + 0.02000 0.02587 + 0.01333 0.02052 + 0.01000 0.01739 + 0.00667 0.01377 + 0.00333 0.00929 + 0.0 0.0 + 0.00333 -0.00572 + 0.00667 -0.00725 + 0.01000 -0.00810 + 0.01333 -0.00862 + 0.02000 -0.00917 + 0.02667 -0.00940 + 0.03333 -0.00947 + 0.04667 -0.00939 + 0.06000 -0.00920 + 0.09333 -0.00866 + 0.12667 -0.00821 + 0.16000 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b/airfoil/data/as5045.dat @@ -0,0 +1,83 @@ +AS5045 (15%) +1.0000 .00125 +.99810 .00168 +.99262 .00289 +.98385 .00461 +.97186 .00684 +.95690 .00935 +.93892 .01196 +.91780 .01477 +.89367 .01788 +.86673 .02140 +.83721 .02541 +.80536 .03000 +.77153 .03526 +.73615 .04132 +.69982 .04811 +.66317 .05543 +.62680 .06283 +.59096 .06923 +.55516 .07433 +.51913 .07831 +.48292 .08123 +.44664 .08325 +.41052 .08449 +.37479 .08499 +.33967 .08478 +.30537 .08387 +.27211 .08229 +.24008 .08005 +.20946 .07717 +.18043 .07367 +.15315 .06959 +.12777 .06496 +.10446 .05981 +.08330 .05416 +.06436 .04806 +.04778 .04161 +.03361 .03483 +.02185 .02787 +.01263 .02078 +.00593 .01366 +.00173 .00668 +.00000 .00008 +.00109 -.00530 +.00587 -.00990 +.01434 -.01476 +.02592 -.01980 +.04036 -.02496 +.05747 -.03017 +.07703 -.03536 +.09884 -.04037 +.12277 -.04507 +.14872 -.04937 +.17657 -.05321 +.20618 -.05657 +.23735 -.05943 +.26989 -.06175 +.30359 -.06349 +.33826 -.06458 +.37369 -.06501 +.40968 -.06473 +.44597 -.06373 +.48229 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b/airfoil/data/clarkysm.dat new file mode 100644 index 0000000..2c4ee50 --- /dev/null +++ b/airfoil/data/clarkysm.dat @@ -0,0 +1,70 @@ + CLARK-Y 11.7% smoothed + 1.00000 0.0 + 0.99572 0.00115 + 0.98296 0.00448 + 0.96194 0.00972 + 0.93301 0.01656 + 0.89668 0.02475 + 0.85355 0.03400 + 0.80438 0.04394 + 0.75000 0.05412 + 0.69134 0.06405 + 0.62941 0.07319 + 0.56526 0.08105 + 0.50000 0.08719 + 0.43474 0.09128 + 0.37059 0.09312 + 0.33928 0.09318 + 0.30866 0.09266 + 0.27886 0.09158 + 0.25000 0.08996 + 0.22221 0.08774 + 0.19562 0.08483 + 0.17033 0.08113 + 0.14645 0.07660 + 0.12408 0.07134 + 0.10332 0.06552 + 0.08427 0.05939 + 0.06699 0.05313 + 0.05156 0.04677 + 0.03806 0.04027 + 0.02653 0.03352 + 0.01704 0.02652 + 0.00961 0.01943 + 0.00428 0.01254 + 0.00107 0.00616 + 0.0 0.00047 + 0.00107 -0.00453 + 0.00428 -0.00898 + 0.00961 -0.01296 + 0.01704 -0.01651 + 0.02653 -0.01959 + 0.03806 -0.02214 + 0.05156 -0.02414 + 0.06699 -0.02567 + 0.08427 -0.02680 + 0.10332 -0.02763 + 0.12408 -0.02816 + 0.14645 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0.0259100 -.0265100 + 0.0511600 -.0337400 + 0.0763000 -.0376800 + 0.1013800 -.0402100 + 0.1514900 -.0431900 + 0.2015000 -.0436700 + 0.3014200 -.0411300 + 0.4012800 -.0373000 + 0.5011200 -.0325600 + 0.6009400 -.0272300 + 0.7007300 -.0212900 + 0.8005100 -.0148600 + 0.9002800 -.0080300 + 0.9501500 -.0044100 + 1.0000000 -.0008000 diff --git a/airfoil/data/clarym18.dat b/airfoil/data/clarym18.dat new file mode 100644 index 0000000..54f98d7 --- /dev/null +++ b/airfoil/data/clarym18.dat @@ -0,0 +1,38 @@ +CLARK YM-18 AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0114900 0.0294000 + 0.0234700 0.0444100 + 0.0477800 0.0644400 + 0.0723100 0.0780900 + 0.0969400 0.0890300 + 0.1463800 0.1052400 + 0.1960200 0.1158400 + 0.2957500 0.1236700 + 0.3957600 0.1233100 + 0.4960200 0.1155600 + 0.5965000 0.1016200 + 0.6971700 0.0822800 + 0.7979800 0.0586500 + 0.8989200 0.0315200 + 0.9494300 0.0166600 + 1.0000000 0.0009000 + + 0.0000000 0.0000000 + 0.0133500 -.0247400 + 0.0261400 -.0330000 + 0.0514700 -.0426300 + 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b/airfoil/data/coanda2.dat new file mode 100644 index 0000000..ebea388 --- /dev/null +++ b/airfoil/data/coanda2.dat @@ -0,0 +1,34 @@ +Coanda 2 +1.0000 0.0070 +0.9500 0.0170 +0.9000 0.0250 +0.8000 0.0390 +0.7000 0.0500 +0.6000 0.0580 +0.5000 0.0650 +0.4000 0.0700 +0.3000 0.0730 +0.2000 0.0710 +0.1500 0.0670 +0.1000 0.0600 +0.0750 0.0545 +0.0500 0.0465 +0.0250 0.0355 +0.0125 0.0270 +0.0000 0.0170 +0.0125 0.0088 +0.0250 0.0040 +0.0500 0.0000 +0.0750 0.0025 +0.1000 0.0060 +0.1500 0.0090 +0.2000 0.0112 +0.3000 0.0130 +0.4000 0.0130 +0.5000 0.0125 +0.6000 0.0115 +0.7000 0.0100 +0.8000 0.0070 +0.9000 0.0020 +0.9500 0.0000 +1.0000 0.0070 diff --git a/airfoil/data/coanda3.dat b/airfoil/data/coanda3.dat new file mode 100644 index 0000000..341edfc --- /dev/null +++ b/airfoil/data/coanda3.dat @@ -0,0 +1,34 @@ +Coanda 3 +1.0000 0.0070 +0.9500 0.0185 +0.9000 0.0280 +0.8000 0.0450 +0.7000 0.0572 +0.6000 0.0670 +0.5000 0.0740 +0.4000 0.0770 +0.3000 0.0770 +0.2000 0.0740 +0.1500 0.0695 +0.1000 0.0620 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0.0000 +0.9500 0.0000 +1.0000 0.0040 diff --git a/airfoil/data/fg2.dat b/airfoil/data/fg2.dat new file mode 100644 index 0000000..26c5e3f --- /dev/null +++ b/airfoil/data/fg2.dat @@ -0,0 +1,34 @@ +Fage & Collins 2 +1.0000 0.0050 +0.9500 0.0185 +0.9000 0.0265 +0.8000 0.0410 +0.7000 0.0530 +0.6000 0.0630 +0.5000 0.0720 +0.4000 0.0790 +0.3000 0.0816 +0.2000 0.0785 +0.1500 0.0720 +0.1000 0.0625 +0.0750 0.0560 +0.0500 0.0465 +0.0250 0.0337 +0.0125 0.0245 +0.0000 0.0083 +0.0125 0.0000 +0.0250 0.0000 +0.0500 0.0000 +0.0750 0.0000 +0.1000 0.0000 +0.1500 0.0000 +0.2000 0.0000 +0.3000 0.0000 +0.4000 0.0000 +0.5000 0.0000 +0.6000 0.0000 +0.7000 0.0000 +0.8000 0.0000 +0.9000 0.0000 +0.9500 0.0000 +1.0000 0.0050 diff --git a/airfoil/data/fg3.dat b/airfoil/data/fg3.dat new file mode 100644 index 0000000..98ba018 --- /dev/null +++ b/airfoil/data/fg3.dat @@ -0,0 +1,34 @@ +Fage & Collins 3 +1.0000 0.0065 +0.9500 0.0225 +0.9000 0.0325 +0.8000 0.0533 +0.7000 0.0705 +0.6000 0.0835 +0.5000 0.0925 +0.4000 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0.8966700 0.0036400 + 0.9330100 0.0054600 + 0.9616400 0.0049100 + 0.9829600 0.0033900 + 0.9957200 0.0011800 + 1.0000000 0.0000000 diff --git a/airfoil/data/fx05191.dat b/airfoil/data/fx05191.dat new file mode 100644 index 0000000..bd3e986 --- /dev/null +++ b/airfoil/data/fx05191.dat @@ -0,0 +1,54 @@ +WORTMANN FX 05-191 AIRFOIL + 25.0 25.0 + + 0.0000000 0.0000000 + 0.0042800 0.0131300 + 0.0170400 0.0269600 + 0.0380600 0.0414100 + 0.0669900 0.0555800 + 0.1033300 0.0702000 + 0.1464400 0.0839900 + 0.1956200 0.0964800 + 0.2500000 0.1071300 + 0.3086600 0.1151600 + 0.3705900 0.1199800 + 0.4347400 0.1209100 + 0.5000000 0.1179800 + 0.5652600 0.1117000 + 0.6294100 0.1026600 + 0.6913400 0.0912800 + 0.7500000 0.0764200 + 0.8043800 0.0597500 + 0.8535600 0.0445200 + 0.8966700 0.0316100 + 0.9330100 0.0204300 + 0.9616400 0.0124200 + 0.9829600 0.0060800 + 0.9957200 0.0019100 + 1.0000000 0.0000000 + + 0.0000000 0.0000000 + 0.0042800 -.0102700 + 0.0170400 -.0196800 + 0.0380600 -.0283700 + 0.0669900 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+WORTMANN FX 3 AIRFOIL + 24.0 24.0 + + 0.0000000 0.0000000 + 0.0170400 0.0246400 + 0.0380600 0.0391200 + 0.0669900 0.0533000 + 0.1033300 0.0674300 + 0.1464400 0.0811200 + 0.1956200 0.0939400 + 0.2500000 0.1052300 + 0.3086600 0.1146400 + 0.3705900 0.1217800 + 0.4347400 0.1264800 + 0.5000000 0.1285600 + 0.5652600 0.1277900 + 0.6294100 0.1241900 + 0.6913400 0.1174300 + 0.7500000 0.1036600 + 0.8043800 0.0789700 + 0.8535600 0.0569500 + 0.8966700 0.0394800 + 0.9330100 0.0254100 + 0.9616400 0.0149800 + 0.9829600 0.0071800 + 0.9957200 0.0020800 + 1.0000000 0.0000000 + + 0.0000000 0.0000000 + 0.0170400 -.0179300 + 0.0380600 -.0270200 + 0.0669900 -.0348000 + 0.1033300 -.0426500 + 0.1464400 -.0504500 + 0.1956200 -.0575500 + 0.2500000 -.0636000 + 0.3086600 -.0683300 + 0.3705900 -.0715000 + 0.4347400 -.0726500 + 0.5000000 -.0712100 + 0.5652600 -.0666600 + 0.6294100 -.0568200 + 0.6913400 -.0365900 + 0.7500000 -.0204200 + 0.8043800 -.0084600 + 0.8535600 0.0004900 + 0.8966700 0.0054800 + 0.9330100 0.0078600 + 0.9616400 0.0069400 + 0.9829600 0.0049500 + 0.9957200 0.0017900 + 1.0000000 0.0000000 diff --git a/airfoil/data/fx38153.dat b/airfoil/data/fx38153.dat new file mode 100644 index 0000000..1649863 --- /dev/null +++ b/airfoil/data/fx38153.dat @@ -0,0 +1,102 @@ +FX 38-153 AIRFOIL + 49. 49. + + 0.0000000 0.0000000 + 0.0010200 0.0064500 + 0.0042200 0.0134900 + 0.0096000 0.0191400 + 0.0170200 0.0263000 + 0.0265000 0.0327000 + 0.0380200 0.0397500 + 0.0515800 0.0461100 + 0.0669400 0.0526600 + 0.0842200 0.0584600 + 0.1033000 0.0642400 + 0.1240300 0.0692900 + 0.1464300 0.0742600 + 0.1703400 0.0785300 + 0.1955800 0.0826600 + 0.2222100 0.0861100 + 0.2499800 0.0893200 + 0.2789100 0.0918200 + 0.3086100 0.0940200 + 0.3393300 0.0955100 + 0.3705600 0.0967000 + 0.4024300 0.0971800 + 0.4346900 0.0973900 + 0.4673300 0.0969500 + 0.4999700 0.0961800 + 0.5327400 0.0948200 + 0.5652500 0.0931100 + 0.5975000 0.0908300 + 0.6293800 0.0882100 + 0.6607400 0.0850300 + 0.6913300 0.0814800 + 0.7211500 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/dev/null +++ b/airfoil/data/goe05k.dat @@ -0,0 +1,36 @@ +GOE 5K AIRFOIL + 16. 16. + + 0.0000000 0.0000000 + 0.0250000 0.0078100 + 0.0500000 0.0116100 + 0.0750000 0.0146200 + 0.1000000 0.0173300 + 0.1500000 0.0216400 + 0.2000000 0.0249600 + 0.3000000 0.0299900 + 0.4000000 0.0329200 + 0.5000000 0.0338500 + 0.6000000 0.0329800 + 0.7000000 0.0294100 + 0.8000000 0.0231400 + 0.9000000 0.0138700 + 0.9500000 0.0080800 + 1.0000000 0.0000000 + + 0.0000000 0.0000000 + 0.0250000 -.0034900 + 0.0500000 -.0038900 + 0.0750000 -.0041800 + 0.1000000 -.0042700 + 0.1500000 -.0045600 + 0.2000000 -.0044400 + 0.3000000 -.0040100 + 0.4000000 -.0035800 + 0.5000000 -.0031500 + 0.6000000 -.0027200 + 0.7000000 -.0022900 + 0.8000000 -.0018600 + 0.9000000 -.0014300 + 0.9500000 -.0012200 + 1.0000000 0.0000000 diff --git a/airfoil/data/goe06k.dat b/airfoil/data/goe06k.dat new file mode 100644 index 0000000..e1a1c9b --- /dev/null +++ b/airfoil/data/goe06k.dat @@ -0,0 +1,36 @@ +GOE 6K AIRFOIL + 16. 16. + + 0.0000000 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--git a/airfoil/data/goe114.dat b/airfoil/data/goe114.dat new file mode 100644 index 0000000..dd4f49c --- /dev/null +++ b/airfoil/data/goe114.dat @@ -0,0 +1,38 @@ +GOE 114 (MVA MK.1) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0122500 0.0071300 + 0.0245400 0.0130700 + 0.0491900 0.0229400 + 0.0738600 0.0323100 + 0.0986200 0.0391800 + 0.1481800 0.0516300 + 0.1978200 0.0616800 + 0.2973800 0.0741000 + 0.3972600 0.0776200 + 0.4973600 0.0747600 + 0.5976400 0.0670000 + 0.6980800 0.0543400 + 0.7986600 0.0380900 + 0.8993000 0.0199500 + 0.9496400 0.0102200 + 1.0000000 0.0000000 + + 0.0000000 0.0000000 + 0.0127100 -.0058500 + 0.0253400 -.0097100 + 0.0505800 -.0165100 + 0.0757500 -.0213300 + 0.1008700 -.0247400 + 0.1509700 -.0274700 + 0.2010000 -.0282000 + 0.3007500 -.0211800 + 0.4003800 -.0106700 + 0.5001600 -.0046400 + 0.6000200 -.0006200 + 0.6999700 0.0009100 + 0.7999500 0.0013400 + 0.8999800 0.0006700 + 0.9499900 0.0003300 + 1.0000000 0.0000000 diff --git a/airfoil/data/goe115.dat b/airfoil/data/goe115.dat new file mode 100644 index 0000000..5f783b4 --- /dev/null +++ b/airfoil/data/goe115.dat @@ -0,0 +1,38 @@ +GOE 115 (MVA MK.2) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0120800 0.0130800 + 0.0243700 0.0197800 + 0.0490400 0.0302600 + 0.0737400 0.0395500 + 0.0984900 0.0476300 + 0.1480800 0.0604100 + 0.1977800 0.0698900 + 0.2974500 0.0801600 + 0.3973500 0.0833400 + 0.4975300 0.0775200 + 0.5978900 0.0663100 + 0.6983300 0.0525100 + 0.7988600 0.0360000 + 0.8994100 0.0187000 + 0.9496900 0.0097000 + 1.0000000 0.0000000 + + 0.0000000 0.0000000 + 0.0128200 -.0101900 + 0.0254000 -.0126900 + 0.0505700 -.0178900 + 0.0756800 -.0213900 + 0.1007800 -.0244000 + 0.1508100 -.0260300 + 0.2008100 -.0254100 + 0.3005300 -.0166400 + 0.4002700 -.0085700 + 0.5001000 -.0032000 + 0.5999800 0.0006800 + 0.6999199 0.0024600 + 0.7999200 0.0026400 + 0.8999400 0.0018200 + 0.9499900 0.0004100 + 1.0000000 0.0000000 diff --git a/airfoil/data/goe116.dat b/airfoil/data/goe116.dat new file mode 100644 index 0000000..3feaa54 --- /dev/null +++ b/airfoil/data/goe116.dat @@ -0,0 +1,38 @@ +GOE 116 (MVA MK.3) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0121900 0.0117200 + 0.0245000 0.0188500 + 0.0491900 0.0307000 + 0.0739500 0.0398500 + 0.0987200 0.0484000 + 0.1484000 0.0608100 + 0.1981600 0.0700200 + 0.2978100 0.0832500 + 0.3977000 0.0873800 + 0.4978000 0.0835200 + 0.5981000 0.0721600 + 0.6985199 0.0563100 + 0.7989800 0.0386500 + 0.8994500 0.0209000 + 0.9497000 0.0114200 + 1.0000000 0.0017500 + + 0.0000000 0.0000000 + 0.0127100 -.0080700 + 0.0253500 -.0134300 + 0.0505300 -.0202700 + 0.0756300 -.0240100 + 0.1006700 -.0254500 + 0.1505600 -.0213300 + 0.2004300 -.0163200 + 0.3002600 -.0096900 + 0.4001600 -.0057600 + 0.5000600 -.0023200 + 0.6000100 -.0002900 + 0.6999800 0.0008400 + 0.7999700 0.0009800 + 0.9000000 -.0001800 + 0.9500300 -.0010700 + 1.0000000 -.0017500 diff --git a/airfoil/data/goe117.dat b/airfoil/data/goe117.dat new file mode 100644 index 0000000..609fd57 --- /dev/null +++ b/airfoil/data/goe117.dat @@ -0,0 +1,38 @@ +GOE 117 (MVA MK.4) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0122300 0.0136400 + 0.0246000 0.0201800 + 0.0494000 0.0304700 + 0.0742300 0.0393500 + 0.0990700 0.0473400 + 0.1487700 0.0626200 + 0.1985500 0.0740900 + 0.2983000 0.0866500 + 0.3982500 0.0893100 + 0.4983800 0.0826700 + 0.5986000 0.0716300 + 0.6988500 0.0583000 + 0.7992200 0.0405600 + 0.8996100 0.0214300 + 0.9497700 0.0116200 + 1.0000000 0.0000000 + + 0.0000000 0.0000000 + 0.0126900 -.0095500 + 0.0252400 -.0121100 + 0.0503000 -.0151100 + 0.0753300 -.0167200 + 0.1003500 -.0176300 + 0.1503000 -.0152500 + 0.2002400 -.0121800 + 0.3000600 -.0032200 + 0.3999600 0.0022400 + 0.4998900 0.0056000 + 0.5998800 0.0061600 + 0.6999000 0.0051200 + 0.7999200 0.0040800 + 0.8999600 0.0022400 + 0.9499700 0.0015200 + 1.0000000 0.0000000 diff --git a/airfoil/data/goe118.dat b/airfoil/data/goe118.dat new file mode 100644 index 0000000..d7f3e50 --- /dev/null +++ b/airfoil/data/goe118.dat @@ -0,0 +1,38 @@ +GOE 118 (MVA MK.7) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0124000 0.0120000 + 0.0248500 0.0191000 + 0.0497300 0.0334000 + 0.0746500 0.0441000 + 0.0995600 0.0549000 + 0.1494300 0.0706000 + 0.1993300 0.0837000 + 0.2992200 0.0972100 + 0.3992000 0.0994100 + 0.4992500 0.0931200 + 0.5993500 0.0807200 + 0.6994900 0.0639300 + 0.7996399 0.0450400 + 0.8998100 0.0241400 + 0.9498900 0.0130500 + 1.0000000 0.0010500 + + 0.0000000 0.0000000 + 0.0125200 -.0045000 + 0.0250500 -.0061000 + 0.0500700 -.0087000 + 0.0750600 -.0075000 + 0.1000400 -.0047900 + 0.1500000 0.0005100 + 0.1999600 0.0045100 + 0.2999100 0.0108100 + 0.3998800 0.0152200 + 0.4998600 0.0174200 + 0.5998600 0.0172300 + 0.6998800 0.0150300 + 0.7999200 0.0103400 + 0.8999600 0.0051400 + 0.9499800 0.0020500 + 1.0000000 -.0010500 diff --git a/airfoil/data/goe11k.dat b/airfoil/data/goe11k.dat new file mode 100644 index 0000000..7d2a1b7 --- /dev/null +++ b/airfoil/data/goe11k.dat @@ -0,0 +1,34 @@ +GOE 11K AIRFOIL + 15. 15. + + 0.0000000 0.0000000 + 0.0250000 0.0192800 + 0.0500000 0.0269500 + 0.1000000 0.0372100 + 0.1500000 0.0447700 + 0.2000000 0.0507200 + 0.3000000 0.0588300 + 0.4000000 0.0625400 + 0.5000000 0.0644500 + 0.6000000 0.0633600 + 0.7000000 0.0568700 + 0.8000000 0.0449800 + 0.9000000 0.0272900 + 0.9500000 0.0161500 + 1.0000000 0.0000000 + + 0.0000000 0.0000000 + 0.0250000 -.0129200 + 0.0500000 -.0152500 + 0.1000000 -.0160900 + 0.1500000 -.0153300 + 0.2000000 -.0145800 + 0.3000000 -.0130700 + 0.4000000 -.0115600 + 0.5000000 -.0100500 + 0.6000000 -.0085400 + 0.7000000 -.0070300 + 0.8000000 -.0055200 + 0.9000000 -.0040100 + 0.9500000 -.0032600 + 1.0000000 0.0000000 diff --git a/airfoil/data/goe121.dat b/airfoil/data/goe121.dat new file mode 100644 index 0000000..e8bb101 --- /dev/null +++ b/airfoil/data/goe121.dat @@ -0,0 +1,38 @@ +GOE 121 (MVA H.1) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0122800 0.0153700 + 0.0246700 0.0230500 + 0.0494900 0.0359000 + 0.0743700 0.0443600 + 0.0992500 0.0529100 + 0.1491100 0.0628200 + 0.1990100 0.0700300 + 0.2989300 0.0752400 + 0.3989400 0.0744600 + 0.4990100 0.0693900 + 0.5991200 0.0621100 + 0.6993000 0.0498300 + 0.7994900 0.0362500 + 0.8997200 0.0197800 + 0.9498300 0.0118900 + 1.0000000 0.0010000 + + 0.0000000 0.0000000 + 0.0126700 -.0123200 + 0.0251900 -.0142400 + 0.0502100 -.0144900 + 0.0751800 -.0125300 + 0.1001200 -.0083800 + 0.1500300 -.0022700 + 0.1999500 0.0036400 + 0.2998000 0.0139600 + 0.3997500 0.0175800 + 0.4997500 0.0179000 + 0.5997900 0.0150200 + 0.6998300 0.0120400 + 0.7998700 0.0091600 + 0.8999299 0.0051800 + 0.9499500 0.0022800 + 1.0000000 -.0010000 diff --git a/airfoil/data/goe122.dat b/airfoil/data/goe122.dat new file mode 100644 index 0000000..2e5e954 --- /dev/null +++ b/airfoil/data/goe122.dat @@ -0,0 +1,38 @@ +GOE 122 (MVA H.2) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0123800 0.0183800 + 0.0248300 0.0256600 + 0.0497600 0.0379200 + 0.0746900 0.0480800 + 0.0996400 0.0559400 + 0.1495800 0.0656600 + 0.1995300 0.0725900 + 0.2995000 0.0771300 + 0.3995300 0.0738800 + 0.4995700 0.0673200 + 0.5996300 0.0569700 + 0.6997100 0.0449100 + 0.7998000 0.0306600 + 0.8999000 0.0152000 + 0.9499500 0.0083300 + 1.0000000 0.0012500 + + 0.0000000 0.0000000 + 0.0125500 -.0076200 + 0.0250500 -.0075400 + 0.0500400 -.0067800 + 0.0750400 -.0055200 + 0.1000300 -.0042500 + 0.1500200 -.0023300 + 0.2000000 -.0003100 + 0.2999700 0.0041300 + 0.3999600 0.0059800 + 0.4999600 0.0066200 + 0.5999600 0.0055700 + 0.6999800 0.0034100 + 0.7999800 0.0015700 + 0.9000000 -.0001900 + 0.9500100 -.0009700 + 1.0000000 -.0012500 diff --git a/airfoil/data/goe123.dat b/airfoil/data/goe123.dat new file mode 100644 index 0000000..efd34f9 --- /dev/null +++ b/airfoil/data/goe123.dat @@ -0,0 +1,38 @@ +GOE 123 AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0125000 0.0181300 + 0.0250000 0.0262500 + 0.0500000 0.0395000 + 0.0750000 0.0487500 + 0.1000000 0.0570000 + 0.1500000 0.0685000 + 0.2000000 0.0760000 + 0.2500000 0.0805000 + 0.3000000 0.0830000 + 0.4000000 0.0840000 + 0.5000000 0.0800000 + 0.6000000 0.0720000 + 0.7000000 0.0590000 + 0.8000000 0.0420000 + 0.9000000 0.0220000 + 1.0000000 0.0020000 + + 0.0000000 0.0000000 + 0.0125000 -.0088700 + 0.0250000 -.0077500 + 0.0500000 -.0035000 + 0.0750000 0.0017500 + 0.1000000 0.0070000 + 0.1500000 0.0175000 + 0.2000000 0.0230000 + 0.2500000 0.0265000 + 0.3000000 0.0290000 + 0.4000000 0.0300000 + 0.5000000 0.0270000 + 0.6000000 0.0220000 + 0.7000000 0.0170000 + 0.8000000 0.0110000 + 0.9000000 0.0060000 + 1.0000000 0.0000000 diff --git a/airfoil/data/goe124.dat b/airfoil/data/goe124.dat new file mode 100644 index 0000000..c1ff0b7 --- /dev/null +++ b/airfoil/data/goe124.dat @@ -0,0 +1,38 @@ +GOE 124 (MVA H.4) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0123200 0.0210500 + 0.0247400 0.0310100 + 0.0496200 0.0450200 + 0.0745300 0.0551300 + 0.0994600 0.0629500 + 0.1493500 0.0759700 + 0.1992700 0.0855900 + 0.2992100 0.0932400 + 0.3992100 0.0929900 + 0.4992700 0.0861400 + 0.5993700 0.0737900 + 0.6995100 0.0581500 + 0.7996600 0.0404000 + 0.8998200 0.0213500 + 0.9499000 0.0118700 + 1.0000000 0.0025000 + + 0.0000000 0.0000000 + 0.0125900 -.0108900 + 0.0250900 -.0107900 + 0.0500600 -.0072700 + 0.0750400 -.0046600 + 0.1000200 -.0021500 + 0.1499800 0.0023700 + 0.1999400 0.0072000 + 0.2998800 0.0140500 + 0.3998500 0.0182000 + 0.4998300 0.0196500 + 0.5998500 0.0172000 + 0.6998800 0.0141500 + 0.7999099 0.0101000 + 0.8999600 0.0048500 + 0.9499800 0.0019700 + 1.0000000 -.0025000 diff --git a/airfoil/data/goe12k.dat b/airfoil/data/goe12k.dat new file mode 100644 index 0000000..a2a059d --- /dev/null +++ b/airfoil/data/goe12k.dat @@ -0,0 +1,34 @@ +GOE 12K AIRFOIL + 15. 15. + + 0.0000000 0.0000000 + 0.0250000 0.0287600 + 0.0500000 0.0402200 + 0.1000000 0.0554400 + 0.1500000 0.0667600 + 0.2000000 0.0755800 + 0.3000000 0.0876200 + 0.4000000 0.0930600 + 0.5000000 0.0960000 + 0.6000000 0.0944400 + 0.7000000 0.0846800 + 0.8000000 0.0670200 + 0.9000000 0.0395600 + 0.9500000 0.0239800 + 1.0000000 0.0000000 + + 0.0000000 0.0000000 + 0.0250000 -.0192400 + 0.0500000 -.0226800 + 0.1000000 -.0239600 + 0.1500000 -.0228400 + 0.2000000 -.0217200 + 0.3000000 -.0194800 + 0.4000000 -.0172400 + 0.5000000 -.0150000 + 0.6000000 -.0127600 + 0.7000000 -.0105200 + 0.8000000 -.0082800 + 0.9000000 -.0060400 + 0.9500000 -.0049200 + 1.0000000 0.0000000 diff --git a/airfoil/data/goe133.dat b/airfoil/data/goe133.dat new file mode 100644 index 0000000..00c9552 --- /dev/null +++ b/airfoil/data/goe133.dat @@ -0,0 +1,38 @@ +GOE 133 (MVA H.11) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0125000 0.0221100 + 0.0250000 0.0312200 + 0.0500000 0.0434500 + 0.0750000 0.0526700 + 0.1000000 0.0609000 + 0.1500000 0.0708500 + 0.2000000 0.0768000 + 0.3000000 0.0827000 + 0.4000000 0.0803000 + 0.5000000 0.0735000 + 0.6000000 0.0644000 + 0.7000000 0.0523000 + 0.8000000 0.0382000 + 0.9000000 0.0211000 + 0.9500000 0.0115500 + 1.0000000 0.0020000 + + 0.0000000 0.0000000 + 0.0125000 -.0068900 + 0.0250000 -.0087700 + 0.0500000 -.0081500 + 0.0750000 -.0068300 + 0.1000000 -.0051000 + 0.1500000 -.0016500 + 0.2000000 0.0008000 + 0.3000000 0.0037000 + 0.4000000 0.0051000 + 0.5000000 0.0060000 + 0.6000000 0.0064000 + 0.7000000 0.0063000 + 0.8000000 0.0052000 + 0.9000000 0.0031000 + 0.9500000 0.0015500 + 1.0000000 0.0000000 diff --git a/airfoil/data/goe134.dat b/airfoil/data/goe134.dat new file mode 100644 index 0000000..91303dc --- /dev/null +++ b/airfoil/data/goe134.dat @@ -0,0 +1,38 @@ +GOE 134 (MVA H.12) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0125000 0.0207100 + 0.0250000 0.0311200 + 0.0500000 0.0450400 + 0.0750000 0.0552700 + 0.1000000 0.0632900 + 0.1500000 0.0754300 + 0.2000000 0.0826800 + 0.3000000 0.0882700 + 0.4000000 0.0868600 + 0.5000000 0.0805500 + 0.6000000 0.0707400 + 0.7000000 0.0583300 + 0.8000000 0.0452200 + 0.9000000 0.0286100 + 0.9500000 0.0190600 + 1.0000000 0.0090000 + + 0.0000000 0.0000000 + 0.0125000 -.0087900 + 0.0250000 -.0086800 + 0.0500000 -.0084500 + 0.0750000 -.0082300 + 0.1000000 -.0080100 + 0.1500000 -.0075700 + 0.2000000 -.0071200 + 0.3000000 -.0062300 + 0.4000000 -.0053400 + 0.5000000 -.0044500 + 0.6000000 -.0035600 + 0.7000000 -.0026700 + 0.8000000 -.0017800 + 0.9000000 -.0008900 + 0.9500000 -.0004500 + 1.0000000 0.0000000 diff --git a/airfoil/data/goe137.dat b/airfoil/data/goe137.dat new file mode 100644 index 0000000..b0aa3b0 --- /dev/null +++ b/airfoil/data/goe137.dat @@ -0,0 +1,38 @@ +GOE 137 (MVA H.15) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0123200 0.0175300 + 0.0247100 0.0276600 + 0.0495600 0.0420200 + 0.0744500 0.0522900 + 0.0993600 0.0610500 + 0.1492400 0.0719700 + 0.1991500 0.0801000 + 0.2990800 0.0870600 + 0.3991100 0.0856100 + 0.4991700 0.0785700 + 0.5993000 0.0668200 + 0.6994400 0.0528800 + 0.7996000 0.0376400 + 0.8997900 0.0199900 + 0.9498900 0.0105200 + 1.0000000 0.0014500 + + 0.0000000 0.0000000 + 0.0125900 -.0089700 + 0.0251100 -.0105400 + 0.0501200 -.0110700 + 0.0751200 -.0112100 + 0.1001000 -.0099400 + 0.1500700 -.0063200 + 0.2000400 -.0033900 + 0.2999900 0.0011600 + 0.3999700 0.0028200 + 0.4999600 0.0038700 + 0.5999500 0.0038300 + 0.6999600 0.0033800 + 0.7999800 0.0019400 + 0.9000000 0.0003900 + 0.9500100 -.0007800 + 1.0000000 -.0014500 diff --git a/airfoil/data/goe13k.dat b/airfoil/data/goe13k.dat new file mode 100644 index 0000000..bc9ce39 --- /dev/null +++ b/airfoil/data/goe13k.dat @@ -0,0 +1,34 @@ +GOE 13K AIRFOIL + 15. 15. + + 0.0000000 0.0000000 + 0.0250000 0.0383500 + 0.0500000 0.0535900 + 0.1000000 0.0738900 + 0.1500000 0.0889900 + 0.2000000 0.1008800 + 0.3000000 0.1168700 + 0.4000000 0.1241600 + 0.5000000 0.1280500 + 0.6000000 0.1260400 + 0.7000000 0.1130300 + 0.8000000 0.0893200 + 0.9000000 0.0542100 + 0.9500000 0.0321100 + 1.0000000 0.0000000 + + 0.0000000 0.0000000 + 0.0250000 -.0255500 + 0.0500000 -.0301000 + 0.1000000 -.0319100 + 0.1500000 -.0304200 + 0.2000000 -.0289200 + 0.3000000 -.0259300 + 0.4000000 -.0229400 + 0.5000000 -.0199500 + 0.6000000 -.0169600 + 0.7000000 -.0139700 + 0.8000000 -.0109800 + 0.9000000 -.0079900 + 0.9500000 -.0065000 + 1.0000000 0.0000000 diff --git a/airfoil/data/goe14.dat b/airfoil/data/goe14.dat new file mode 100644 index 0000000..cbe737b --- /dev/null +++ b/airfoil/data/goe14.dat @@ -0,0 +1,38 @@ +GOE 14 AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0119700 0.0297100 + 0.0242000 0.0446300 + 0.0488400 0.0648700 + 0.0735800 0.0793100 + 0.0984000 0.0897600 + 0.1481200 0.1051400 + 0.1979700 0.1137300 + 0.2978800 0.1188200 + 0.3979700 0.1136000 + 0.4981700 0.1025900 + 0.5984300 0.0878800 + 0.6987800 0.0685700 + 0.7991700 0.0465700 + 0.8995800 0.0235600 + 0.9497899 0.0119500 + 1.0000000 0.0006500 + + 0.0000000 0.0000000 + 0.0128100 -.0172700 + 0.0253200 -.0180500 + 0.0502300 -.0131000 + 0.0750600 -.0031600 + 0.0999100 0.0050800 + 0.1497600 0.0131700 + 0.1997400 0.0163100 + 0.2996500 0.0198500 + 0.3996900 0.0183800 + 0.4997200 0.0159200 + 0.5997600 0.0137100 + 0.6998100 0.0104900 + 0.7998800 0.0067800 + 0.8999299 0.0029500 + 0.9499800 0.0010600 + 1.0000000 -.0006500 diff --git a/airfoil/data/goe140.dat b/airfoil/data/goe140.dat new file mode 100644 index 0000000..a8e65a6 --- /dev/null +++ b/airfoil/data/goe140.dat @@ -0,0 +1,38 @@ +GOE 140 (MVA H.17) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0123500 0.0176100 + 0.0247400 0.0299200 + 0.0495900 0.0469300 + 0.0744900 0.0590500 + 0.0994100 0.0682600 + 0.1492700 0.0839000 + 0.1992000 0.0924300 + 0.2991600 0.0968000 + 0.3992000 0.0923700 + 0.4992700 0.0834400 + 0.5993800 0.0711100 + 0.6995100 0.0564900 + 0.7996500 0.0398600 + 0.8998001 0.0224300 + 0.9498900 0.0129600 + 1.0000000 0.0029000 + + 0.0000000 0.0000000 + 0.0125900 -.0108900 + 0.0251000 -.0113800 + 0.0500800 -.0086600 + 0.0750300 -.0039500 + 0.1000100 -.0007300 + 0.1499600 0.0042000 + 0.1999400 0.0064400 + 0.2999200 0.0090100 + 0.3999100 0.0104800 + 0.4999100 0.0102500 + 0.5999100 0.0099200 + 0.6999300 0.0084900 + 0.7999500 0.0053600 + 0.8999800 0.0020300 + 0.9500000 -.0004300 + 1.0000000 -.0029000 diff --git a/airfoil/data/goe142.dat b/airfoil/data/goe142.dat new file mode 100644 index 0000000..e8ebbb3 --- /dev/null +++ b/airfoil/data/goe142.dat @@ -0,0 +1,104 @@ +GOE 142 (MVA H.19) AIRFOIL + 50. 50. + + 0.0000000 0.0000000 + 0.0004800 0.0026500 + 0.0009600 0.0038500 + 0.0014600 0.0047900 + 0.0019500 0.0056100 + 0.0024400 0.0063400 + 0.0029400 0.0070200 + 0.0039200 0.0082500 + 0.0049100 0.0093600 + 0.0073900 0.0118100 + 0.0098700 0.0139500 + 0.0123500 0.0158800 + 0.0148400 0.0176700 + 0.0198100 0.0209500 + 0.0247800 0.0238900 + 0.0347300 0.0290900 + 0.0496700 0.0356600 + 0.0746000 0.0443300 + 0.0995400 0.0508900 + 0.1244900 0.0559000 + 0.1494500 0.0597700 + 0.1744300 0.0627300 + 0.1994100 0.0649600 + 0.2243900 0.0666000 + 0.2493800 0.0677400 + 0.2743800 0.0684400 + 0.2993700 0.0687600 + 0.3493700 0.0684600 + 0.3993900 0.0670900 + 0.4494100 0.0648400 + 0.4994400 0.0618300 + 0.5494700 0.0581400 + 0.5995100 0.0538300 + 0.6495500 0.0489500 + 0.6745800 0.0463000 + 0.6996000 0.0435200 + 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+ 0.0000000 0.0000000 + 0.0126500 -.0113400 + 0.0251800 -.0140700 + 0.0501700 -.0131500 + 0.0751400 -.0111300 + 0.1001100 -.0085000 + 0.1500700 -.0055600 + 0.2000400 -.0032100 + 0.2999900 0.0009800 + 0.3999500 0.0034800 + 0.4999400 0.0047700 + 0.5999300 0.0054700 + 0.6999400 0.0044600 + 0.7999600 0.0034600 + 0.8999800 0.0017500 + 0.9500000 -.0001000 + 1.0000000 -.0014500 diff --git a/airfoil/data/goe144.dat b/airfoil/data/goe144.dat new file mode 100644 index 0000000..b26461b --- /dev/null +++ b/airfoil/data/goe144.dat @@ -0,0 +1,38 @@ +GOE 144 (MVA H.21) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0122600 0.0157800 + 0.0246300 0.0249700 + 0.0494000 0.0397400 + 0.0742600 0.0491100 + 0.0991500 0.0564900 + 0.1489800 0.0680300 + 0.1988800 0.0748800 + 0.2987800 0.0813800 + 0.3988000 0.0799800 + 0.4989000 0.0732800 + 0.5990500 0.0635900 + 0.6992199 0.0519900 + 0.7994200 0.0387900 + 0.8996900 0.0208000 + 0.9498200 0.0117500 + 1.0000000 0.0000000 + + 0.0000000 0.0000000 + 0.0126400 -.0092100 + 0.0251800 -.0118200 + 0.0502100 -.0142500 + 0.0751900 -.0128700 + 0.1001700 -.0113000 + 0.1500700 -.0043500 + 0.1999700 0.0019000 + 0.2998200 0.0118000 + 0.3997800 0.0144000 + 0.4997800 0.0148000 + 0.5998000 0.0139500 + 0.6998200 0.0122000 + 0.7998800 0.0080000 + 0.8999400 0.0041000 + 0.9499700 0.0020500 + 1.0000000 0.0000000 diff --git a/airfoil/data/goe147.dat b/airfoil/data/goe147.dat new file mode 100644 index 0000000..19d1444 --- /dev/null +++ b/airfoil/data/goe147.dat @@ -0,0 +1,38 @@ +GOE 147 (MVA H.6) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0122200 0.0181900 + 0.0245800 0.0271800 + 0.0493700 0.0412600 + 0.0742000 0.0520400 + 0.0991000 0.0584200 + 0.1489800 0.0666900 + 0.1989200 0.0703500 + 0.2989100 0.0707900 + 0.3989700 0.0668200 + 0.4991100 0.0581600 + 0.5992600 0.0480000 + 0.6994300 0.0370400 + 0.7996100 0.0253700 + 0.8997900 0.0138100 + 0.9498800 0.0079800 + 1.0000000 0.0016500 + + 0.0000000 0.0000000 + 0.0126100 -.0078800 + 0.0251700 -.0111100 + 0.0502300 -.0151300 + 0.0752400 -.0158500 + 0.1002000 -.0132600 + 0.1501300 -.0087000 + 0.2000500 -.0029300 + 0.2999300 0.0044000 + 0.3999200 0.0072400 + 0.4999000 0.0067700 + 0.5999200 0.0053100 + 0.6999400 0.0036400 + 0.7999700 0.0018800 + 0.8999800 0.0007000 + 0.9499900 -.0003400 + 1.0000000 -.0016500 diff --git a/airfoil/data/goe14k.dat b/airfoil/data/goe14k.dat new file mode 100644 index 0000000..08c6ef9 --- /dev/null +++ b/airfoil/data/goe14k.dat @@ -0,0 +1,34 @@ +GOE 14K AIRFOIL + 15. 15. + + 0.0000000 0.0000000 + 0.0250000 0.0237500 + 0.0500000 0.0340000 + 0.1000000 0.0480000 + 0.1500000 0.0581000 + 0.2000000 0.0661000 + 0.3000000 0.0776000 + 0.4000000 0.0838000 + 0.5000000 0.0870000 + 0.6000000 0.0850000 + 0.7000000 0.0776000 + 0.8000000 0.0612000 + 0.9000000 0.0380000 + 0.9500000 0.0226000 + 1.0000000 0.0000000 + + 0.0000000 0.0000000 + 0.0250000 -.0176500 + 0.0500000 -.0233000 + 0.1000000 -.0300000 + 0.1500000 -.0336000 + 0.2000000 -.0353000 + 0.3000000 -.0358000 + 0.4000000 -.0344000 + 0.5000000 -.0330000 + 0.6000000 -.0316000 + 0.7000000 -.0296000 + 0.8000000 -.0262000 + 0.9000000 -.0195000 + 0.9500000 -.0134000 + 1.0000000 0.0000000 diff --git a/airfoil/data/goe15.dat b/airfoil/data/goe15.dat new file mode 100644 index 0000000..3f1c0d7 --- /dev/null +++ b/airfoil/data/goe15.dat @@ -0,0 +1,38 @@ +GOE 15 AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0120800 0.0273800 + 0.0243600 0.0417700 + 0.0490500 0.0621500 + 0.0738200 0.0768300 + 0.0986500 0.0882100 + 0.1484100 0.1039700 + 0.1982500 0.1144300 + 0.2981200 0.1225600 + 0.3982000 0.1182900 + 0.4983300 0.1090200 + 0.5985600 0.0938600 + 0.6988800 0.0733900 + 0.7992100 0.0519300 + 0.8995900 0.0269600 + 0.9497800 0.0142300 + 1.0000000 0.0000000 + + 0.0000000 0.0000000 + 0.0127100 -.0136100 + 0.0252300 -.0149100 + 0.0500800 -.0050300 + 0.0749300 0.0048500 + 0.0998100 0.0127300 + 0.1496500 0.0229900 + 0.1995800 0.0277500 + 0.2995000 0.0325800 + 0.3995300 0.0308100 + 0.4995800 0.0273400 + 0.5996900 0.0205800 + 0.6998100 0.0121100 + 0.7999000 0.0062400 + 0.8999800 0.0014700 + 0.9499900 0.0005300 + 1.0000000 0.0000000 diff --git a/airfoil/data/goe155.dat b/airfoil/data/goe155.dat new file mode 100644 index 0000000..f46f11a --- /dev/null +++ b/airfoil/data/goe155.dat @@ -0,0 +1,38 @@ +GOE 155 (SSW D.1) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0123900 0.0171800 + 0.0248400 0.0250600 + 0.0497600 0.0384100 + 0.0746900 0.0490700 + 0.0996300 0.0586300 + 0.1495400 0.0722400 + 0.1995000 0.0796600 + 0.2994500 0.0869900 + 0.3994600 0.0865200 + 0.4994900 0.0815500 + 0.5995500 0.0714800 + 0.6996500 0.0563100 + 0.7997600 0.0387400 + 0.8998800 0.0192700 + 0.9499400 0.0095800 + 1.0000000 0.0020000 + + 0.0000000 0.0000000 + 0.0125500 -.0082200 + 0.0250500 -.0075400 + 0.0500400 -.0057800 + 0.0750100 -.0023300 + 0.1000000 0.0000300 + 0.1499600 0.0064400 + 0.1999300 0.0117600 + 0.2998900 0.0167900 + 0.3998800 0.0191200 + 0.4998800 0.0191500 + 0.5998900 0.0175800 + 0.6999199 0.0127100 + 0.7999500 0.0078400 + 0.9000000 0.0001700 + 0.9500100 -.0012100 + 1.0000000 -.0020000 diff --git a/airfoil/data/goe15k.dat b/airfoil/data/goe15k.dat new file mode 100644 index 0000000..4e5e50d --- /dev/null +++ b/airfoil/data/goe15k.dat @@ -0,0 +1,34 @@ +GOE 15K AIRFOIL + 15. 15. + + 0.0000000 0.0000000 + 0.0250000 0.0296400 + 0.0500000 0.0424700 + 0.1000000 0.0600500 + 0.1500000 0.0726200 + 0.2000000 0.0826000 + 0.3000000 0.0969500 + 0.4000000 0.1047000 + 0.5000000 0.1087500 + 0.6000000 0.1063000 + 0.7000000 0.0969500 + 0.8000000 0.0765000 + 0.9000000 0.0474500 + 0.9500000 0.0282200 + 1.0000000 0.0000000 + + 0.0000000 0.0000000 + 0.0250000 -.0221600 + 0.0500000 -.0291200 + 0.1000000 -.0374500 + 0.1500000 -.0419800 + 0.2000000 -.0441000 + 0.3000000 -.0447500 + 0.4000000 -.0430000 + 0.5000000 -.0412500 + 0.6000000 -.0395000 + 0.7000000 -.0370500 + 0.8000000 -.0327000 + 0.9000000 -.0243500 + 0.9500000 -.0167800 + 1.0000000 0.0000000 diff --git a/airfoil/data/goe164.dat b/airfoil/data/goe164.dat new file mode 100644 index 0000000..51a8d1b --- /dev/null +++ b/airfoil/data/goe164.dat @@ -0,0 +1,38 @@ +GOE 164 (MVA MK.10) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0122700 0.0222300 + 0.0246500 0.0333600 + 0.0494700 0.0502200 + 0.0743500 0.0615800 + 0.0992300 0.0729500 + 0.1490900 0.0861700 + 0.1989900 0.0955000 + 0.2989200 0.1020500 + 0.3989300 0.1015100 + 0.4990000 0.0947600 + 0.5991200 0.0837200 + 0.6992800 0.0686800 + 0.7994600 0.0515300 + 0.8996700 0.0315900 + 0.9498100 0.0177200 + 1.0000000 0.0005500 + + 0.0000000 0.0000000 + 0.0125700 -.0065700 + 0.0250900 -.0086400 + 0.0501100 -.0099700 + 0.0751100 -.0103100 + 0.1000900 -.0089400 + 0.1500200 -.0020200 + 0.1999300 0.0070100 + 0.2999700 0.0211700 + 0.3996700 0.0313200 + 0.4996400 0.0339700 + 0.5996500 0.0336300 + 0.6997000 0.0288800 + 0.7997900 0.0194400 + 0.8999000 0.0094900 + 0.9499500 0.0050200 + 1.0000000 -.0005500 diff --git a/airfoil/data/goe165.dat b/airfoil/data/goe165.dat new file mode 100644 index 0000000..779269f --- /dev/null +++ b/airfoil/data/goe165.dat @@ -0,0 +1,38 @@ +GOE 165 (MVA MK.11) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0119500 0.0194400 + 0.0240800 0.0324800 + 0.0486500 0.0476800 + 0.0732100 0.0628800 + 0.0979300 0.0728800 + 0.1475000 0.0881900 + 0.1972300 0.0977000 + 0.2970800 0.1029400 + 0.3971300 0.1010800 + 0.4973000 0.0952200 + 0.5976600 0.0824700 + 0.6980700 0.0678300 + 0.7985300 0.0516800 + 0.8991100 0.0313300 + 0.9494600 0.0188600 + 1.0000000 0.0006000 + + 0.0000000 0.0000000 + 0.0126900 -.0066400 + 0.0253100 -.0108800 + 0.0504200 -.0148700 + 0.0755500 -.0193500 + 0.1006000 -.0209400 + 0.1506900 -.0241200 + 0.2006600 -.0233000 + 0.3004200 -.0146700 + 0.3999100 0.0032600 + 0.4994300 0.0199800 + 0.5992200 0.0274200 + 0.6992400 0.0267600 + 0.7993900 0.0215000 + 0.8996400 0.0127500 + 0.9498300 0.0060800 + 1.0000000 -.0006000 diff --git a/airfoil/data/goe167.dat b/airfoil/data/goe167.dat new file mode 100644 index 0000000..cf5a67f --- /dev/null +++ b/airfoil/data/goe167.dat @@ -0,0 +1,38 @@ +GOE 167 (V.KARMAN PROP.2) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0123600 0.0182000 + 0.0247800 0.0283900 + 0.0496800 0.0412800 + 0.0746000 0.0521700 + 0.0995200 0.0620700 + 0.1494100 0.0766500 + 0.1993400 0.0853300 + 0.2992600 0.0958000 + 0.3992700 0.0944700 + 0.4993500 0.0838500 + 0.5994600 0.0704200 + 0.6995700 0.0553900 + 0.7997000 0.0391600 + 0.8998300 0.0223300 + 0.9499000 0.0130100 + 1.0000000 0.0045000 + + 0.0000000 0.0000000 + 0.0125800 -.0110000 + 0.0250900 -.0120100 + 0.0500900 -.0113100 + 0.0750800 -.0103200 + 0.1000700 -.0087300 + 0.1500600 -.0073400 + 0.2000500 -.0063600 + 0.3000400 -.0050900 + 0.4000300 -.0038200 + 0.5000200 -.0030500 + 0.6000200 -.0027800 + 0.7000200 -.0025100 + 0.8000200 -.0023400 + 0.9000200 -.0025700 + 0.9500300 -.0039800 + 1.0000000 -.0045000 diff --git a/airfoil/data/goe16k.dat b/airfoil/data/goe16k.dat new file mode 100644 index 0000000..5c8f938 --- /dev/null +++ b/airfoil/data/goe16k.dat @@ -0,0 +1,34 @@ +GOE 16K AIRFOIL + 15. 15. + + 0.0000000 0.0000000 + 0.0250000 0.0359200 + 0.0500000 0.0515500 + 0.1000000 0.0727000 + 0.1500000 0.0879500 + 0.2000000 0.1001000 + 0.3000000 0.1174000 + 0.4000000 0.1268000 + 0.5000000 0.1316000 + 0.6000000 0.1286000 + 0.7000000 0.1173000 + 0.8000000 0.0925000 + 0.9000000 0.0574000 + 0.9500000 0.0341500 + 1.0000000 0.0000000 + + 0.0000000 0.0000000 + 0.0250000 -.0266800 + 0.0500000 -.0352500 + 0.1000000 -.0452000 + 0.1500000 -.0507500 + 0.2000000 -.0533000 + 0.3000000 -.0541000 + 0.4000000 -.0520000 + 0.5000000 -.0499000 + 0.6000000 -.0478000 + 0.7000000 -.0448000 + 0.8000000 -.0396000 + 0.9000000 -.0295000 + 0.9500000 -.0203500 + 1.0000000 0.0000000 diff --git a/airfoil/data/goe173.dat b/airfoil/data/goe173.dat new file mode 100644 index 0000000..47dce1b --- /dev/null +++ b/airfoil/data/goe173.dat @@ -0,0 +1,38 @@ +GOE 173 (ALBATROS 6020) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0124100 0.0195600 + 0.0248600 0.0311100 + 0.0497800 0.0472300 + 0.0747300 0.0593400 + 0.0996800 0.0689600 + 0.1496200 0.0836900 + 0.1995800 0.0915200 + 0.2995600 0.0964800 + 0.3995600 0.0953400 + 0.4996000 0.0878000 + 0.5996500 0.0755600 + 0.6997200 0.0599200 + 0.7998000 0.0429800 + 0.8998900 0.0248400 + 0.9499400 0.0139700 + 1.0000000 0.0009000 + + 0.0000000 0.0000000 + 0.0125300 -.0054400 + 0.0250200 -.0043800 + 0.0500100 -.0019700 + 0.0750000 0.0008400 + 0.0999800 0.0036600 + 0.1499600 0.0091900 + 0.1999400 0.0139200 + 0.2999100 0.0198800 + 0.3998900 0.0228400 + 0.4998900 0.0230000 + 0.5999100 0.0205600 + 0.6999199 0.0167200 + 0.7999500 0.0115800 + 0.8999700 0.0056400 + 0.9499900 0.0028700 + 1.0000000 -.0009000 diff --git a/airfoil/data/goe174.dat b/airfoil/data/goe174.dat new file mode 100644 index 0000000..d81dc27 --- /dev/null +++ b/airfoil/data/goe174.dat @@ -0,0 +1,38 @@ +GOE 174 (ALBATROS 5020) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0123600 0.0212800 + 0.0247900 0.0317700 + 0.0496900 0.0465400 + 0.0746000 0.0599000 + 0.0995300 0.0689700 + 0.1494400 0.0828100 + 0.1993800 0.0913500 + 0.2993500 0.0967200 + 0.3993600 0.0945000 + 0.4994200 0.0863700 + 0.5995000 0.0737500 + 0.6995900 0.0600200 + 0.7997100 0.0425000 + 0.8998400 0.0243700 + 0.9499000 0.0147100 + 1.0000000 0.0014500 + + 0.0000000 0.0000000 + 0.0125500 -.0081200 + 0.0250500 -.0080300 + 0.0500500 -.0072600 + 0.0750400 -.0058900 + 0.1000200 -.0041200 + 0.1500000 -.0000900 + 0.1999600 0.0055500 + 0.2999100 0.0126200 + 0.3998900 0.0169000 + 0.4998800 0.0175700 + 0.5999000 0.0152500 + 0.6999199 0.0124200 + 0.7999400 0.0090000 + 0.8999700 0.0037700 + 0.9499900 0.0008100 + 1.0000000 -.0014500 diff --git a/airfoil/data/goe176.dat b/airfoil/data/goe176.dat new file mode 100644 index 0000000..1549c69 --- /dev/null +++ b/airfoil/data/goe176.dat @@ -0,0 +1,38 @@ +GOE 176 (ALBATROS 7020) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0121400 0.0220000 + 0.0244400 0.0343900 + 0.0492100 0.0487900 + 0.0739900 0.0625900 + 0.0988400 0.0718000 + 0.1486200 0.0854000 + 0.1984700 0.0949100 + 0.2983900 0.0994200 + 0.3984100 0.0987300 + 0.4985400 0.0904500 + 0.5987300 0.0783700 + 0.6989800 0.0630900 + 0.7992700 0.0452100 + 0.8995700 0.0264300 + 0.9497400 0.0161400 + 1.0000000 0.0011500 + + 0.0000000 0.0000000 + 0.0126200 -.0072000 + 0.0251600 -.0098900 + 0.0501900 -.0132900 + 0.0752300 -.0153900 + 0.1002500 -.0156800 + 0.1502200 -.0136700 + 0.2001300 -.0082700 + 0.2999400 0.0038400 + 0.3998000 0.0124600 + 0.4997100 0.0178700 + 0.5997100 0.0180900 + 0.6924500 0.0158200 + 0.7998000 0.0125200 + 0.8998900 0.0065300 + 0.9499500 0.0032400 + 1.0000000 -.0011500 diff --git a/airfoil/data/goe177.dat b/airfoil/data/goe177.dat new file mode 100644 index 0000000..3df4247 --- /dev/null +++ b/airfoil/data/goe177.dat @@ -0,0 +1,38 @@ +GOE 177 AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0125000 0.0151100 + 0.0250000 0.0267200 + 0.0500000 0.0394500 + 0.0750000 0.0516800 + 0.1000000 0.0599000 + 0.1500000 0.0733500 + 0.2000000 0.0818000 + 0.3000000 0.0867000 + 0.4000000 0.0836000 + 0.5000000 0.0755000 + 0.6000000 0.0644000 + 0.7000000 0.0513000 + 0.8000000 0.0372000 + 0.9000000 0.0211000 + 0.9500000 0.0115500 + 1.0000000 0.0020000 + + 0.0000000 0.0000000 + 0.0125000 -.0058900 + 0.0250000 -.0077700 + 0.0500000 -.0085500 + 0.0750000 -.0063200 + 0.1000000 -.0041000 + 0.1500000 0.0003500 + 0.2000000 0.0048000 + 0.3000000 0.0127000 + 0.4000000 0.0176000 + 0.5000000 0.0175000 + 0.6000000 0.0154000 + 0.7000000 0.0123000 + 0.8000000 0.0082000 + 0.9000000 0.0041000 + 0.9500000 0.0025500 + 1.0000000 0.0000000 diff --git a/airfoil/data/goe178.dat b/airfoil/data/goe178.dat new file mode 100644 index 0000000..874950e --- /dev/null +++ b/airfoil/data/goe178.dat @@ -0,0 +1,38 @@ +GOE 178 AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0125000 0.0161900 + 0.0250000 0.0253700 + 0.0500000 0.0377500 + 0.0750000 0.0491200 + 0.1000000 0.0585000 + 0.1500000 0.0722500 + 0.2000000 0.0800000 + 0.3000000 0.0865000 + 0.4000000 0.0820000 + 0.5000000 0.0735000 + 0.6000000 0.0630000 + 0.7000000 0.0505000 + 0.8000000 0.0360000 + 0.9000000 0.0205000 + 0.9500000 0.0112500 + 1.0000000 0.0030000 + + 0.0000000 0.0000000 + 0.0125000 -.0108100 + 0.0250000 -.0126300 + 0.0500000 -.0142500 + 0.0750000 -.0128800 + 0.1000000 -.0110000 + 0.1500000 -.0077500 + 0.2000000 -.0040000 + 0.3000000 0.0015000 + 0.4000000 0.0060000 + 0.5000000 0.0085000 + 0.6000000 0.0090000 + 0.7000000 0.0085000 + 0.8000000 0.0070000 + 0.9000000 0.0045000 + 0.9500000 0.0022500 + 1.0000000 0.0000000 diff --git a/airfoil/data/goe180.dat b/airfoil/data/goe180.dat new file mode 100644 index 0000000..e75acd6 --- /dev/null +++ b/airfoil/data/goe180.dat @@ -0,0 +1,38 @@ +GOE 180 (MVA H.26) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0125000 0.0199600 + 0.0250000 0.0293200 + 0.0500000 0.0436500 + 0.0750000 0.0544800 + 0.1000000 0.0620000 + 0.1500000 0.0734500 + 0.2000000 0.0801000 + 0.3000000 0.0874000 + 0.4000000 0.0852000 + 0.5000000 0.0778000 + 0.6000000 0.0681000 + 0.7000000 0.0561000 + 0.8000000 0.0412000 + 0.9000000 0.0237000 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0.0007500 + + 0.0000000 0.0000000 + 0.0126600 -.0115200 + 0.0252000 -.0140400 + 0.0502000 -.0142800 + 0.0751800 -.0126300 + 0.1001600 -.0113700 + 0.1500900 -.0061600 + 0.2000200 -.0010500 + 0.2998800 0.0081700 + 0.3997900 0.0146000 + 0.4997200 0.0193200 + 0.5997200 0.0196500 + 0.6997600 0.0166700 + 0.7998500 0.0108000 + 0.8999400 0.0045200 + 0.9499800 0.0013400 + 1.0000000 -.0007500 diff --git a/airfoil/data/goe184.dat b/airfoil/data/goe184.dat new file mode 100644 index 0000000..fbda585 --- /dev/null +++ b/airfoil/data/goe184.dat @@ -0,0 +1,38 @@ +GOE 184 (MVA H.29) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0122000 0.0202800 + 0.0245700 0.0294600 + 0.0493400 0.0449200 + 0.0741900 0.0553800 + 0.0990600 0.0641500 + 0.1488900 0.0760700 + 0.1987600 0.0852000 + 0.2986600 0.0916600 + 0.3986900 0.0898200 + 0.4988100 0.0814800 + 0.5989700 0.0706400 + 0.6991900 0.0555100 + 0.7994300 0.0390700 + 0.8996900 0.0209400 + 0.9498400 0.0110700 + 1.0000000 0.0011000 + + 0.0000000 0.0000000 + 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-.0006200 + 0.0500000 0.0011100 + 0.0750000 0.0021800 + 0.1000000 0.0029900 + 0.1500000 0.0042800 + 0.2000000 0.0053400 + 0.3000100 0.0069600 + 0.4000100 0.0079800 + 0.5000100 0.0079000 + 0.6000100 0.0067200 + 0.7000000 0.0055400 + 0.8000000 0.0032600 + 0.9000000 -.0007200 + 0.9500000 -.0024600 + 1.0000000 -.0025000 diff --git a/airfoil/data/goe188.dat b/airfoil/data/goe188.dat new file mode 100644 index 0000000..e6b504f --- /dev/null +++ b/airfoil/data/goe188.dat @@ -0,0 +1,38 @@ +GOE 188 (SCHTTE-LANZ 3U10) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0125000 0.0212100 + 0.0250000 0.0309300 + 0.0500000 0.0441600 + 0.0750000 0.0545800 + 0.1000000 0.0632100 + 0.1500000 0.0750600 + 0.2000000 0.0829200 + 0.3000000 0.0886300 + 0.4000000 0.0870400 + 0.5000000 0.0809500 + 0.6000000 0.0693600 + 0.7000000 0.0549700 + 0.8000000 0.0388800 + 0.9000000 0.0233900 + 0.9500000 0.0150500 + 1.0000000 0.0050000 + + 0.0000000 0.0000000 + 0.0125000 -.0010900 + 0.0250000 -.0010700 + 0.0500000 -.0010500 + 0.0750000 -.0010200 + 0.1000000 -.0009900 + 0.1500000 -.0009400 + 0.2000000 -.0008800 + 0.3000000 -.0007700 + 0.4000000 -.0006600 + 0.5000000 -.0005500 + 0.6000000 -.0004400 + 0.7000000 -.0003300 + 0.8000000 -.0002200 + 0.9000000 -.0001100 + 0.9500000 -.0000500 + 1.0000000 0.0000000 diff --git a/airfoil/data/goe190.dat b/airfoil/data/goe190.dat new file mode 100644 index 0000000..3683c7f --- /dev/null +++ b/airfoil/data/goe190.dat @@ -0,0 +1,38 @@ +GOE 190 (MVA MK.18) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0116200 0.0251100 + 0.0237200 0.0364300 + 0.0481500 0.0525900 + 0.0684900 0.0627600 + 0.0973800 0.0745300 + 0.1468800 0.0887700 + 0.1965300 0.0987200 + 0.2962100 0.1076300 + 0.3962400 0.1068500 + 0.4965400 0.0983800 + 0.5969300 0.0872100 + 0.6975000 0.0710500 + 0.7981000 0.0538900 + 0.8988800 0.0318400 + 0.9494300 0.0162200 + 1.0000000 0.0000000 + + 0.0000000 0.0000000 + 0.0129700 -.0134400 + 0.0256400 -.0182000 + 0.0507900 -.0225100 + 0.0759000 -.0254300 + 0.1009800 -.0278500 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0.3000000 0.0051000 + 0.4000000 0.0138000 + 0.5000000 0.0205000 + 0.6000000 0.0242000 + 0.7000000 0.0229000 + 0.8000000 0.0166000 + 0.9000000 0.0083000 + 0.9500000 0.0041500 + 1.0000000 0.0000000 diff --git a/airfoil/data/goe198.dat b/airfoil/data/goe198.dat new file mode 100644 index 0000000..4c24920 --- /dev/null +++ b/airfoil/data/goe198.dat @@ -0,0 +1,38 @@ +GOE 198 (L.F.G. 5294) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0122900 0.0223200 + 0.0246900 0.0329300 + 0.0495700 0.0458700 + 0.0744500 0.0582000 + 0.0993600 0.0682400 + 0.1492200 0.0827100 + 0.1991200 0.0926800 + 0.2990500 0.1010300 + 0.3990300 0.1028700 + 0.4990800 0.0970200 + 0.5991700 0.0874600 + 0.6993100 0.0726100 + 0.7995099 0.0518600 + 0.8997400 0.0275000 + 0.9498500 0.0163800 + 1.0000000 0.0042500 + + 0.0000000 0.0000000 + 0.0126300 -.0135800 + 0.0251300 -.0134600 + 0.0500900 -.0095300 + 0.0750300 -.0034900 + 0.0999900 0.0012400 + 0.1499200 0.0088200 + 0.1998600 0.0150900 + 0.2997700 0.0245300 + 0.3997400 0.0275800 + 0.4997400 0.0274200 + 0.5997800 0.0236700 + 0.6998300 0.0179100 + 0.7999000 0.0107600 + 0.8999600 0.0038000 + 0.9500000 0.0002800 + 1.0000000 -.0042500 diff --git a/airfoil/data/goe199.dat b/airfoil/data/goe199.dat new file mode 100644 index 0000000..df625d6 --- /dev/null +++ b/airfoil/data/goe199.dat @@ -0,0 +1,38 @@ +GOE 199 (L.F.G. 5406) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0124400 0.0206400 + 0.0249100 0.0296700 + 0.0498700 0.0444400 + 0.0748400 0.0556200 + 0.0998100 0.0656900 + 0.1497800 0.0774300 + 0.1997600 0.0833800 + 0.2997400 0.0884700 + 0.3997500 0.0876600 + 0.4997600 0.0816500 + 0.5997900 0.0724400 + 0.6998300 0.0585300 + 0.7998800 0.0419200 + 0.8999299 0.0242100 + 0.9499600 0.0149500 + 1.0000000 0.0055000 + + 0.0000000 0.0000000 + 0.0125200 -.0083600 + 0.0250200 -.0067300 + 0.0500100 -.0029500 + 0.0750000 0.0008200 + 0.0999900 0.0033900 + 0.1499800 0.0081300 + 0.1999700 0.0116800 + 0.2999600 0.0151700 + 0.3999600 0.0154600 + 0.4999600 0.0141500 + 0.5999700 0.0103400 + 0.6999800 0.0052300 + 0.8000000 0.0002200 + 0.9000100 -.0031900 + 0.9500200 -.0056400 + 1.0000000 -.0055000 diff --git a/airfoil/data/goe207.dat b/airfoil/data/goe207.dat new file mode 100644 index 0000000..aa96fba --- /dev/null +++ b/airfoil/data/goe207.dat @@ -0,0 +1,38 @@ +GOE 207 (AVIATIK V8) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0122500 0.0222400 + 0.0246400 0.0329700 + 0.0494000 0.0543500 + 0.0742200 0.0702200 + 0.0991000 0.0812000 + 0.1489100 0.0986500 + 0.1988200 0.1071000 + 0.2987900 0.1098000 + 0.3988600 0.1030100 + 0.4990000 0.0902100 + 0.5991700 0.0751200 + 0.6993600 0.0578300 + 0.7995600 0.0397400 + 0.8997600 0.0215400 + 0.9498600 0.0129000 + 1.0000000 0.0037500 + + 0.0000000 0.0000000 + 0.0126600 -.0146600 + 0.0251500 -.0134200 + 0.0500800 -.0071500 + 0.0750000 0.0000300 + 0.0999400 0.0053000 + 0.1498500 0.0137600 + 0.1997900 0.0194100 + 0.2997500 0.0228100 + 0.3997600 0.0216200 + 0.4997900 0.0187200 + 0.5998400 0.0145300 + 0.6998800 0.0106300 + 0.7999300 0.0060400 + 0.8999900 0.0009400 + 0.9500100 -.0011000 + 1.0000000 -.0037500 diff --git a/airfoil/data/goe210.dat b/airfoil/data/goe210.dat new file mode 100644 index 0000000..a49cd7a --- /dev/null +++ b/airfoil/data/goe210.dat @@ -0,0 +1,38 @@ +GOE 210 (DAIMLER) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0124100 0.0181600 + 0.0248600 0.0281200 + 0.0498000 0.0395500 + 0.0747600 0.0486700 + 0.0997200 0.0557000 + 0.1496800 0.0639500 + 0.1996500 0.0695000 + 0.2996200 0.0753000 + 0.3996200 0.0762000 + 0.4996400 0.0726000 + 0.5996800 0.0640000 + 0.6997400 0.0512000 + 0.7998200 0.0366000 + 0.8999000 0.0207000 + 0.9499500 0.0109500 + 1.0000000 0.0008000 + + 0.0000000 0.0000000 + 0.0125300 -.0057400 + 0.0250300 -.0056000 + 0.0500200 -.0044500 + 0.0750100 -.0022700 + 0.1000000 0.0000000 + 0.1499800 0.0032500 + 0.1999700 0.0058000 + 0.2999600 0.0090000 + 0.3999500 0.0106600 + 0.4999400 0.0118000 + 0.5999400 0.0112000 + 0.6999600 0.0093900 + 0.7999600 0.0072000 + 0.8999800 0.0038000 + 0.9499900 0.0014500 + 1.0000000 -.0008000 diff --git a/airfoil/data/goe217.dat b/airfoil/data/goe217.dat new file mode 100644 index 0000000..04fbaf6 --- /dev/null +++ b/airfoil/data/goe217.dat @@ -0,0 +1,38 @@ +GOE 217 (MVA MK.12) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0100400 0.0440600 + 0.0215600 0.0617000 + 0.0453700 0.0830300 + 0.0694600 0.0993800 + 0.0937800 0.1115300 + 0.1428600 0.1279700 + 0.1922600 0.1387300 + 0.2916700 0.1492700 + 0.3919300 0.1446700 + 0.4927200 0.1304900 + 0.5938000 0.1111300 + 0.6950901 0.0879900 + 0.7965200 0.0624500 + 0.8980700 0.0346100 + 0.9488600 0.0204500 + 1.0000000 0.0037000 + + 0.0000000 0.0000000 + 0.0136000 -.0197400 + 0.0263600 -.0243300 + 0.0517400 -.0311100 + 0.0770700 -.0370000 + 0.1023500 -.0419900 + 0.1526600 -.0476800 + 0.2026500 -.0474900 + 0.3022200 -.0398400 + 0.4013700 -.0246000 + 0.5002200 -.0038900 + 0.5990800 0.0164300 + 0.6983000 0.0304700 + 0.7984900 0.0270600 + 0.8992600 0.0131800 + 0.9497400 0.0047000 + 1.0000000 -.0037000 diff --git a/airfoil/data/goe222.dat b/airfoil/data/goe222.dat new file mode 100644 index 0000000..c53e148 --- /dev/null +++ b/airfoil/data/goe222.dat @@ -0,0 +1,38 @@ +GOE 222 (MVA H.33) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0109700 0.0285900 + 0.0226900 0.0432100 + 0.0465300 0.0649900 + 0.0705200 0.0837700 + 0.0947600 0.0980700 + 0.1436300 0.1191800 + 0.1928800 0.1331200 + 0.2919400 0.1506200 + 0.3917900 0.1534600 + 0.4920900 0.1478300 + 0.5928200 0.1342200 + 0.6941100 0.1101300 + 0.7956401 0.0815700 + 0.8975900 0.0450200 + 0.9487400 0.0235600 + 1.0000000 0.0015000 + + 0.0000000 0.0000000 + 0.0134000 -.0167800 + 0.0262100 -.0226000 + 0.0515900 -.0297400 + 0.0769100 -.0355900 + 0.1020900 -.0390400 + 0.1522900 -.0428500 + 0.2023100 -.0431800 + 0.3018100 -.0338500 + 0.4009700 -.0180500 + 0.5001700 -.0032400 + 0.5995200 0.0090700 + 0.6992000 0.0149100 + 0.7991900 0.0150600 + 0.8994300 0.0106200 + 0.9496900 0.0058100 + 1.0000000 -.0015000 diff --git a/airfoil/data/goe223.dat b/airfoil/data/goe223.dat new file mode 100644 index 0000000..3ba0204 --- /dev/null +++ b/airfoil/data/goe223.dat @@ -0,0 +1,38 @@ +GOE 223 (MVA H.34) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0109000 0.0247100 + 0.0224500 0.0392600 + 0.0459600 0.0622900 + 0.0698000 0.0800400 + 0.0940500 0.0916100 + 0.1426700 0.1127700 + 0.1917000 0.1255100 + 0.2908000 0.1416000 + 0.3906500 0.1438900 + 0.4913300 0.1339400 + 0.5922900 0.1187000 + 0.6937600 0.0960900 + 0.7956401 0.0671200 + 0.8977400 0.0348500 + 0.9488800 0.0171800 + 1.0000000 0.0010000 + + 0.0000000 0.0000000 + 0.0134900 -.0151200 + 0.0262900 -.0197900 + 0.0518000 -.0276300 + 0.0771800 -.0334800 + 0.1024300 -.0373400 + 0.1528900 -.0443600 + 0.2031400 -.0483000 + 0.3030100 -.0463000 + 0.4022000 -.0338600 + 0.5012000 -.0184200 + 0.6002800 -.0042800 + 0.6995500 0.0069700 + 0.7992900 0.0109500 + 0.8994800 0.0079700 + 0.9497600 0.0037300 + 1.0000000 -.0010000 diff --git a/airfoil/data/goe225.dat b/airfoil/data/goe225.dat new file mode 100644 index 0000000..f27d139 --- /dev/null +++ b/airfoil/data/goe225.dat @@ -0,0 +1,38 @@ +GOE 225 (MVA H.35) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0118900 0.0278600 + 0.0241300 0.0398300 + 0.0487300 0.0577700 + 0.0734000 0.0732100 + 0.0981300 0.0853500 + 0.1477500 0.1027400 + 0.1974900 0.1147300 + 0.2971900 0.1285100 + 0.3971400 0.1306000 + 0.4972800 0.1239900 + 0.5975300 0.1126900 + 0.6979200 0.0948800 + 0.7985200 0.0676900 + 0.8991900 0.0367900 + 0.9495500 0.0204000 + 1.0000000 0.0030000 + + 0.0000000 0.0000000 + 0.0128400 -.0154200 + 0.0254200 -.0193400 + 0.0505000 -.0229900 + 0.0755100 -.0232500 + 0.1004800 -.0217000 + 0.1504000 -.0183100 + 0.2002900 -.0132100 + 0.2999700 0.0015700 + 0.3996500 0.0158500 + 0.4993700 0.0288400 + 0.5992000 0.0367200 + 0.6992000 0.0364100 + 0.7993700 0.0286100 + 0.8996800 0.0148000 + 0.9498600 0.0065000 + 1.0000000 -.0030000 diff --git a/airfoil/data/goe226.dat b/airfoil/data/goe226.dat new file mode 100644 index 0000000..f422f43 --- /dev/null +++ b/airfoil/data/goe226.dat @@ -0,0 +1,38 @@ +GOE 226 (MVA H.36) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0117400 0.0298000 + 0.0239300 0.0421100 + 0.0484100 0.0625300 + 0.0729900 0.0788600 + 0.0976500 0.0919900 + 0.1471400 0.1122500 + 0.1968000 0.1255200 + 0.2964400 0.1395600 + 0.3964400 0.1396100 + 0.4966000 0.1331600 + 0.5970100 0.1172200 + 0.6975700 0.0952900 + 0.7983000 0.0668600 + 0.8991300 0.0339300 + 0.9495500 0.0177100 + 1.0000000 0.0010000 + + 0.0000000 0.0000000 + 0.0129000 -.0156700 + 0.0255300 -.0208500 + 0.0506200 -.0242100 + 0.0756300 -.0245700 + 0.1005900 -.0229400 + 0.1504800 -.0188600 + 0.2003300 -.0128900 + 0.2999500 0.0021500 + 0.3995700 0.0166900 + 0.4992700 0.0287300 + 0.5990900 0.0357800 + 0.6990400 0.0378300 + 0.7992300 0.0303800 + 0.8995900 0.0159400 + 0.9498000 0.0077200 + 1.0000000 -.0010000 diff --git a/airfoil/data/goe227.dat b/airfoil/data/goe227.dat new file mode 100644 index 0000000..8db3422 --- /dev/null +++ b/airfoil/data/goe227.dat @@ -0,0 +1,38 @@ +GOE 227 (MVA H.37) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0125000 0.0253600 + 0.0250000 0.0377300 + 0.0500000 0.0584500 + 0.0750000 0.0751700 + 0.1000000 0.0879000 + 0.1500000 0.1083500 + 0.2000000 0.1228000 + 0.2500000 0.1322500 + 0.3000000 0.1377000 + 0.4000000 0.1406000 + 0.5000000 0.1355000 + 0.6000000 0.1184000 + 0.7000000 0.0973000 + 0.8000000 0.0692000 + 0.9000000 0.0381000 + 1.0000000 0.0030000 + + 0.0000000 0.0000000 + 0.0125000 -.0166400 + 0.0250000 -.0222700 + 0.0500000 -.0265500 + 0.0750000 -.0268200 + 0.1000000 -.0261000 + 0.1500000 -.0226500 + 0.2000000 -.0192000 + 0.2500000 -.0137500 + 0.3000000 -.0063000 + 0.4000000 0.0086000 + 0.5000000 0.0215000 + 0.6000000 0.0314000 + 0.7000000 0.0343000 + 0.8000000 0.0322000 + 0.9000000 0.0201000 + 1.0000000 0.0000000 diff --git a/airfoil/data/goe228.dat b/airfoil/data/goe228.dat new file mode 100644 index 0000000..f9dc718 --- /dev/null +++ b/airfoil/data/goe228.dat @@ -0,0 +1,38 @@ +GOE 228 (MVA H.38) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0112700 0.0304600 + 0.0231800 0.0449400 + 0.0472500 0.0679100 + 0.0715200 0.0859000 + 0.0959400 0.1003900 + 0.1451700 0.1207300 + 0.1944400 0.1373700 + 0.2938100 0.1529000 + 0.3938300 0.1524500 + 0.4942300 0.1425200 + 0.5948900 0.1260900 + 0.6958200 0.1031800 + 0.7970300 0.0732800 + 0.8984100 0.0393900 + 0.9491700 0.0204400 + 1.0000000 0.0015000 + + 0.0000000 0.0000000 + 0.0131100 -.0149700 + 0.0258300 -.0204500 + 0.0510800 -.0267300 + 0.0762100 -.0299100 + 0.1013100 -.0324000 + 0.1513900 -.0343700 + 0.2013700 -.0338400 + 0.3010300 -.0253100 + 0.4005400 -.0132800 + 0.5000700 -.0017500 + 0.5995800 0.0102800 + 0.6992800 0.0178200 + 0.7992600 0.0183700 + 0.8995200 0.0119300 + 0.9497600 0.0059700 + 1.0000000 -.0015000 diff --git a/airfoil/data/goe229.dat b/airfoil/data/goe229.dat new file mode 100644 index 0000000..c2d4e0a --- /dev/null +++ b/airfoil/data/goe229.dat @@ -0,0 +1,38 @@ +GOE 229 (MVA H.39) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0109600 0.0232300 + 0.0224100 0.0389900 + 0.0557500 0.0640400 + 0.0695400 0.0821200 + 0.0936100 0.0962200 + 0.1421600 0.1179500 + 0.1913000 0.1309200 + 0.2903100 0.1458000 + 0.3901300 0.1484400 + 0.4907500 0.1391300 + 0.5918500 0.1226600 + 0.6934000 0.0992100 + 0.7953200 0.0703900 + 0.8975300 0.0371900 + 0.9487000 0.0195900 + 1.0000000 0.0010000 + + 0.0000000 0.0000000 + 0.0134400 -.0141100 + 0.0262900 -.0192500 + 0.0518000 -.0270600 + 0.0772600 -.0338600 + 0.1025400 -.0381800 + 0.1530200 -.0453200 + 0.2032600 -.0489800 + 0.3031500 -.0473400 + 0.4023500 -.0352400 + 0.5012800 -.0191700 + 0.6003100 -.0045800 + 0.6995300 0.0070200 + 0.7992900 0.0106500 + 0.8994500 0.0083100 + 0.9497600 0.0036600 + 1.0000000 -.0010000 diff --git a/airfoil/data/goe233.dat b/airfoil/data/goe233.dat new file mode 100644 index 0000000..93e8f44 --- /dev/null +++ b/airfoil/data/goe233.dat @@ -0,0 +1,38 @@ +GOE 233 (MVA CA4) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0119300 0.0265600 + 0.0242000 0.0371200 + 0.0488500 0.0531600 + 0.0735700 0.0659900 + 0.0983400 0.0768300 + 0.1479900 0.0929000 + 0.1977600 0.1032800 + 0.2974700 0.1167400 + 0.3974100 0.1194000 + 0.4975300 0.1138700 + 0.5978200 0.1005400 + 0.6982200 0.0821200 + 0.7987300 0.0584900 + 0.8993200 0.0313700 + 0.9496400 0.0164600 + 1.0000000 0.0015500 + + 0.0000000 0.0000000 + 0.0127600 -.0121200 + 0.0253200 -.0149500 + 0.0504200 -.0195100 + 0.0754500 -.0205700 + 0.1004600 -.0210300 + 0.1503900 -.0178400 + 0.2002700 -.0126600 + 0.2998500 0.0069900 + 0.3992800 0.0333400 + 0.4989100 0.0505000 + 0.5987700 0.0567600 + 0.6988300 0.0538300 + 0.7991200 0.0405000 + 0.8995600 0.0204800 + 0.9498000 0.0092600 + 1.0000000 -.0015500 diff --git a/airfoil/data/goe234.dat b/airfoil/data/goe234.dat new file mode 100644 index 0000000..bec949b --- /dev/null +++ b/airfoil/data/goe234.dat @@ -0,0 +1,38 @@ +GOE 234 (MVA CA5) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0117500 0.0292000 + 0.0239500 0.0407200 + 0.0484400 0.0606400 + 0.0730500 0.0759800 + 0.0977300 0.0884100 + 0.1472200 0.1080800 + 0.1969100 0.1200600 + 0.2965700 0.1333200 + 0.3964900 0.1365900 + 0.4966500 0.1303600 + 0.5970100 0.1164400 + 0.6975300 0.0962300 + 0.7982200 0.0692100 + 0.8990100 0.0386000 + 0.9494700 0.0207000 + 1.0000000 0.0037000 + + 0.0000000 0.0000000 + 0.0128500 -.0135700 + 0.0254600 -.0180500 + 0.0505600 -.0217000 + 0.0756100 -.0237600 + 0.1006700 -.0260100 + 0.1506600 -.0255300 + 0.2005700 -.0221500 + 0.3000200 -.0008900 + 0.3992000 0.0311600 + 0.4986300 0.0532100 + 0.5984200 0.0613800 + 0.6985600 0.0560500 + 0.7988500 0.0446300 + 0.8994300 0.0220200 + 0.9497700 0.0089100 + 1.0000000 -.0037000 diff --git a/airfoil/data/goe235.dat b/airfoil/data/goe235.dat new file mode 100644 index 0000000..1189fe8 --- /dev/null +++ b/airfoil/data/goe235.dat @@ -0,0 +1,38 @@ +GOE 235 (SCHTTE-LANZ) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0121900 0.0203900 + 0.0245900 0.0264800 + 0.0494300 0.0369600 + 0.0743000 0.0453400 + 0.0991900 0.0526300 + 0.1490800 0.0598000 + 0.1990300 0.0631700 + 0.2989600 0.0674000 + 0.3989800 0.0662400 + 0.4990500 0.0619900 + 0.5991900 0.0523300 + 0.6993600 0.0416700 + 0.7995700 0.0277100 + 0.8997700 0.0149600 + 0.9498800 0.0077300 + 1.0000000 0.0016000 + + 0.0000000 0.0000000 + 0.0127400 -.0157000 + 0.0252600 -.0166100 + 0.0502000 -.0130300 + 0.0751600 -.0105400 + 0.1001300 -.0085600 + 0.1500800 -.0050900 + 0.2000300 -.0022200 + 0.2999600 0.0025200 + 0.3999300 0.0045600 + 0.4999400 0.0040000 + 0.5999600 0.0028400 + 0.6999700 0.0017800 + 0.7999800 0.0012200 + 0.9000000 0.0000600 + 0.9500200 -.0010700 + 1.0000000 -.0016000 diff --git a/airfoil/data/goe238.dat b/airfoil/data/goe238.dat new file mode 100644 index 0000000..f15d53c --- /dev/null +++ b/airfoil/data/goe238.dat @@ -0,0 +1,38 @@ +GOE 238 (HANSA-BRANDENBURG) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0121300 0.0236900 + 0.0244700 0.0337800 + 0.0492600 0.0476700 + 0.0740700 0.0595600 + 0.0989100 0.0698400 + 0.1486800 0.0847200 + 0.1985400 0.0937000 + 0.2983800 0.1041500 + 0.3984200 0.1010200 + 0.4986200 0.0885800 + 0.5988900 0.0708400 + 0.6992000 0.0510100 + 0.7995000 0.0322700 + 0.8997400 0.0166400 + 0.9498600 0.0091200 + 1.0000000 0.0000000 + + 0.0000000 0.0000000 + 0.0127200 -.0140000 + 0.0252400 -.0152100 + 0.0501900 -.0122200 + 0.0751400 -.0092300 + 0.1001200 -.0078400 + 0.1500400 -.0028600 + 0.1999700 0.0016200 + 0.2999100 0.0060800 + 0.3998900 0.0073400 + 0.4999100 0.0057000 + 0.5999500 0.0031600 + 0.6999800 0.0010200 + 0.8000100 -.0005200 + 0.9000000 0.0000400 + 0.9500100 -.0004800 + 1.0000000 0.0000000 diff --git a/airfoil/data/goe239.dat b/airfoil/data/goe239.dat new file mode 100644 index 0000000..ce2cd46 --- /dev/null +++ b/airfoil/data/goe239.dat @@ -0,0 +1,38 @@ +GOE 239 (MVA H.31) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0120600 0.0242200 + 0.0243600 0.0350400 + 0.0490800 0.0503900 + 0.0738500 0.0632400 + 0.0986700 0.0733000 + 0.1483700 0.0895000 + 0.1982000 0.0997500 + 0.2980000 0.1098200 + 0.3980000 0.1098400 + 0.4981600 0.1010700 + 0.5983700 0.0894900 + 0.6986500 0.0740200 + 0.7990300 0.0530400 + 0.8994700 0.0290700 + 0.9496900 0.0167800 + 1.0000000 0.0021000 + + 0.0000000 0.0000000 + 0.0127300 -.0123700 + 0.0252900 -.0160400 + 0.0503400 -.0185000 + 0.0753400 -.0189300 + 0.1003400 -.0184700 + 0.1503100 -.0170600 + 0.2002200 -.0122600 + 0.3000100 -.0005400 + 0.3998100 0.0106800 + 0.4997000 0.0162900 + 0.5996600 0.0188100 + 0.6996700 0.0182300 + 0.7997700 0.0126600 + 0.8998700 0.0070800 + 0.9499500 0.0029900 + 1.0000000 -.0021000 diff --git a/airfoil/data/goe240.dat b/airfoil/data/goe240.dat new file mode 100644 index 0000000..b0d84d5 --- /dev/null +++ b/airfoil/data/goe240.dat @@ -0,0 +1,38 @@ +GOE 240 (KOLLER) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0123600 0.0181900 + 0.0247900 0.0284900 + 0.0496900 0.0414700 + 0.0746000 0.0529600 + 0.0995500 0.0606500 + 0.1494700 0.0711200 + 0.1994100 0.0785000 + 0.2993600 0.0850500 + 0.3993600 0.0853000 + 0.4994000 0.0796500 + 0.5994700 0.0708000 + 0.6995800 0.0565500 + 0.7997000 0.0402000 + 0.8998300 0.0232500 + 0.9499100 0.0119200 + 1.0000000 0.0011000 + + 0.0000000 0.0000000 + 0.0125600 -.0085100 + 0.0250600 -.0084100 + 0.0500500 -.0071200 + 0.0750300 -.0037400 + 0.1000000 -.0003500 + 0.1499700 0.0043200 + 0.1999300 0.0089000 + 0.2998900 0.0150500 + 0.3998700 0.0179000 + 0.4998700 0.0176500 + 0.5998800 0.0157000 + 0.6999100 0.0116500 + 0.7999500 0.0070000 + 0.8999800 0.0024500 + 0.9500000 0.0006200 + 1.0000000 -.0011000 diff --git a/airfoil/data/goe241.dat b/airfoil/data/goe241.dat new file mode 100644 index 0000000..2162c68 --- /dev/null +++ b/airfoil/data/goe241.dat @@ -0,0 +1,38 @@ +GOE 241 (MVA PR.1) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0112700 0.0381600 + 0.0231500 0.0573500 + 0.0472800 0.0846200 + 0.0716700 0.1033100 + 0.0961700 0.1189000 + 0.1454300 0.1418800 + 0.1950100 0.1548800 + 0.2945700 0.1687900 + 0.3946200 0.1670100 + 0.4950000 0.1552400 + 0.5956100 0.1364800 + 0.6964400 0.1106300 + 0.7974700 0.0786800 + 0.8986200 0.0427400 + 0.9492800 0.0223700 + 1.0000000 0.0020000 + + 0.0000000 0.0000000 + 0.0129900 -.0152800 + 0.0256300 -.0195700 + 0.0507200 -.0223700 + 0.0757800 -.0242600 + 0.1008300 -.0258500 + 0.1509000 -.0278400 + 0.2008900 -.0277300 + 0.3006300 -.0195200 + 0.4001600 -.0048200 + 0.4995800 0.0130900 + 0.5990500 0.0294900 + 0.6988500 0.0357000 + 0.7989300 0.0333300 + 0.8993599 0.0199600 + 0.9497100 0.0088800 + 1.0000000 -.0020000 diff --git a/airfoil/data/goe242.dat b/airfoil/data/goe242.dat new file mode 100644 index 0000000..190472c --- /dev/null +++ b/airfoil/data/goe242.dat @@ -0,0 +1,38 @@ +GOE 242 (MVA PR.2) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0117900 0.0278000 + 0.0239000 0.0431100 + 0.0483700 0.0637300 + 0.0729600 0.0800600 + 0.0975800 0.0949900 + 0.1470200 0.1167500 + 0.1966800 0.1300200 + 0.2963300 0.1440600 + 0.3962600 0.1466000 + 0.4965300 0.1359600 + 0.5970000 0.1177200 + 0.6975700 0.0952900 + 0.7983000 0.0668600 + 0.8991001 0.0354300 + 0.9495201 0.0190100 + 1.0000000 0.0020000 + + 0.0000000 0.0000000 + 0.0127600 -.0101700 + 0.0253300 -.0128500 + 0.0504300 -.0167100 + 0.0755000 -.0195700 + 0.1005500 -.0214400 + 0.1506000 -.0236600 + 0.2005700 -.0223900 + 0.3004500 -.0175400 + 0.4001100 -.0043000 + 0.4996200 0.0147400 + 0.5992000 0.0314800 + 0.6989700 0.0403200 + 0.7990300 0.0378800 + 0.8994200 0.0229400 + 0.9497000 0.0117200 + 1.0000000 -.0020000 diff --git a/airfoil/data/goe243.dat b/airfoil/data/goe243.dat new file mode 100644 index 0000000..77d40f5 --- /dev/null +++ b/airfoil/data/goe243.dat @@ -0,0 +1,38 @@ +GOE 243 (MVA PR.3) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0108300 0.0384700 + 0.0225700 0.0559800 + 0.0463900 0.0830200 + 0.0705400 0.1025700 + 0.0948600 0.1181300 + 0.1440300 0.1372700 + 0.1934400 0.1509100 + 0.2928600 0.1642400 + 0.3928800 0.1635900 + 0.4933000 0.1539600 + 0.5940900 0.1358400 + 0.6952000 0.1102400 + 0.7965800 0.0786500 + 0.8981700 0.0420700 + 0.9490700 0.0212800 + 1.0000000 0.0015000 + + 0.0000000 0.0000000 + 0.0134500 -.0219100 + 0.0261500 -.0263600 + 0.0513200 -.0302700 + 0.0764000 -.0321800 + 0.1014600 -.0335900 + 0.1515800 -.0364100 + 0.2015800 -.0362300 + 0.3010800 -.0249000 + 0.4003100 -.0070900 + 0.4994500 0.0127300 + 0.5985600 0.0330400 + 0.6980300 0.0453600 + 0.7980800 0.0442200 + 0.8989500 0.0241000 + 0.9495100 0.0113000 + 1.0000000 -.0015000 diff --git a/airfoil/data/goe244.dat b/airfoil/data/goe244.dat new file mode 100644 index 0000000..2c75572 --- /dev/null +++ b/airfoil/data/goe244.dat @@ -0,0 +1,38 @@ +GOE 244 (MVA PR.4) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0116000 0.0407600 + 0.0236000 0.0635200 + 0.0479600 0.0928600 + 0.0725200 0.1126000 + 0.0972100 0.1270400 + 0.1467400 0.1482300 + 0.1964000 0.1635200 + 0.2961400 0.1755200 + 0.3961800 0.1737200 + 0.4963800 0.1644200 + 0.5967900 0.1461300 + 0.6973600 0.1201400 + 0.7981000 0.0865600 + 0.8989900 0.0459800 + 0.9494900 0.0230900 + 1.0000000 0.0010000 + + 0.0000000 0.0000000 + 0.0128700 -.0169200 + 0.0254300 -.0194400 + 0.0504800 -.0218900 + 0.0754700 -.0213400 + 0.1004600 -.0207900 + 0.1504100 -.0187900 + 0.2002800 -.0127900 + 0.2999400 0.0026000 + 0.3995900 0.0185900 + 0.4992100 0.0357800 + 0.5989500 0.0476800 + 0.6988500 0.0523700 + 0.7989600 0.0470800 + 0.8993800 0.0282900 + 0.9496900 0.0138900 + 1.0000000 -.0010000 diff --git a/airfoil/data/goe255.dat b/airfoil/data/goe255.dat new file mode 100644 index 0000000..c876a2b --- /dev/null +++ b/airfoil/data/goe255.dat @@ -0,0 +1,38 @@ +GOE 255 (MVA CA.6) AIRFOIL + 17. 17. + + 0.0000100 0.0000000 + 0.0108500 0.0239500 + 0.0223200 0.0387500 + 0.0457500 0.0613700 + 0.0696700 0.0770300 + 0.0937900 0.0897000 + 0.1425200 0.1080800 + 0.1915900 0.1214800 + 0.2906900 0.1343400 + 0.3903900 0.1387500 + 0.4909900 0.1300200 + 0.5920900 0.1142300 + 0.6936901 0.0910700 + 0.7955101 0.0648300 + 0.8974800 0.0364000 + 0.9486901 0.0189400 + 1.0000000 0.0025000 + + 0.0000100 0.0000000 + 0.0135200 -.0146600 + 0.0265400 -.0221600 + 0.0522400 -.0321800 + 0.0776900 -.0387200 + 0.1030300 -.0436600 + 0.1534300 -.0493700 + 0.2035900 -.0516900 + 0.3035200 -.0507700 + 0.4028700 -.0413800 + 0.5022200 -.0320000 + 0.6016200 -.0233100 + 0.7010900 -.0157100 + 0.8006800 -.0098100 + 0.9004100 -.0059000 + 0.9502700 -.0039500 + 1.0000000 -.0025000 diff --git a/airfoil/data/goe256.dat b/airfoil/data/goe256.dat new file mode 100644 index 0000000..1ce8c76 --- /dev/null +++ b/airfoil/data/goe256.dat @@ -0,0 +1,38 @@ +GOE 256 (JUNKERS E) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0117200 0.0248700 + 0.0238300 0.0375400 + 0.0482000 0.0575100 + 0.0727500 0.0719700 + 0.0974100 0.0830400 + 0.1468700 0.1000900 + 0.1964700 0.1129400 + 0.2960900 0.1252500 + 0.3960700 0.1258800 + 0.4962600 0.1197100 + 0.5966500 0.1071500 + 0.6973000 0.0864900 + 0.7980800 0.0614400 + 0.8989900 0.0323900 + 0.9494600 0.0173700 + 1.0000000 0.0012500 + + 0.0000000 0.0000000 + 0.0131900 -.0220900 + 0.0258900 -.0283900 + 0.0510400 -.0334000 + 0.0760900 -.0348200 + 0.1011100 -.0356400 + 0.1511300 -.0362800 + 0.2011400 -.0365100 + 0.3010800 -.0345900 + 0.4009800 -.0314700 + 0.5008900 -.0283500 + 0.6007900 -.0252300 + 0.7006900 -.0221000 + 0.8005900 -.0189800 + 0.9003800 -.0120600 + 0.9502000 -.0064100 + 1.0000000 -.0012500 diff --git a/airfoil/data/goe257.dat b/airfoil/data/goe257.dat new file mode 100644 index 0000000..7027bbb --- /dev/null +++ b/airfoil/data/goe257.dat @@ -0,0 +1,38 @@ +GOE 257 AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0124500 0.0161400 + 0.0249200 0.0252800 + 0.0498800 0.0376600 + 0.0748400 0.0484400 + 0.0998200 0.0575200 + 0.1497800 0.0694800 + 0.1997500 0.0766400 + 0.2997300 0.0849600 + 0.3997300 0.0836800 + 0.4997500 0.0776000 + 0.5997900 0.0661200 + 0.6998300 0.0526400 + 0.7998700 0.0394600 + 0.8999299 0.0232800 + 0.9499500 0.0148400 + 1.0000000 0.0064000 + + 0.0000000 0.0000000 + 0.0125300 -.0095600 + 0.0250300 -.0095200 + 0.0500300 -.0089400 + 0.0750300 -.0082600 + 0.1000200 -.0071800 + 0.1500200 -.0059200 + 0.2000200 -.0046600 + 0.3000100 -.0033400 + 0.4000100 -.0025200 + 0.5000100 -.0027000 + 0.6000100 -.0023800 + 0.7000100 -.0030600 + 0.8000100 -.0038400 + 0.9000200 -.0051200 + 0.9500200 -.0065600 + 1.0000000 -.0064000 diff --git a/airfoil/data/goe264.dat b/airfoil/data/goe264.dat new file mode 100644 index 0000000..64a52a4 --- /dev/null +++ b/airfoil/data/goe264.dat @@ -0,0 +1,38 @@ +GOE 264 AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0122100 0.0165200 + 0.0276500 0.0267600 + 0.0497600 0.0382200 + 0.0746800 0.0492800 + 0.0996300 0.0577400 + 0.1495400 0.0723600 + 0.2017300 0.0818400 + 0.2892600 0.0880200 + 0.3994500 0.0863600 + 0.4994900 0.0795000 + 0.5995600 0.0689400 + 0.6996400 0.0567800 + 0.7997400 0.0409200 + 0.8998500 0.0228600 + 0.9499199 0.0126800 + 1.0000000 0.0032000 + + 0.0000000 0.0000000 + 0.0125600 -.0092200 + 0.0261500 -.0109600 + 0.0500500 -.0079800 + 0.0750300 -.0040200 + 0.1000000 0.0006400 + 0.1499400 0.0100600 + 0.1998900 0.0172800 + 0.2998300 0.0259200 + 0.3998300 0.0265600 + 0.4998500 0.0235000 + 0.5998700 0.0198400 + 0.6999100 0.0145800 + 0.7999400 0.0094200 + 0.8999700 0.0046600 + 0.9499900 0.0012800 + 1.0000000 -.0032000 diff --git a/airfoil/data/goe265.dat b/airfoil/data/goe265.dat new file mode 100644 index 0000000..4437d5a --- /dev/null +++ b/airfoil/data/goe265.dat @@ -0,0 +1,38 @@ +GOE 265 AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0122600 0.0266100 + 0.0246500 0.0390200 + 0.0494900 0.0564400 + 0.0743800 0.0689700 + 0.0993000 0.0778900 + 0.1491700 0.0923400 + 0.1990900 0.1012800 + 0.2990400 0.1069800 + 0.3990700 0.1035700 + 0.4991700 0.0929700 + 0.5993000 0.0780600 + 0.6994600 0.0602600 + 0.7996300 0.0416600 + 0.8998100 0.0215500 + 0.9498900 0.0118000 + 1.0000000 0.0010500 + + 0.0000000 0.0000000 + 0.0125700 -.0082900 + 0.0250900 -.0097800 + 0.0500700 -.0075500 + 0.0750200 -.0023300 + 0.0999600 0.0039900 + 0.1498600 0.0159400 + 0.1997700 0.0252900 + 0.2996600 0.0376800 + 0.3996300 0.0415800 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0.0022900 + 1.0000000 0.0000000 diff --git a/airfoil/data/goe276.dat b/airfoil/data/goe276.dat new file mode 100644 index 0000000..924db69 --- /dev/null +++ b/airfoil/data/goe276.dat @@ -0,0 +1,38 @@ +GOE 276 (DAIMLER VII) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0124100 0.0173700 + 0.0248600 0.0265300 + 0.0497900 0.0396700 + 0.0747300 0.0496000 + 0.0997000 0.0563400 + 0.1496400 0.0665100 + 0.1996100 0.0723800 + 0.2995900 0.0766200 + 0.3996000 0.0734600 + 0.4996300 0.0692000 + 0.5996600 0.0623400 + 0.6997200 0.0526800 + 0.7997900 0.0387200 + 0.8998700 0.0232600 + 0.9499199 0.0152300 + 1.0000000 0.0040000 + + 0.0000000 0.0000000 + 0.0125500 -.0088300 + 0.0250500 -.0087600 + 0.0500300 -.0061300 + 0.0750200 -.0040800 + 0.1000100 -.0024600 + 0.1500000 -.0005900 + 0.1999900 0.0010300 + 0.2999800 0.0040200 + 0.3999700 0.0061600 + 0.4999600 0.0067000 + 0.5999700 0.0061400 + 0.6999700 0.0050800 + 0.7999800 0.0029200 + 0.9000000 0.0002600 + 0.9500100 -.0021700 + 1.0000000 -.0040000 diff --git a/airfoil/data/goe277.dat b/airfoil/data/goe277.dat new file mode 100644 index 0000000..9fbe492 --- /dev/null +++ b/airfoil/data/goe277.dat @@ -0,0 +1,38 @@ +GOE 277 (DAIMLER VIII) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0123300 0.0185100 + 0.0247500 0.0283200 + 0.0496200 0.0427500 + 0.0745300 0.0526700 + 0.0994500 0.0609000 + 0.1493400 0.0735400 + 0.1992700 0.0813900 + 0.2992300 0.0855900 + 0.3992500 0.0831900 + 0.4993100 0.0761900 + 0.5994000 0.0662900 + 0.6995201 0.0533000 + 0.7996500 0.0391000 + 0.8998100 0.0214000 + 0.9498900 0.0117500 + 1.0000000 0.0016000 + + 0.0000000 0.0000000 + 0.0125900 -.0094900 + 0.0250900 -.0103700 + 0.0500800 -.0090500 + 0.0750600 -.0077500 + 0.1000500 -.0063900 + 0.1500300 -.0037500 + 0.2000100 -.0015000 + 0.2999800 0.0022000 + 0.3999700 0.0038000 + 0.4999600 0.0047000 + 0.5999600 0.0044000 + 0.6999700 0.0033600 + 0.7999800 0.0022000 + 0.8999900 0.0007000 + 0.9500100 -.0005500 + 1.0000000 -.0016000 diff --git a/airfoil/data/goe278.dat b/airfoil/data/goe278.dat new file mode 100644 index 0000000..646f77a --- /dev/null +++ b/airfoil/data/goe278.dat @@ -0,0 +1,38 @@ +GOE 278 (DAIMLER IX) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0123500 0.0203900 + 0.0248000 0.0277800 + 0.0497100 0.0395600 + 0.0746400 0.0495400 + 0.0995800 0.0575300 + 0.1495000 0.0682900 + 0.1994500 0.0754600 + 0.2994200 0.0797900 + 0.3994300 0.0785200 + 0.4994600 0.0734500 + 0.5995300 0.0647800 + 0.6996100 0.0541100 + 0.7997100 0.0392400 + 0.8998500 0.0211700 + 0.9499199 0.0116300 + 1.0000000 0.0010000 + + 0.0000000 0.0000000 + 0.0125600 -.0082100 + 0.0250600 -.0076200 + 0.0500300 -.0048000 + 0.0750200 -.0020500 + 0.1000000 0.0002300 + 0.1499800 0.0026900 + 0.1999700 0.0035600 + 0.2999600 0.0053900 + 0.3999600 0.0061200 + 0.4999600 0.0061800 + 0.5999600 0.0059800 + 0.6999700 0.0046100 + 0.7999800 0.0027400 + 0.9000000 0.0003700 + 0.9500100 -.0004300 + 1.0000000 -.0010000 diff --git a/airfoil/data/goe279.dat b/airfoil/data/goe279.dat new file mode 100644 index 0000000..cedafb1 --- /dev/null +++ b/airfoil/data/goe279.dat @@ -0,0 +1,38 @@ +GOE 279 (DAIMLER X) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0124100 0.0235500 + 0.0248800 0.0320000 + 0.0498200 0.0454900 + 0.0747900 0.0555900 + 0.0997600 0.0624800 + 0.1497200 0.0730800 + 0.1996900 0.0795700 + 0.2996800 0.0841500 + 0.3996800 0.0837400 + 0.4997000 0.0786200 + 0.5997300 0.0702100 + 0.6997700 0.0593900 + 0.7998300 0.0433800 + 0.8999100 0.0242600 + 0.9499500 0.0135600 + 1.0000000 0.0018500 + + 0.0000000 0.0000000 + 0.0125200 -.0056500 + 0.0250200 -.0051000 + 0.0500100 -.0015100 + 0.0750000 0.0006900 + 0.0999900 0.0026800 + 0.1499800 0.0052800 + 0.1999700 0.0075700 + 0.2999600 0.0098500 + 0.3999600 0.0108400 + 0.4999600 0.0099200 + 0.5999700 0.0086100 + 0.6999700 0.0069900 + 0.7999800 0.0051200 + 0.8999900 0.0021500 + 0.9500000 0.0004600 + 1.0000000 -.0018500 diff --git a/airfoil/data/goe280.dat b/airfoil/data/goe280.dat new file mode 100644 index 0000000..e7daf4d --- /dev/null +++ b/airfoil/data/goe280.dat @@ -0,0 +1,38 @@ +GOE 280 (DAIMLER XI) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0124500 0.0167300 + 0.0249200 0.0306700 + 0.0498800 0.0461300 + 0.0748400 0.0575000 + 0.0998300 0.0645700 + 0.1498000 0.0741000 + 0.1997800 0.0800400 + 0.2997700 0.0851100 + 0.3997700 0.0833800 + 0.4997900 0.0771500 + 0.5998200 0.0683200 + 0.6998500 0.0558900 + 0.7998900 0.0417600 + 0.8999400 0.0234300 + 0.9499600 0.0138600 + 1.0000000 0.0040000 + + 0.0000000 0.0000000 + 0.0125200 -.0066700 + 0.0250200 -.0057300 + 0.0500100 -.0025600 + 0.0750000 -.0006000 + 0.1000000 0.0010700 + 0.1499900 0.0033000 + 0.1999900 0.0048400 + 0.2999800 0.0058100 + 0.3999800 0.0055800 + 0.4999900 0.0052500 + 0.5999900 0.0045200 + 0.6999900 0.0030400 + 0.8000000 0.0013600 + 0.9000000 -.0007700 + 0.9500100 -.0023300 + 1.0000000 -.0040000 diff --git a/airfoil/data/goe281.dat b/airfoil/data/goe281.dat new file mode 100644 index 0000000..b04b940 --- /dev/null +++ b/airfoil/data/goe281.dat @@ -0,0 +1,38 @@ +GOE 281 (DAIMLER XII) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0124000 0.0165700 + 0.0248400 0.0266500 + 0.0497500 0.0425900 + 0.0746900 0.0533400 + 0.0996400 0.0607900 + 0.1495800 0.0717800 + 0.1995400 0.0783800 + 0.2995000 0.0850700 + 0.3995100 0.0838600 + 0.4995300 0.0791500 + 0.5995900 0.0688400 + 0.6996700 0.0564300 + 0.7997600 0.0412200 + 0.8998600 0.0233100 + 0.9499199 0.0128000 + 1.0000000 0.0026000 + + 0.0000000 0.0000000 + 0.0125500 -.0084300 + 0.0250400 -.0074500 + 0.0500300 -.0056000 + 0.0750200 -.0040600 + 0.1000200 -.0029100 + 0.1500000 -.0005100 + 0.1999900 0.0012800 + 0.2999700 0.0046700 + 0.3999600 0.0070600 + 0.4999500 0.0076500 + 0.5999600 0.0075400 + 0.6999700 0.0051300 + 0.7999900 0.0022200 + 0.9000000 -.0000900 + 0.9500100 -.0016900 + 1.0000000 -.0026000 diff --git a/airfoil/data/goe282.dat b/airfoil/data/goe282.dat new file mode 100644 index 0000000..33b3981 --- /dev/null +++ b/airfoil/data/goe282.dat @@ -0,0 +1,38 @@ +GOE 282 (DAIMLER XIII) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0122600 0.0189600 + 0.0245800 0.0325200 + 0.0493800 0.0483400 + 0.0742400 0.0588600 + 0.0991300 0.0677800 + 0.1489600 0.0807200 + 0.1988700 0.0877700 + 0.2987800 0.0946500 + 0.3987900 0.0941400 + 0.4988700 0.0874400 + 0.5989900 0.0779300 + 0.6991700 0.0647200 + 0.7993700 0.0489100 + 0.8996400 0.0282100 + 0.9497899 0.0165500 + 1.0000000 0.0032000 + + 0.0000000 0.0000000 + 0.0126300 -.0100400 + 0.0251700 -.0128800 + 0.0501900 -.0145500 + 0.0752000 -.0151300 + 0.1001800 -.0139100 + 0.1501100 -.0087600 + 0.2000400 -.0033200 + 0.2999500 0.0039700 + 0.3998900 0.0063200 + 0.4999000 0.0075500 + 0.5999000 0.0077400 + 0.6999199 0.0063300 + 0.7999500 0.0039200 + 0.8999900 0.0005100 + 0.9500200 -.0013400 + 1.0000000 -.0032000 diff --git a/airfoil/data/goe284.dat b/airfoil/data/goe284.dat new file mode 100644 index 0000000..14a71d1 --- /dev/null +++ b/airfoil/data/goe284.dat @@ -0,0 +1,38 @@ +GOE 284 AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 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0.1365300 + 0.3929200 0.1352700 + 0.4935400 0.1234400 + 0.5944900 0.1052200 + 0.6956000 0.0840100 + 0.7968600 0.0599200 + 0.8982800 0.0329200 + 0.9490300 0.0184800 + 1.0000000 0.0029500 + + 0.0000000 0.0000000 + 0.0137300 -.0233800 + 0.0265600 -.0298100 + 0.0519500 -.0372800 + 0.0771900 -.0417600 + 0.1023100 -.0440400 + 0.1523800 -.0455200 + 0.2023400 -.0447100 + 0.3019200 -.0365900 + 0.4012400 -.0237000 + 0.5006600 -.0125900 + 0.6002400 -.0044800 + 0.6999900 0.0001400 + 0.7999300 0.0012800 + 0.8999700 0.0006100 + 0.9500500 -.0009600 + 1.0000000 -.0029500 diff --git a/airfoil/data/goe289.dat b/airfoil/data/goe289.dat new file mode 100644 index 0000000..88992bd --- /dev/null +++ b/airfoil/data/goe289.dat @@ -0,0 +1,38 @@ +GOE 289 (MVA 289) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0125000 0.0260100 + 0.0250000 0.0390100 + 0.0500000 0.0605200 + 0.0750000 0.0770400 + 0.1000000 0.0915500 + 0.1500000 0.1140800 + 0.2000000 0.1291000 + 0.3000000 0.1416500 + 0.4000000 0.1402000 + 0.5000000 0.1292500 + 0.6000000 0.1118000 + 0.7000000 0.0888500 + 0.8000000 0.0629000 + 0.9000000 0.0329500 + 0.9500000 0.0174700 + 1.0000000 0.0000000 + + 0.0000000 0.0000000 + 0.0125000 -.0194900 + 0.0250000 -.0244900 + 0.0500000 -.0304700 + 0.0750000 -.0334600 + 0.1000000 -.0344500 + 0.1500000 -.0339200 + 0.2000000 -.0324000 + 0.3000000 -.0263500 + 0.4000000 -.0178000 + 0.5000000 -.0117500 + 0.6000000 -.0067000 + 0.7000000 -.0026500 + 0.8000000 -.0006000 + 0.9000000 -.0000500 + 0.9500000 -.0005200 + 1.0000000 0.0000000 diff --git a/airfoil/data/goe290.dat b/airfoil/data/goe290.dat new file mode 100644 index 0000000..e85c589 --- /dev/null +++ b/airfoil/data/goe290.dat @@ -0,0 +1,38 @@ +GOE 290 (MVA 290) AIRFOIL + 17. 17. + + 0.0000100 0.0000000 + 0.0105800 0.0281200 + 0.0223400 0.0390300 + 0.0460000 0.0585500 + 0.0699500 0.0738800 + 0.0941900 0.0850400 + 0.1429000 0.1038700 + 0.1921800 0.1143400 + 0.2914700 0.1247400 + 0.3916500 0.1220900 + 0.4925700 0.1086900 + 0.5937200 0.0918100 + 0.6950400 0.0725400 + 0.7965100 0.0509800 + 0.8980400 0.0287300 + 0.9489400 0.0155100 + 1.0000000 0.0030000 + + 0.0000100 0.0000000 + 0.0140700 -.0228400 + 0.0270700 -.0302500 + 0.0526000 -.0380000 + 0.0779000 -.0422700 + 0.1031400 -.0458500 + 0.1534400 -.0502000 + 0.2036200 -.0528700 + 0.3034700 -.0506400 + 0.4030000 -.0438300 + 0.5025400 -.0370300 + 0.6020700 -.0302200 + 0.7016000 -.0234100 + 0.8011400 -.0166000 + 0.9006700 -.0097900 + 0.9504400 -.0063900 + 1.0000000 -.0030000 diff --git a/airfoil/data/goe298.dat b/airfoil/data/goe298.dat new file mode 100644 index 0000000..3e0a235 --- /dev/null +++ b/airfoil/data/goe298.dat @@ -0,0 +1,38 @@ +GOE 298 AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0113300 0.0282700 + 0.0233400 0.0399700 + 0.0475900 0.0581700 + 0.0720800 0.0703900 + 0.0967700 0.0789100 + 0.1462200 0.0912600 + 0.1959500 0.0988200 + 0.2956900 0.1039600 + 0.3956900 0.1040000 + 0.4960800 0.0944600 + 0.5966500 0.0809300 + 0.6973300 0.0626500 + 0.7982100 0.0430900 + 0.8990900 0.0218700 + 0.9494700 0.0127600 + 1.0000000 0.0029500 + + 0.0000000 0.0000000 + 0.0135800 -.0260400 + 0.0264000 -.0338100 + 0.0516700 -.0402600 + 0.0767100 -.0412200 + 0.1016200 -.0389900 + 0.1514100 -.0340200 + 0.2012000 -.0289600 + 0.3008300 -.0201300 + 0.4005400 -.0130000 + 0.5004100 -.0094700 + 0.6002900 -.0070200 + 0.7002400 -.0055300 + 0.8001700 -.0041300 + 0.9001000 -.0023900 + 0.9500800 -.0020200 + 1.0000000 -.0029500 diff --git a/airfoil/data/goe29b.dat b/airfoil/data/goe29b.dat new file mode 100644 index 0000000..1974007 --- /dev/null +++ b/airfoil/data/goe29b.dat @@ -0,0 +1,38 @@ +GOE 29B AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0120400 0.0248200 + 0.0242800 0.0389500 + 0.0488800 0.0600100 + 0.0736200 0.0743700 + 0.0984300 0.0843300 + 0.1481700 0.0986600 + 0.1980300 0.1056800 + 0.2979200 0.1120400 + 0.3980100 0.1072000 + 0.4982100 0.0962700 + 0.5985100 0.0802300 + 0.6988300 0.0630000 + 0.7992000 0.0428700 + 0.8995900 0.0218300 + 0.9497800 0.0115700 + 1.0000000 0.0014000 + + 0.0000000 0.0000000 + 0.0128200 -.0169600 + 0.0253600 -.0195300 + 0.0503000 -.0162600 + 0.0751800 -.0096000 + 0.1000800 -.0042400 + 0.1499100 0.0050900 + 0.1997800 0.0116200 + 0.2996500 0.0189700 + 0.3996100 0.0208300 + 0.4996200 0.0204900 + 0.5996500 0.0186500 + 0.6997200 0.0153100 + 0.7998000 0.0108800 + 0.8999200 0.0042400 + 0.9499800 0.0011700 + 1.0000000 -.0014000 diff --git a/airfoil/data/goe300.dat b/airfoil/data/goe300.dat new file mode 100644 index 0000000..03d4da8 --- /dev/null +++ b/airfoil/data/goe300.dat @@ -0,0 +1,32 @@ +GOE 300 (FRIEDRICHSHAFEN G20) AIRFOIL + 14. 14. + + 0.0000000 0.0000000 + 0.0250000 0.0389500 + 0.0500000 0.0566000 + 0.1000000 0.0784000 + 0.1500000 0.0915000 + 0.2000000 0.1015000 + 0.3000000 0.1090000 + 0.4000000 0.1078000 + 0.5000000 0.0989000 + 0.6000000 0.0854000 + 0.7000000 0.0685000 + 0.8000000 0.0485000 + 0.9000000 0.0256000 + 1.0000000 0.0018000 + + 0.0000000 0.0000000 + 0.0250000 -.0097500 + 0.0500000 -.0080000 + 0.1000000 0.0030000 + 0.1500000 0.0125000 + 0.2000000 0.0186000 + 0.3000000 0.0247000 + 0.4000000 0.0245000 + 0.5000000 0.0215000 + 0.6000000 0.0173000 + 0.7000000 0.0130000 + 0.8000000 0.0086000 + 0.9000000 0.0040000 + 1.0000000 0.0000000 diff --git a/airfoil/data/goe301.dat b/airfoil/data/goe301.dat new file mode 100644 index 0000000..f314d1b --- /dev/null +++ b/airfoil/data/goe301.dat @@ -0,0 +1,38 @@ +GOE 301 (FRIEDRICHSHAFEN G 13) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0122200 0.0274200 + 0.0246000 0.0395500 + 0.0494200 0.0573000 + 0.0742800 0.0710600 + 0.0991800 0.0808100 + 0.1490200 0.0958200 + 0.1989300 0.1053300 + 0.2886400 0.1137400 + 0.3988500 0.1123700 + 0.4989400 0.1043900 + 0.5990800 0.0904100 + 0.6992500 0.0734300 + 0.7994400 0.0544500 + 0.8996800 0.0309800 + 0.9498200 0.0179900 + 1.0000000 0.0015000 + + 0.0000000 0.0000000 + 0.0126000 -.0100700 + 0.0251200 -.0114400 + 0.0500900 -.0086900 + 0.0750500 -.0044300 + 0.1000100 -.0011800 + 0.1499600 0.0043300 + 0.1999100 0.0090400 + 0.2998500 0.0148600 + 0.3998200 0.0173800 + 0.4998200 0.0179000 + 0.5998200 0.0174200 + 0.6998500 0.0144400 + 0.7998900 0.0104600 + 0.8999400 0.0054800 + 0.9499800 0.0016900 + 1.0000000 -.0015000 diff --git a/airfoil/data/goe303.dat b/airfoil/data/goe303.dat new file mode 100644 index 0000000..6064fa5 --- /dev/null +++ b/airfoil/data/goe303.dat @@ -0,0 +1,38 @@ +GOE 303 (FRIEDRICHSHAFEN G03) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0122400 0.0258300 + 0.0246200 0.0372500 + 0.0494600 0.0530100 + 0.0743400 0.0647600 + 0.0992400 0.0745200 + 0.1490900 0.0887300 + 0.1990100 0.0970400 + 0.2989100 0.1059600 + 0.3989100 0.1062900 + 0.4989800 0.0993100 + 0.5991000 0.0873400 + 0.6992700 0.0716700 + 0.7994600 0.0526900 + 0.8997000 0.0292200 + 0.9498300 0.0167400 + 1.0000000 0.0022500 + + 0.0000000 0.0000000 + 0.0126200 -.0105800 + 0.0251300 -.0122400 + 0.0501200 -.0119900 + 0.0751000 -.0099300 + 0.1000800 -.0074700 + 0.1500300 -.0024600 + 0.1999800 0.0021500 + 0.2999200 0.0075700 + 0.3998800 0.0113000 + 0.4998700 0.0123200 + 0.5998900 0.0111500 + 0.6999100 0.0087700 + 0.7999400 0.0057000 + 0.8999900 0.0012200 + 0.9500100 -.0011600 + 1.0000000 -.0022500 diff --git a/airfoil/data/goe304.dat b/airfoil/data/goe304.dat new file mode 100644 index 0000000..882d91f --- /dev/null +++ b/airfoil/data/goe304.dat @@ -0,0 +1,38 @@ +GOE 304 (FRIEDRICHSHAFEN G02) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0121000 0.0269800 + 0.0244400 0.0379600 + 0.0491900 0.0542300 + 0.0740300 0.0651000 + 0.0989000 0.0742700 + 0.1487000 0.0873100 + 0.1985700 0.0960500 + 0.2984300 0.1057300 + 0.3984200 0.1065200 + 0.4985100 0.1004000 + 0.5986900 0.0880900 + 0.6989400 0.0714800 + 0.7992401 0.0513700 + 0.8995800 0.0282600 + 0.9497700 0.0153000 + 1.0000000 0.0011500 + + 0.0000000 0.0000000 + 0.0127100 -.0142100 + 0.0252300 -.0156300 + 0.0501700 -.0117500 + 0.0751200 -.0078800 + 0.1000600 -.0039100 + 0.1499600 0.0027300 + 0.1998800 0.0082700 + 0.2997600 0.0159500 + 0.3997000 0.0199400 + 0.4996900 0.0207200 + 0.5997100 0.0195100 + 0.6997800 0.0148900 + 0.7998500 0.0098800 + 0.8999400 0.0040600 + 0.9499800 0.0013100 + 1.0000000 -.0011500 diff --git a/airfoil/data/goe308.dat b/airfoil/data/goe308.dat new file mode 100644 index 0000000..2819491 --- /dev/null +++ b/airfoil/data/goe308.dat @@ -0,0 +1,38 @@ +GOE 308 (MVA H.40) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0124000 0.0175700 + 0.0248400 0.0270500 + 0.0497500 0.0427900 + 0.0746800 0.0547400 + 0.0996200 0.0638900 + 0.1495500 0.0761800 + 0.1995000 0.0843800 + 0.2994600 0.0908700 + 0.3994800 0.0879600 + 0.4995200 0.0811500 + 0.5995800 0.0706400 + 0.6996601 0.0573300 + 0.7997600 0.0408200 + 0.8998700 0.0228100 + 0.9499300 0.0123000 + 1.0000000 0.0000000 + + 0.0000000 0.0000000 + 0.0125600 -.0093300 + 0.0250600 -.0105500 + 0.0500600 -.0109000 + 0.0750600 -.0094600 + 0.1000300 -.0058100 + 0.1500000 -.0004100 + 0.1999700 0.0048800 + 0.2999400 0.0099700 + 0.3999400 0.0101600 + 0.4999600 0.0069500 + 0.5999800 0.0035400 + 0.7000000 -.0001700 + 0.8000300 -.0051800 + 0.9000300 -.0042900 + 0.9500100 -.0023900 + 1.0000000 0.0000000 diff --git a/airfoil/data/goe309.dat b/airfoil/data/goe309.dat new file mode 100644 index 0000000..ec4d0b9 --- /dev/null +++ b/airfoil/data/goe309.dat @@ -0,0 +1,38 @@ +GOE 309 (MVA H.41) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0125100 0.0158900 + 0.0250200 0.0264800 + 0.0500300 0.0430600 + 0.0750400 0.0543500 + 0.1000400 0.0633300 + 0.1500500 0.0747900 + 0.2000600 0.0820600 + 0.3000600 0.0888900 + 0.4000600 0.0866200 + 0.5000600 0.0791500 + 0.6000500 0.0674800 + 0.7000400 0.0525100 + 0.8000300 0.0365400 + 0.9000100 0.0195700 + 0.9500100 0.0102400 + 1.0000000 0.0020000 + + 0.0000000 0.0000000 + 0.0124900 -.0085100 + 0.0249900 -.0101200 + 0.0499900 -.0103300 + 0.0749900 -.0090500 + 0.1000000 -.0064700 + 0.1500000 -.0027000 + 0.2000000 0.0000600 + 0.3000000 0.0045900 + 0.4000000 0.0026200 + 0.5000000 -.0017500 + 0.6000000 -.0068200 + 0.6999900 -.0101900 + 0.7999900 -.0106600 + 0.8999900 -.0075300 + 0.9500000 -.0048600 + 1.0000000 -.0020000 diff --git a/airfoil/data/goe310.dat b/airfoil/data/goe310.dat new file mode 100644 index 0000000..137328c --- /dev/null +++ b/airfoil/data/goe310.dat @@ -0,0 +1,38 @@ +GOE 310 (MVA H.42) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0123100 0.0176300 + 0.0247200 0.0259600 + 0.0496100 0.0366300 + 0.0744900 0.0483900 + 0.0994000 0.0570500 + 0.1492700 0.0686800 + 0.1991900 0.0766100 + 0.2990900 0.0856700 + 0.3990800 0.0867300 + 0.4991500 0.0803900 + 0.5992600 0.0697500 + 0.6994000 0.0566100 + 0.7995700 0.0406800 + 0.8997800 0.0211400 + 0.9498800 0.0110700 + 1.0000000 0.0000000 + + 0.0000000 0.0000000 + 0.0126000 -.0094700 + 0.0251100 -.0108300 + 0.0501500 -.0137700 + 0.0751600 -.0151000 + 0.1001500 -.0145400 + 0.1501100 -.0106100 + 0.2000500 -.0042800 + 0.2999500 0.0042800 + 0.3999000 0.0095400 + 0.4999200 0.0074000 + 0.5999900 0.0010600 + 0.7000300 -.0031800 + 0.8000600 -.0058200 + 0.9000599 -.0052600 + 0.9500400 -.0037300 + 1.0000000 0.0000000 diff --git a/airfoil/data/goe311.dat b/airfoil/data/goe311.dat new file mode 100644 index 0000000..b81e210 --- /dev/null +++ b/airfoil/data/goe311.dat @@ -0,0 +1,38 @@ +GOE 311 (MVA H.43) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0123000 0.0192300 + 0.0246800 0.0299600 + 0.0495100 0.0461200 + 0.0744000 0.0569900 + 0.0992900 0.0673500 + 0.1491300 0.0816800 + 0.1990300 0.0912100 + 0.2989300 0.1012700 + 0.3989300 0.1007300 + 0.4990400 0.0906900 + 0.5991700 0.0784500 + 0.6993500 0.0615100 + 0.7995400 0.0434800 + 0.8997600 0.0223400 + 0.9498800 0.0111700 + 1.0000000 0.0021000 + + 0.0000000 0.0000000 + 0.0125900 -.0083700 + 0.0251300 -.0119300 + 0.0501300 -.0121700 + 0.0751300 -.0119000 + 0.1001000 -.0092400 + 0.1500100 -.0005100 + 0.1999300 0.0069200 + 0.2998100 0.0180800 + 0.3997800 0.0207400 + 0.4998300 0.0165000 + 0.5998900 0.0100600 + 0.6999600 0.0037200 + 0.8000200 -.0015200 + 0.9000300 -.0028600 + 0.9500300 -.0026300 + 1.0000000 -.0021000 diff --git a/airfoil/data/goe314.dat b/airfoil/data/goe314.dat new file mode 100644 index 0000000..5ff0de6 --- /dev/null +++ b/airfoil/data/goe314.dat @@ -0,0 +1,38 @@ +GOE 314 (HANSA-BRANDENBURG) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0121400 0.0204800 + 0.0245500 0.0306600 + 0.0493500 0.0439300 + 0.0741800 0.0558900 + 0.0990400 0.0654600 + 0.1488700 0.0769900 + 0.1987700 0.0835200 + 0.2987200 0.0870900 + 0.3987800 0.0826600 + 0.4989000 0.0746300 + 0.5990600 0.0641100 + 0.6992600 0.0505800 + 0.7994900 0.0349500 + 0.8997200 0.0190300 + 0.9498500 0.0103600 + 1.0000000 0.0000000 + + 0.0000000 0.0000000 + 0.0127100 -.0130100 + 0.0252100 -.0143300 + 0.0501500 -.0107600 + 0.0751100 -.0073000 + 0.1000500 -.0037300 + 0.1499900 0.0007000 + 0.1999400 0.0040400 + 0.2999000 0.0067100 + 0.3999000 0.0069800 + 0.4999100 0.0058500 + 0.5999300 0.0046200 + 0.6999700 0.0018900 + 0.7999800 0.0002500 + 0.9005300 -.0010300 + 0.9500000 -.0002300 + 1.0000000 0.0000000 diff --git a/airfoil/data/goe315.dat b/airfoil/data/goe315.dat new file mode 100644 index 0000000..17be3e0 --- /dev/null +++ b/airfoil/data/goe315.dat @@ -0,0 +1,38 @@ +GOE 315 (HANSA-BRANDENBURG III.5) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0122700 0.0214300 + 0.0247000 0.0287600 + 0.0495500 0.0420300 + 0.0744600 0.0513900 + 0.0993700 0.0595500 + 0.1492500 0.0707800 + 0.1991900 0.0766100 + 0.2991400 0.0813700 + 0.3991700 0.0787300 + 0.4992600 0.0696900 + 0.5993800 0.0583500 + 0.6995400 0.0438200 + 0.7996800 0.0297800 + 0.8998300 0.0159400 + 0.9499100 0.0084700 + 1.0000000 0.0000000 + + 0.0000000 0.0000000 + 0.0126100 -.0102700 + 0.0251100 -.0103300 + 0.0500800 -.0079700 + 0.0750600 -.0058000 + 0.1000400 -.0036400 + 0.1500100 -.0010100 + 0.1999900 0.0005200 + 0.2999900 0.0005800 + 0.4000000 0.0000400 + 0.5000000 0.0000000 + 0.6000000 0.0002600 + 0.6999900 0.0005200 + 0.8000100 -.0005200 + 0.9000100 -.0005600 + 0.9500100 -.0005300 + 1.0000000 0.0000000 diff --git a/airfoil/data/goe316.dat b/airfoil/data/goe316.dat new file mode 100644 index 0000000..8e3d543 --- /dev/null +++ b/airfoil/data/goe316.dat @@ -0,0 +1,38 @@ +GOE 316 (HANSA-BRANDENBURG IV.5) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0123000 0.0210200 + 0.0247100 0.0308300 + 0.0495800 0.0443700 + 0.0744700 0.0556100 + 0.0993900 0.0642400 + 0.1492700 0.0769200 + 0.1991900 0.0852900 + 0.2991700 0.0878400 + 0.3992000 0.0839900 + 0.4992900 0.0749400 + 0.5994000 0.0626900 + 0.6995500 0.0472500 + 0.7997000 0.0319000 + 0.8998400 0.0170500 + 0.9499100 0.0092200 + 1.0000000 0.0021000 + + 0.0000000 0.0000000 + 0.0126100 -.0104800 + 0.0251000 -.0114500 + 0.0500900 -.0090200 + 0.0750600 -.0072800 + 0.1000500 -.0056500 + 0.1500300 -.0036700 + 0.2000300 -.0032000 + 0.3000300 -.0029500 + 0.4000200 -.0025000 + 0.5000300 -.0026500 + 0.6000300 -.0027000 + 0.7000300 -.0028500 + 0.8000300 -.0029000 + 0.9000200 -.0025500 + 0.9500200 -.0025700 + 1.0000000 -.0021000 diff --git a/airfoil/data/goe318.dat b/airfoil/data/goe318.dat new file mode 100644 index 0000000..00ef3b9 --- /dev/null +++ b/airfoil/data/goe318.dat @@ -0,0 +1,38 @@ +GOE 318 (HANSA-BRANDENBURG VI.5) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0122900 0.0195300 + 0.0246900 0.0290600 + 0.0495400 0.0431300 + 0.0744200 0.0544900 + 0.0993300 0.0634500 + 0.1491800 0.0773800 + 0.1991100 0.0840100 + 0.2990600 0.0888700 + 0.3990900 0.0855300 + 0.4992000 0.0755900 + 0.5993600 0.0600500 + 0.6995500 0.0429200 + 0.7997200 0.0262800 + 0.8998700 0.0125400 + 0.9499300 0.0068700 + 1.0000000 0.0020000 + + 0.0000000 0.0000000 + 0.0126300 -.0108700 + 0.0251300 -.0123300 + 0.0501200 -.0117700 + 0.0751200 -.0112000 + 0.1001100 -.0098900 + 0.1500800 -.0071100 + 0.2000500 -.0049800 + 0.3000300 -.0024200 + 0.4000200 -.0017600 + 0.5000200 -.0018000 + 0.6000200 -.0018400 + 0.7000300 -.0023800 + 0.8000300 -.0030200 + 0.9000300 -.0024600 + 0.9500300 -.0025300 + 1.0000000 -.0020000 diff --git a/airfoil/data/goe319.dat b/airfoil/data/goe319.dat new file mode 100644 index 0000000..f448576 --- /dev/null +++ b/airfoil/data/goe319.dat @@ -0,0 +1,38 @@ +GOE 319 (HANSA-BRANDENBURG II) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0120600 0.0306700 + 0.0243700 0.0438500 + 0.0491100 0.0617100 + 0.0739200 0.0745700 + 0.0987900 0.0839300 + 0.1486000 0.0967500 + 0.1985100 0.1033700 + 0.2984300 0.1088100 + 0.3984600 0.1065600 + 0.4986000 0.0968000 + 0.5988100 0.0823500 + 0.6990800 0.0637000 + 0.7993600 0.0439500 + 0.8996800 0.0220000 + 0.9498400 0.0113300 + 1.0000000 0.0005500 + + 0.0000000 0.0000000 + 0.0127000 -.0139200 + 0.0252100 -.0146400 + 0.0501800 -.0127700 + 0.0751400 -.0099100 + 0.1001000 -.0069500 + 0.1500300 -.0023300 + 0.1999700 0.0022900 + 0.2999100 0.0063300 + 0.3999100 0.0062800 + 0.4999300 0.0047200 + 0.5999400 0.0041700 + 0.6999600 0.0026100 + 0.7999800 0.0014600 + 0.9000100 -.0008900 + 0.9500200 -.0012700 + 1.0000000 -.0005500 diff --git a/airfoil/data/goe320.dat b/airfoil/data/goe320.dat new file mode 100644 index 0000000..2ce09f5 --- /dev/null +++ b/airfoil/data/goe320.dat @@ -0,0 +1,38 @@ +GOE 320 (HANSA-BRANDENBURG II.1) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0119100 0.0319200 + 0.0241400 0.0462500 + 0.0487200 0.0689000 + 0.0734200 0.0849600 + 0.0982000 0.0970200 + 0.1479500 0.1106400 + 0.1977900 0.1189700 + 0.2977100 0.1235200 + 0.3977400 0.1215800 + 0.4978900 0.1139400 + 0.5981900 0.0978000 + 0.6985800 0.0764600 + 0.7990400 0.0518200 + 0.8995000 0.0271900 + 0.9497300 0.0146200 + 1.0000000 0.0026500 + + 0.0000000 0.0000000 + 0.0128700 -.0188600 + 0.0253800 -.0207300 + 0.0503500 -.0187700 + 0.0752900 -.0158000 + 0.1002300 -.0126400 + 0.1501300 -.0068200 + 0.2000600 -.0034900 + 0.3000000 0.0002600 + 0.3999800 0.0012200 + 0.4999800 0.0012700 + 0.5999900 0.0005300 + 0.7000100 -.0003100 + 0.8000200 -.0010600 + 0.9000400 -.0020000 + 0.9500500 -.0025800 + 1.0000000 -.0026500 diff --git a/airfoil/data/goe321.dat b/airfoil/data/goe321.dat new file mode 100644 index 0000000..251d454 --- /dev/null +++ b/airfoil/data/goe321.dat @@ -0,0 +1,38 @@ +GOE 321 (HANSA-BRANDENBURG III.1) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0121400 0.0256700 + 0.0244800 0.0378400 + 0.0492200 0.0559800 + 0.0740400 0.0695300 + 0.0988900 0.0800700 + 0.1487200 0.0924600 + 0.1986100 0.1004500 + 0.2985100 0.1072300 + 0.3985400 0.1055200 + 0.4987000 0.0941100 + 0.5989100 0.0784900 + 0.6991900 0.0585800 + 0.7994500 0.0397700 + 0.8997100 0.0209600 + 0.9498500 0.0109600 + 1.0000000 0.0021500 + + 0.0000000 0.0000000 + 0.0127000 -.0137200 + 0.0252200 -.0156500 + 0.0502100 -.0148000 + 0.0751800 -.0128600 + 0.1001500 -.0111100 + 0.1501200 -.0086200 + 0.2000900 -.0067300 + 0.3000600 -.0043400 + 0.4000500 -.0036600 + 0.5000700 -.0047700 + 0.6000700 -.0051900 + 0.7000700 -.0047000 + 0.8000500 -.0038200 + 0.9000500 -.0035300 + 0.9500400 -.0028400 + 1.0000000 -.0021500 diff --git a/airfoil/data/goe322.dat b/airfoil/data/goe322.dat new file mode 100644 index 0000000..cf5b5ea --- /dev/null +++ b/airfoil/data/goe322.dat @@ -0,0 +1,38 @@ +GOE 322 (HANSA-BRANDENBURG IV.1) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0121400 0.0246800 + 0.0244300 0.0395500 + 0.0491100 0.0612100 + 0.0738700 0.0778700 + 0.0986800 0.0909300 + 0.1484500 0.1071500 + 0.1983000 0.1173800 + 0.2981800 0.1255200 + 0.3982100 0.1234700 + 0.4983700 0.1122300 + 0.5986300 0.0941800 + 0.6989800 0.0706400 + 0.7993100 0.0474900 + 0.8996300 0.0257400 + 0.9497899 0.0142700 + 1.0000000 0.0030000 + + 0.0000000 0.0000000 + 0.0127000 -.0138200 + 0.0252300 -.0158300 + 0.0502400 -.0167700 + 0.0752200 -.0154100 + 0.1002000 -.0140500 + 0.1501500 -.0103200 + 0.2001200 -.0081000 + 0.3000700 -.0051500 + 0.4000600 -.0042000 + 0.5000600 -.0041500 + 0.6000600 -.0038000 + 0.7000600 -.0038500 + 0.8000500 -.0034000 + 0.9000500 -.0033500 + 0.9500500 -.0036200 + 1.0000000 -.0030000 diff --git a/airfoil/data/goe323.dat b/airfoil/data/goe323.dat new file mode 100644 index 0000000..05c43be --- /dev/null +++ b/airfoil/data/goe323.dat @@ -0,0 +1,38 @@ +GOE 323 (HANSA-BRANDENBURG V.1) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0120800 0.0256000 + 0.0243700 0.0385000 + 0.0509900 0.0584600 + 0.0738600 0.0698100 + 0.0986900 0.0799100 + 0.1484700 0.0934300 + 0.1983400 0.1013400 + 0.2982500 0.1069800 + 0.3983100 0.1034100 + 0.4985300 0.0896500 + 0.5988500 0.0700900 + 0.6991900 0.0495300 + 0.7994700 0.0321700 + 0.8997500 0.0153100 + 0.9498700 0.0081300 + 1.0000000 0.0005500 + + 0.0000000 0.0000000 + 0.0127400 -.0145900 + 0.0252700 -.0164900 + 0.0502400 -.0149800 + 0.0752200 -.0135700 + 0.1002000 -.0120600 + 0.1501500 -.0091500 + 0.2001000 -.0062300 + 0.3000600 -.0034900 + 0.4000500 -.0029600 + 0.5000600 -.0034200 + 0.6000600 -.0033900 + 0.7000500 -.0033500 + 0.8000400 -.0027200 + 0.9000300 -.0016800 + 0.9500200 -.0013700 + 1.0000000 -.0005500 diff --git a/airfoil/data/goe324.dat b/airfoil/data/goe324.dat new file mode 100644 index 0000000..58879d0 --- /dev/null +++ b/airfoil/data/goe324.dat @@ -0,0 +1,38 @@ +GOE 324 (HANSA-BRANDENBURG) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0119800 0.0322000 + 0.0242600 0.0452000 + 0.0489400 0.0651000 + 0.0737200 0.0787000 + 0.0985200 0.0905100 + 0.1482500 0.1072200 + 0.1980900 0.1171300 + 0.2979600 0.1251600 + 0.3980600 0.1192900 + 0.4983000 0.1044200 + 0.5986500 0.0826600 + 0.6990400 0.0587900 + 0.7994000 0.0365300 + 0.8997200 0.0173700 + 0.9498600 0.0085800 + 1.0000000 0.0012000 + + 0.0000000 0.0000000 + 0.0127600 -.0161900 + 0.0252800 -.0170900 + 0.0502500 -.0155800 + 0.0752400 -.0142300 + 0.1002100 -.0130000 + 0.1501700 -.0102500 + 0.2001400 -.0084400 + 0.3001000 -.0062100 + 0.4000700 -.0045800 + 0.5000700 -.0040500 + 0.6000700 -.0040200 + 0.7000700 -.0044900 + 0.8000600 -.0039600 + 0.9000500 -.0028300 + 0.9500300 -.0020100 + 1.0000000 -.0012000 diff --git a/airfoil/data/goe325.dat b/airfoil/data/goe325.dat new file mode 100644 index 0000000..92c9920 --- /dev/null +++ b/airfoil/data/goe325.dat @@ -0,0 +1,38 @@ +GOE 325 (PFALZ 54) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0125000 0.0181100 + 0.0250000 0.0282200 + 0.0500000 0.0424500 + 0.0750000 0.0536700 + 0.1000000 0.0629000 + 0.1500000 0.0763500 + 0.2000000 0.0838000 + 0.3000000 0.0877000 + 0.4000000 0.0846000 + 0.5000000 0.0765000 + 0.6000000 0.0674000 + 0.7000000 0.0553000 + 0.8000000 0.0412000 + 0.9000000 0.0231000 + 0.9500000 0.0125500 + 1.0000000 0.0030000 + + 0.0000000 0.0000000 + 0.0125000 -.0088900 + 0.0250000 -.0097800 + 0.0500000 -.0085500 + 0.0750000 -.0063200 + 0.1000000 -.0041000 + 0.1500000 -.0006500 + 0.2000000 0.0018000 + 0.3000000 0.0057000 + 0.4000000 0.0076000 + 0.5000000 0.0080000 + 0.6000000 0.0074000 + 0.7000000 0.0063000 + 0.8000000 0.0047000 + 0.9000000 0.0026000 + 0.9500000 0.0015500 + 1.0000000 0.0000000 diff --git a/airfoil/data/goe326.dat b/airfoil/data/goe326.dat new file mode 100644 index 0000000..1891359 --- /dev/null +++ b/airfoil/data/goe326.dat @@ -0,0 +1,38 @@ +GOE 326 (PFALZ 55) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0132100 0.0197000 + 0.0247300 0.0295300 + 0.0496100 0.0440000 + 0.0745100 0.0538800 + 0.0994400 0.0613000 + 0.1493300 0.0736600 + 0.1992700 0.0815000 + 0.2992000 0.0877200 + 0.3992200 0.0860300 + 0.4992800 0.0789400 + 0.5993700 0.0690500 + 0.6995100 0.0541700 + 0.7996500 0.0380800 + 0.8998200 0.0198900 + 0.9499000 0.0112400 + 1.0000000 0.0015000 + + 0.0000000 0.0000000 + 0.0125900 -.0094000 + 0.0250900 -.0106000 + 0.0500800 -.0085400 + 0.0750600 -.0064200 + 0.1000400 -.0046900 + 0.1500200 -.0012300 + 0.1999800 0.0018200 + 0.2999500 0.0059300 + 0.3999200 0.0084400 + 0.4999200 0.0088500 + 0.5999300 0.0073600 + 0.6999500 0.0053700 + 0.7999800 0.0024800 + 0.9000000 0.0000900 + 0.9500100 -.0009500 + 1.0000000 -.0015000 diff --git a/airfoil/data/goe328.dat b/airfoil/data/goe328.dat new file mode 100644 index 0000000..9e72ae2 --- /dev/null +++ b/airfoil/data/goe328.dat @@ -0,0 +1,38 @@ +GOE 328 AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0125000 0.0171900 + 0.0250000 0.0253700 + 0.0500000 0.0377500 + 0.0750000 0.0481300 + 0.1000000 0.0565000 + 0.1500000 0.0702500 + 0.2000000 0.0780000 + 0.3000000 0.0845000 + 0.4000000 0.0830000 + 0.5000000 0.0775000 + 0.6000000 0.0670000 + 0.7000000 0.0535000 + 0.8000000 0.0380000 + 0.9000000 0.0215000 + 0.9500000 0.0132500 + 1.0000000 0.0050000 + + 0.0000000 0.0000000 + 0.0125000 -.0138100 + 0.0250000 -.0146200 + 0.0500000 -.0122500 + 0.0750000 -.0098800 + 0.1000000 -.0075000 + 0.1500000 -.0037500 + 0.2000000 -.0010000 + 0.3000000 0.0025000 + 0.4000000 0.0040000 + 0.5000000 0.0045000 + 0.6000000 0.0040000 + 0.7000000 0.0030000 + 0.8000000 0.0020000 + 0.9000000 0.0010000 + 0.9500000 0.0007500 + 1.0000000 0.0000000 diff --git a/airfoil/data/goe329.dat b/airfoil/data/goe329.dat new file mode 100644 index 0000000..4e2b1ce --- /dev/null +++ b/airfoil/data/goe329.dat @@ -0,0 +1,38 @@ +GOE 329 (PFALZ 58) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0123000 0.0203200 + 0.0247000 0.0304400 + 0.0495400 0.0466900 + 0.0744200 0.0592300 + 0.0993100 0.0701700 + 0.1491500 0.0870600 + 0.1990400 0.0979500 + 0.2989600 0.1061300 + 0.3989800 0.1039100 + 0.4990600 0.0963900 + 0.5991700 0.0847700 + 0.6993300 0.0685500 + 0.7995300 0.0482400 + 0.8997400 0.0263200 + 0.9498500 0.0151100 + 1.0000000 0.0030000 + + 0.0000000 0.0000000 + 0.0126200 -.0126800 + 0.0251200 -.0120500 + 0.0500900 -.0096100 + 0.0750700 -.0072600 + 0.1000500 -.0055200 + 0.1500200 -.0020300 + 0.1999900 0.0011600 + 0.2999600 0.0045400 + 0.3999400 0.0056200 + 0.4999400 0.0058000 + 0.5999500 0.0047800 + 0.6999700 0.0030600 + 0.7999800 0.0019400 + 0.9000000 0.0002200 + 0.9500100 -.0007900 + 1.0000000 -.0030000 diff --git a/airfoil/data/goe330.dat b/airfoil/data/goe330.dat new file mode 100644 index 0000000..867bc12 --- /dev/null +++ b/airfoil/data/goe330.dat @@ -0,0 +1,38 @@ +GOE 330 (PFALZ 59) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0122600 0.0206400 + 0.0246400 0.0312800 + 0.0494400 0.0490700 + 0.0742800 0.0623500 + 0.0991500 0.0735400 + 0.1489900 0.0882100 + 0.1988700 0.0984900 + 0.2987600 0.1074400 + 0.3987700 0.1065900 + 0.4988400 0.1009400 + 0.5989800 0.0888900 + 0.6991500 0.0735400 + 0.7994000 0.0521900 + 0.8996700 0.0283500 + 0.9498300 0.0149200 + 1.0000000 0.0005000 + + 0.0000000 0.0000000 + 0.0126200 -.0106500 + 0.0251300 -.0117100 + 0.0501200 -.0107200 + 0.0750900 -.0076400 + 0.1000700 -.0058500 + 0.1500300 -.0022700 + 0.2000000 0.0003000 + 0.2999400 0.0054500 + 0.3999000 0.0086000 + 0.4998800 0.0107500 + 0.5998700 0.0109000 + 0.6999000 0.0090500 + 0.7999300 0.0062000 + 0.9000000 0.0003500 + 0.9500000 -.0000700 + 1.0000000 -.0005000 diff --git a/airfoil/data/goe331.dat b/airfoil/data/goe331.dat new file mode 100644 index 0000000..b1d8376 --- /dev/null +++ b/airfoil/data/goe331.dat @@ -0,0 +1,38 @@ +GOE 331 (PFALZ 60) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0122100 0.0301200 + 0.0245900 0.0424400 + 0.0494100 0.0612800 + 0.0742600 0.0758200 + 0.0991600 0.0869600 + 0.1489900 0.1037500 + 0.1989000 0.1137300 + 0.2988200 0.1212000 + 0.3988200 0.1215700 + 0.4988900 0.1145400 + 0.5990200 0.1012100 + 0.6992100 0.0815800 + 0.7994400 0.0579500 + 0.8996900 0.0322300 + 0.9498400 0.0168100 + 1.0000000 0.0013000 + + 0.0000000 0.0000000 + 0.0126100 -.0108800 + 0.0250800 -.0086600 + 0.0500400 -.0041100 + 0.0750000 -.0001700 + 0.0999700 0.0029700 + 0.1499200 0.0080500 + 0.1998900 0.0114400 + 0.2998600 0.0148100 + 0.3998500 0.0157800 + 0.4998500 0.0151500 + 0.5998700 0.0134200 + 0.6999000 0.0101900 + 0.7999300 0.0068600 + 0.8999700 0.0030300 + 0.9499900 0.0009100 + 1.0000000 -.0013000 diff --git a/airfoil/data/goe332.dat b/airfoil/data/goe332.dat new file mode 100644 index 0000000..9282117 --- /dev/null +++ b/airfoil/data/goe332.dat @@ -0,0 +1,38 @@ +GOE 332 (PFALZ 61) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0121300 0.0241900 + 0.0244400 0.0358800 + 0.0491500 0.0547600 + 0.0739400 0.0681500 + 0.0987700 0.0795300 + 0.1485100 0.0963000 + 0.1983200 0.1080700 + 0.2981400 0.1198200 + 0.3981200 0.1211700 + 0.4982300 0.1142200 + 0.5984500 0.0997800 + 0.6987500 0.0808300 + 0.7991000 0.0581900 + 0.8994700 0.0339400 + 0.9496900 0.0197200 + 1.0000000 0.0015000 + + 0.0000000 0.0000000 + 0.0127300 -.0140000 + 0.0252500 -.0161100 + 0.0502500 -.0162200 + 0.0752400 -.0153300 + 0.1002000 -.0130500 + 0.1501200 -.0074700 + 0.2000500 -.0034000 + 0.2999700 0.0020500 + 0.3999000 0.0062000 + 0.4998800 0.0074500 + 0.5998800 0.0075000 + 0.6998800 0.0074500 + 0.7999200 0.0054000 + 0.8999700 0.0019500 + 0.9499900 0.0007200 + 1.0000000 -.0015000 diff --git a/airfoil/data/goe335.dat b/airfoil/data/goe335.dat new file mode 100644 index 0000000..32807cd --- /dev/null +++ b/airfoil/data/goe335.dat @@ -0,0 +1,38 @@ +GOE 335 (D.F.W.) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0125000 0.0160900 + 0.0250000 0.0251900 + 0.0500000 0.0383800 + 0.0750000 0.0480600 + 0.1000000 0.0567500 + 0.1500000 0.0686300 + 0.2000000 0.0765000 + 0.3000000 0.0812500 + 0.4000000 0.0790000 + 0.5000000 0.0737500 + 0.6000000 0.0640000 + 0.7000000 0.0507500 + 0.8000000 0.0355000 + 0.9000000 0.0202500 + 0.9500000 0.0106300 + 1.0000000 0.0000000 + + 0.0000000 0.0000000 + 0.0125000 -.0069100 + 0.0250000 -.0073100 + 0.0500000 -.0056300 + 0.0750000 -.0034400 + 0.1000000 -.0007500 + 0.1500000 0.0041200 + 0.2000000 0.0080000 + 0.3000000 0.0142500 + 0.4000000 0.0170000 + 0.5000000 0.0162500 + 0.6000000 0.0140000 + 0.7000000 0.0107500 + 0.8000000 0.0070000 + 0.9000000 0.0037500 + 0.9500000 0.0021300 + 1.0000000 0.0000000 diff --git a/airfoil/data/goe336.dat b/airfoil/data/goe336.dat new file mode 100644 index 0000000..b6518c6 --- /dev/null +++ b/airfoil/data/goe336.dat @@ -0,0 +1,38 @@ +GOE 336 (MVA H.44) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0123800 0.0195700 + 0.0247900 0.0326500 + 0.0497200 0.0473000 + 0.0746500 0.0589500 + 0.0996000 0.0673000 + 0.1495200 0.0802000 + 0.1994700 0.0887000 + 0.2994100 0.0988000 + 0.3994200 0.0967000 + 0.4994800 0.0875000 + 0.5995500 0.0743000 + 0.6996601 0.0578000 + 0.7997500 0.0413000 + 0.8998600 0.0226000 + 0.9499300 0.0125000 + 1.0000000 0.0015000 + + 0.0000000 0.0000000 + 0.0125700 -.0110200 + 0.0250700 -.0123500 + 0.0500700 -.0122000 + 0.0750600 -.0097500 + 0.1000400 -.0064000 + 0.1500000 -.0008000 + 0.1999800 0.0037000 + 0.2999400 0.0093000 + 0.3999400 0.0094000 + 0.4999600 0.0059000 + 0.5999900 0.0011000 + 0.7000200 -.0033000 + 0.8000400 -.0072000 + 0.9000400 -.0071000 + 0.9500300 -.0058000 + 1.0000000 -.0015000 diff --git a/airfoil/data/goe342.dat b/airfoil/data/goe342.dat new file mode 100644 index 0000000..11e17cd --- /dev/null +++ b/airfoil/data/goe342.dat @@ -0,0 +1,36 @@ +GOE 342 AIRFOIL + 16. 16. + + 0.0000000 0.0000000 + 0.0125000 0.0201000 + 0.0250000 0.0292000 + 0.0500000 0.0414000 + 0.0750000 0.0506000 + 0.1000000 0.0578000 + 0.1500000 0.0702000 + 0.2000000 0.0786000 + 0.3000000 0.0854000 + 0.4000000 0.0872000 + 0.5000000 0.0850000 + 0.6000000 0.0778000 + 0.7000000 0.0636000 + 0.8000000 0.0464000 + 0.9000000 0.0262000 + 1.0000000 0.0030000 + + 0.0000000 0.0000000 + 0.0125000 -.0079000 + 0.0250000 -.0058000 + 0.0500000 0.0004000 + 0.0750000 0.0046000 + 0.1000000 0.0098000 + 0.1500000 0.0177000 + 0.2000000 0.0246000 + 0.3000000 0.0334000 + 0.4000000 0.0372000 + 0.5000000 0.0375000 + 0.6000000 0.0358000 + 0.7000000 0.0306000 + 0.8000000 0.0224000 + 0.9000000 0.0122000 + 1.0000000 0.0000000 diff --git a/airfoil/data/goe344.dat b/airfoil/data/goe344.dat new file mode 100644 index 0000000..27bfd75 --- /dev/null +++ b/airfoil/data/goe344.dat @@ -0,0 +1,38 @@ +GOE 344 (PFALZ 71) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0123400 0.0177100 + 0.0247700 0.0253200 + 0.0496900 0.0351400 + 0.0746200 0.0422700 + 0.0995800 0.0477900 + 0.1495200 0.0551400 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--git a/airfoil/data/goe675.dat b/airfoil/data/goe675.dat new file mode 100644 index 0000000..3df8b27 --- /dev/null +++ b/airfoil/data/goe675.dat @@ -0,0 +1,38 @@ +GOE 675 AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0114100 0.0314000 + 0.0235100 0.0428200 + 0.0478600 0.0616600 + 0.0723600 0.0760100 + 0.0969500 0.0878700 + 0.1463300 0.1055900 + 0.1959100 0.1178100 + 0.2954900 0.1297700 + 0.3954700 0.1302400 + 0.4956700 0.1247200 + 0.5961000 0.1122100 + 0.6967800 0.0927100 + 0.7977000 0.0662200 + 0.8987900 0.0347300 + 0.9493600 0.0184900 + 1.0000000 0.0017500 + + 0.0000000 0.0000000 + 0.0132000 -.0200400 + 0.0259100 -.0261000 + 0.0511200 -.0322200 + 0.0761600 -.0333500 + 0.1011500 -.0329900 + 0.1510500 -.0302500 + 0.2009400 -.0270200 + 0.3006600 -.0190500 + 0.4004400 -.0125800 + 0.5002600 -.0076200 + 0.6001400 -.0041400 + 0.7000800 -.0021700 + 0.8000400 -.0012000 + 0.9000400 -.0012200 + 0.9500500 -.0014900 + 1.0000000 -.0017500 diff --git a/airfoil/data/goe676.dat b/airfoil/data/goe676.dat new file mode 100644 index 0000000..8ec201c --- /dev/null +++ b/airfoil/data/goe676.dat @@ -0,0 +1,38 @@ +GOE 676 (= M 12) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0125000 0.0186200 + 0.0250000 0.0270400 + 0.0500000 0.0395700 + 0.0750000 0.0486100 + 0.1000000 0.0551500 + 0.1500000 0.0662200 + 0.2000000 0.0738000 + 0.3000000 0.0799500 + 0.4000000 0.0791000 + 0.5000000 0.0732500 + 0.6000000 0.0629000 + 0.7000000 0.0505500 + 0.8000000 0.0352000 + 0.9000000 0.0193500 + 0.9500000 0.0109200 + 1.0000000 0.0030000 + + 0.0000000 0.0000000 + 0.0125000 -.0159800 + 0.0250000 -.0214600 + 0.0500000 -.0269300 + 0.0750000 -.0298900 + 0.1000000 -.0323500 + 0.1500000 -.0347700 + 0.2000000 -.0367000 + 0.3000000 -.0390500 + 0.4000000 -.0389000 + 0.5000000 -.0367500 + 0.6000000 -.0336000 + 0.7000000 -.0284500 + 0.8000000 -.0213000 + 0.9000000 -.0111500 + 0.9500000 -.0055800 + 1.0000000 0.0000000 diff --git a/airfoil/data/goe677.dat b/airfoil/data/goe677.dat new file mode 100644 index 0000000..4209c4e --- /dev/null +++ b/airfoil/data/goe677.dat @@ -0,0 +1,38 @@ +GOE 677 (= M 6) AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0125000 0.0180300 + 0.0250000 0.0275500 + 0.0500000 0.0406000 + 0.0750000 0.0491500 + 0.1000000 0.0567000 + 0.1500000 0.0678000 + 0.2000000 0.0754000 + 0.3000000 0.0826000 + 0.4000000 0.0808000 + 0.5000000 0.0745000 + 0.6000000 0.0617000 + 0.7000000 0.0474000 + 0.8000000 0.0331000 + 0.9000000 0.0183000 + 0.9500000 0.0114000 + 1.0000000 0.0040000 + + 0.0000000 0.0000000 + 0.0125000 -.0169700 + 0.0250000 -.0224500 + 0.0500000 -.0274000 + 0.0750000 -.0298500 + 0.1000000 -.0318000 + 0.1500000 -.0337000 + 0.2000000 -.0356000 + 0.3000000 -.0369000 + 0.4000000 -.0377000 + 0.5000000 -.0370000 + 0.6000000 -.0358000 + 0.7000000 -.0321000 + 0.8000000 -.0259000 + 0.9000000 -.0147000 + 0.9500000 -.0076000 + 1.0000000 0.0000000 diff --git a/airfoil/data/goe679.dat b/airfoil/data/goe679.dat new file mode 100644 index 0000000..1a5c48f --- /dev/null +++ b/airfoil/data/goe679.dat @@ -0,0 +1,38 @@ +GOE 679 AIRFOIL + 17. 17. + + 0.0000100 0.0000000 + 0.0103800 0.0312100 + 0.0218100 0.0469800 + 0.0452400 0.0700800 + 0.0691800 0.0857000 + 0.0933200 0.0983400 + 0.1421400 0.1156600 + 0.1914400 0.1260200 + 0.2908400 0.1347800 + 0.3910200 0.1320900 + 0.4916400 0.1229300 + 0.5926000 0.1088000 + 0.6939400 0.0891900 + 0.7955101 0.0660900 + 0.8973500 0.0390200 + 0.9484000 0.0214900 + 1.0000000 0.0000000 + + 0.0000100 0.0000000 + 0.0142800 -.0260300 + 0.0272900 -.0336400 + 0.0529200 -.0429000 + 0.0783100 -.0486700 + 0.1035400 -.0519600 + 0.1536800 -.0540500 + 0.2036200 -.0531500 + 0.3032300 -.0473800 + 0.4027600 -.0406100 + 0.5023000 -.0338400 + 0.6018400 -.0270700 + 0.7013800 -.0203100 + 0.8009200 -.0135400 + 0.9004600 -.0067700 + 0.9502300 -.0033800 + 1.0000000 0.0000000 diff --git a/airfoil/data/goe681.dat b/airfoil/data/goe681.dat new file mode 100644 index 0000000..e968d5d --- /dev/null +++ b/airfoil/data/goe681.dat @@ -0,0 +1,38 @@ +GOE 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+++ b/airfoil/data/m1.dat @@ -0,0 +1,38 @@ +NACA-M1 AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0125000 0.0103000 + 0.0250000 0.0136000 + 0.0500000 0.0180000 + 0.0750000 0.0210000 + 0.1000000 0.0234000 + 0.1500000 0.0267000 + 0.2000000 0.0288000 + 0.3000000 0.0308000 + 0.4000000 0.0305000 + 0.5000000 0.0285000 + 0.6000000 0.0253000 + 0.7000000 0.0208000 + 0.8000000 0.0154000 + 0.9000000 0.0091000 + 0.9500000 0.0057000 + 1.0000000 0.0020000 + + 0.0000000 0.0000000 + 0.0125000 -.0103000 + 0.0250000 -.0136000 + 0.0500000 -.0180000 + 0.0750000 -.0210000 + 0.1000000 -.0234000 + 0.1500000 -.0267000 + 0.2000000 -.0288000 + 0.3000000 -.0308000 + 0.4000000 -.0305000 + 0.5000000 -.0285000 + 0.6000000 -.0253000 + 0.7000000 -.0208000 + 0.8000000 -.0154000 + 0.9000000 -.0091000 + 0.9500000 -.0057000 + 1.0000000 -.0020000 diff --git a/airfoil/data/m10.dat b/airfoil/data/m10.dat new file mode 100644 index 0000000..16d594f --- /dev/null +++ b/airfoil/data/m10.dat @@ -0,0 +1,38 @@ +NACA M10 AIRFOIL + 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0.0133000 + 0.6000000 0.0058000 + 0.7000000 -.0012000 + 0.8000000 -.0055000 + 0.9000000 -.0056000 + 0.9500000 -.0036000 + 1.0000000 0.0000000 diff --git a/airfoil/data/m21.dat b/airfoil/data/m21.dat new file mode 100644 index 0000000..7edd17a --- /dev/null +++ b/airfoil/data/m21.dat @@ -0,0 +1,38 @@ +NACA M21 AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0125000 0.0221000 + 0.0250000 0.0336000 + 0.0500000 0.0518000 + 0.0750000 0.0662000 + 0.1000000 0.0782000 + 0.1500000 0.0965000 + 0.2000000 0.1090000 + 0.3000000 0.1202000 + 0.4000000 0.1178000 + 0.5000000 0.1055000 + 0.6000000 0.0868000 + 0.7000000 0.0649000 + 0.8000000 0.0421000 + 0.9000000 0.0202000 + 0.9500000 0.0105000 + 1.0000000 0.0024000 + + 0.0000000 0.0000000 + 0.0125000 -.0151000 + 0.0250000 -.0186000 + 0.0500000 -.0185000 + 0.0750000 -.0149700 + 0.1000000 -.0113000 + 0.1500000 -.0065000 + 0.2000000 -.0026000 + 0.3000000 0.0007000 + 0.4000000 -.0011000 + 0.5000000 -.0057000 + 0.6000000 -.0114000 + 0.7000000 -.0156000 + 0.8000000 -.0165000 + 0.9000000 -.0127000 + 0.9500000 -.0087000 + 1.0000000 -.0024000 diff --git a/airfoil/data/m22.dat b/airfoil/data/m22.dat new file mode 100644 index 0000000..09039e7 --- /dev/null +++ b/airfoil/data/m22.dat @@ -0,0 +1,38 @@ +NACA M22 AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0125500 0.0138600 + 0.0250800 0.0225200 + 0.0501200 0.0371300 + 0.0751600 0.0485500 + 0.1002000 0.0590600 + 0.1502500 0.0745000 + 0.2002900 0.0852300 + 0.3003200 0.0942900 + 0.4003000 0.0908600 + 0.5002600 0.0786200 + 0.6002100 0.0613900 + 0.7001400 0.0418500 + 0.8000801 0.0237200 + 0.9000300 0.0094800 + 0.9500200 0.0049200 + 1.0000000 0.0026500 + + 0.0000000 0.0000000 + 0.0124800 -.0070400 + 0.0249800 -.0050800 + 0.0500000 0.0005300 + 0.0750200 0.0063500 + 0.1000400 0.0116600 + 0.1500700 0.0207000 + 0.2000900 0.0269300 + 0.3001100 0.0317900 + 0.4001000 0.0287600 + 0.5000700 0.0199200 + 0.6000300 0.0092900 + 0.7000000 -.0011400 + 0.7999700 -.0082800 + 0.8999700 -.0096100 + 0.9499800 -.0070800 + 1.0000000 -.0026500 diff --git a/airfoil/data/m23.dat b/airfoil/data/m23.dat new file mode 100644 index 0000000..c2de593 --- /dev/null +++ b/airfoil/data/m23.dat @@ -0,0 +1,38 @@ +NACA M23 AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0125900 0.0172300 + 0.0251400 0.0274700 + 0.0502300 0.0433400 + 0.0752900 0.0560100 + 0.1003500 0.0667800 + 0.1504300 0.0833200 + 0.2004900 0.0946600 + 0.3005400 0.1045400 + 0.4005300 0.1011200 + 0.5004600 0.0882000 + 0.6003600 0.0695800 + 0.7002500 0.0484600 + 0.8001500 0.0280400 + 0.9000599 0.0119200 + 0.9500300 0.0061600 + 1.0000000 0.0027000 + + 0.0000000 0.0000000 + 0.0124500 -.0086600 + 0.0249600 -.0076300 + 0.0499800 -.0035600 + 0.0750100 0.0010100 + 0.1000300 0.0056800 + 0.1500700 0.0135200 + 0.2001000 0.0188600 + 0.3001200 0.0231400 + 0.4001000 0.0198200 + 0.5000600 0.0117000 + 0.6000100 0.0021800 + 0.6999600 -.0070400 + 0.7999400 -.0124600 + 0.8999400 -.0116800 + 0.9499600 -.0082400 + 1.0000000 -.0027000 diff --git a/airfoil/data/m24.dat b/airfoil/data/m24.dat new file mode 100644 index 0000000..10ed214 --- /dev/null +++ b/airfoil/data/m24.dat @@ -0,0 +1,38 @@ +NACA M24 AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0127000 0.0228900 + 0.0253000 0.0347800 + 0.0504700 0.0537600 + 0.0755900 0.0681500 + 0.1007000 0.0807300 + 0.1508600 0.0996000 + 0.2009700 0.1125600 + 0.3010700 0.1232000 + 0.4010300 0.1191300 + 0.5009100 0.1046700 + 0.6007200 0.0837000 + 0.7005200 0.0600400 + 0.8003100 0.0362800 + 0.9001400 0.0157100 + 0.9500700 0.0076800 + 1.0000000 0.0023500 + + 0.0000000 0.0000000 + 0.0123800 -.0139100 + 0.0248700 -.0151200 + 0.0498800 -.0141300 + 0.0749000 -.0116500 + 0.0999300 -.0086600 + 0.1499700 -.0032000 + 0.2000100 0.0009700 + 0.3000300 0.0037000 + 0.4000100 0.0007400 + 0.4999500 -.0060200 + 0.5998800 -.0137900 + 0.6998300 -.0197500 + 0.7998101 -.0215200 + 0.8998600 -.0164800 + 0.9499100 -.0106200 + 1.0000000 -.0023500 diff --git a/airfoil/data/m25.dat b/airfoil/data/m25.dat new file mode 100644 index 0000000..b2bb797 --- /dev/null +++ b/airfoil/data/m25.dat @@ -0,0 +1,38 @@ +NACA M25 AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0125100 0.0161000 + 0.0250100 0.0256900 + 0.0500200 0.0436800 + 0.0750200 0.0571700 + 0.1000200 0.0692600 + 0.1500300 0.0884500 + 0.2000400 0.1021300 + 0.3000400 0.1137000 + 0.4000400 0.1099600 + 0.5000300 0.0953200 + 0.6000300 0.0746900 + 0.7000200 0.0516500 + 0.8000100 0.0296200 + 0.9000000 0.0119900 + 0.9500000 0.0060700 + 1.0000000 0.0022500 + + 0.0000000 0.0000000 + 0.0125000 -.0058000 + 0.0250000 -.0022100 + 0.0500000 0.0060800 + 0.0750100 0.0147700 + 0.1000100 0.0223700 + 0.1500100 0.0346500 + 0.2000200 0.0436300 + 0.3000200 0.0510000 + 0.4000200 0.0475600 + 0.5000100 0.0367200 + 0.6000100 0.0226900 + 0.7000000 0.0084500 + 0.8000000 -.0022800 + 0.9000000 -.0070100 + 0.9500000 -.0059300 + 1.0000000 -.0022500 diff --git a/airfoil/data/m26.dat b/airfoil/data/m26.dat new file mode 100644 index 0000000..5cc46e2 --- /dev/null +++ b/airfoil/data/m26.dat @@ -0,0 +1,38 @@ +NACA M26 AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0125200 0.0177800 + 0.0250400 0.0288600 + 0.0500700 0.0483300 + 0.0750900 0.0627900 + 0.1001100 0.0757600 + 0.1501300 0.0962900 + 0.2001600 0.1102000 + 0.3001700 0.1232800 + 0.4001600 0.1214400 + 0.5001500 0.1043000 + 0.6001100 0.0820600 + 0.7000800 0.0576200 + 0.8000500 0.0338800 + 0.9000200 0.0140400 + 0.9500100 0.0070700 + 1.0000000 0.0024000 + + 0.0000000 0.0000000 + 0.0124900 -.0080200 + 0.0249900 -.0057300 + 0.0500000 0.0011300 + 0.0750100 0.0084900 + 0.1000200 0.0155600 + 0.1500400 0.0269900 + 0.2000500 0.0350200 + 0.3000600 0.0417800 + 0.4000500 0.0384400 + 0.5000400 0.0284000 + 0.6000200 0.0153600 + 0.7000000 0.0027200 + 0.7999900 -.0064200 + 0.8999900 -.0092600 + 0.9499900 -.0069300 + 1.0000000 -.0024000 diff --git a/airfoil/data/m27.dat b/airfoil/data/m27.dat new file mode 100644 index 0000000..225352f --- /dev/null +++ b/airfoil/data/m27.dat @@ -0,0 +1,38 @@ +NACA M27 AIRFOIL + 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-0.015045 +0.95 -0.00918 +1 0 diff --git a/airfoil/data/m7.dat b/airfoil/data/m7.dat new file mode 100644 index 0000000..5b863d5 --- /dev/null +++ b/airfoil/data/m7.dat @@ -0,0 +1,36 @@ +NACA M7 AIRFOIL + 16. 16. + + 0.0000000 0.0000000 + 0.0125000 0.0203300 + 0.0250000 0.0273700 + 0.0500000 0.0385400 + 0.0750000 0.0477100 + 0.1000000 0.0554800 + 0.1500000 0.0669200 + 0.2000000 0.0747600 + 0.3000000 0.0809400 + 0.4000000 0.0772200 + 0.5000000 0.0666000 + 0.6000000 0.0519800 + 0.7000000 0.0358600 + 0.8000000 0.0207400 + 0.9000000 0.0094200 + 1.0000000 0.0047000 + + 0.0000000 0.0000000 + 0.0125000 -.0001600 + 0.0250000 0.0000700 + 0.0500000 0.0025400 + 0.0750000 0.0055100 + 0.1000000 0.0075800 + 0.1500000 0.0138200 + 0.2000000 0.0171600 + 0.3000000 0.0191400 + 0.4000000 0.0153200 + 0.5000000 0.0087000 + 0.6000000 0.0005800 + 0.7000000 -.0065400 + 0.8000000 -.0105600 + 0.9000000 -.0088800 + 1.0000000 0.0000000 diff --git a/airfoil/data/m8.dat b/airfoil/data/m8.dat new file mode 100644 index 0000000..74764c5 --- /dev/null +++ b/airfoil/data/m8.dat @@ -0,0 +1,38 @@ +NACA M8 AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0125000 0.0350000 + 0.0250000 0.0506000 + 0.0500000 0.0718000 + 0.0750000 0.0875000 + 0.1000000 0.0995000 + 0.1500000 0.1139000 + 0.2000000 0.1212000 + 0.2500000 0.1250000 + 0.3000000 0.1241000 + 0.4000000 0.1157000 + 0.5000000 0.0989000 + 0.6000000 0.0782000 + 0.7000000 0.0544000 + 0.8000000 0.0331000 + 0.9000000 0.0133000 + 1.0000000 0.0000000 + + 0.0000000 0.0000000 + 0.0125000 -.0100000 + 0.0250000 -.0129000 + 0.0500000 -.0137000 + 0.0750000 -.0120000 + 0.1000000 -.0098000 + 0.1500000 -.0033000 + 0.2000000 0.0174000 + 0.2500000 0.0298000 + 0.3000000 0.0368000 + 0.4000000 0.0443000 + 0.5000000 0.0388000 + 0.6000000 0.0311000 + 0.7000000 0.0194000 + 0.8000000 0.0083000 + 0.9000000 0.0000000 + 1.0000000 0.0000000 diff --git a/airfoil/data/m9.dat b/airfoil/data/m9.dat new file mode 100644 index 0000000..a058188 --- /dev/null +++ b/airfoil/data/m9.dat @@ -0,0 +1,38 @@ +NACA M9 AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0125000 0.0312000 + 0.0250000 0.0459000 + 0.0500000 0.0639000 + 0.0750000 0.0779000 + 0.1000000 0.0885000 + 0.1500000 0.1011000 + 0.2000000 0.1075000 + 0.2500000 0.1111000 + 0.3000000 0.1110000 + 0.4000000 0.1024000 + 0.5000000 0.0878000 + 0.6000000 0.0695000 + 0.7000000 0.0484000 + 0.8000000 0.0294000 + 0.9000000 0.0122000 + 1.0000000 0.0000000 + + 0.0000000 0.0000000 + 0.0125000 -.0083000 + 0.0250000 -.0112000 + 0.0500000 -.0122000 + 0.0750000 -.0107000 + 0.1000000 -.0079000 + 0.1500000 -.0029000 + 0.2000000 0.0053000 + 0.2500000 0.0226000 + 0.3000000 0.0326000 + 0.4000000 0.0391000 + 0.5000000 0.0346000 + 0.6000000 0.0278000 + 0.7000000 0.0172000 + 0.8000000 0.0073000 + 0.9000000 0.0000000 + 1.0000000 0.0000000 diff --git a/airfoil/data/ma409.dat b/airfoil/data/ma409.dat new file mode 100644 index 0000000..d6c80d0 --- /dev/null +++ b/airfoil/data/ma409.dat @@ -0,0 +1,42 @@ +MA409 (original) + 1.00000 0.00070 + 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a/airfoil/data/marske4.dat b/airfoil/data/marske4.dat new file mode 100644 index 0000000..6557b8f --- /dev/null +++ b/airfoil/data/marske4.dat @@ -0,0 +1,38 @@ +MARSKE PIONEER IID TIP AIRFOIL (NACA 431012A*.833 HYBRID) + 17. 17. + + 0.000000 0.000000 + 0.012500 0.032400 + 0.025000 0.042800 + 0.050000 0.057700 + 0.075000 0.066900 + 0.100000 0.073100 + 0.150000 0.077700 + 0.200000 0.077300 + 0.250000 0.074600 + 0.300000 0.071400 + 0.400000 0.064200 + 0.500000 0.054700 + 0.600000 0.043300 + 0.700000 0.030800 + 0.800000 0.020300 + 0.900000 0.010400 + 1.000000 0.000000 + + 0.000000 0.000000 + 0.012500 -0.006900 + 0.025000 -0.009500 + 0.050000 -0.012800 + 0.075000 -0.015400 + 0.100000 -0.017600 + 0.150000 -0.021400 + 0.200000 -0.024600 + 0.250000 -0.027200 + 0.300000 -0.029200 + 0.400000 -0.032700 + 0.500000 -0.033600 + 0.600000 -0.032700 + 0.700000 -0.030000 + 0.800000 -0.022800 + 0.900000 -0.012500 + 1.000000 0.000000 diff --git a/airfoil/data/marske5.dat b/airfoil/data/marske5.dat new 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a/airfoil/data/mh104.dat b/airfoil/data/mh104.dat new file mode 100644 index 0000000..8e70a2a --- /dev/null +++ b/airfoil/data/mh104.dat @@ -0,0 +1,68 @@ +MH 104 15.28% + 1.00000000 0.00000000 + 0.99619582 0.00017047 + 0.98515158 0.00100213 + 0.96764209 0.00285474 + 0.94421447 0.00556001 + 0.91510964 0.00906779 + 0.88074158 0.01357364 + 0.84177999 0.01916802 + 0.79894110 0.02580144 + 0.75297076 0.03334313 + 0.70461763 0.04158593 + 0.65461515 0.05026338 + 0.60366461 0.05906756 + 0.55242353 0.06766426 + 0.50149950 0.07571157 + 0.45144530 0.08287416 + 0.40276150 0.08882939 + 0.35589801 0.09329359 + 0.31131449 0.09592864 + 0.26917194 0.09626763 + 0.22927064 0.09424396 + 0.19167283 0.09023579 + 0.15672257 0.08451656 + 0.12469599 0.07727756 + 0.09585870 0.06875796 + 0.07046974 0.05918984 + 0.04874337 0.04880096 + 0.03081405 0.03786904 + 0.01681379 0.02676332 + 0.00687971 0.01592385 + 0.00143518 0.00647946 + 0.00053606 0.00370956 + 0.00006572 0.00112514 + 0.00001249 -0.00046881 + 0.00023032 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0.82382388 -0.01917110 + 0.86219604 -0.01586085 diff --git a/airfoil/data/mh113.dat b/airfoil/data/mh113.dat new file mode 100644 index 0000000..a1132be --- /dev/null +++ b/airfoil/data/mh113.dat @@ -0,0 +1,62 @@ +MH 113 14.62% + 1.00000000 0.00000000 + 0.99657911 0.00129859 + 0.98693705 0.00520599 + 0.97212357 0.01135726 + 0.95257144 0.01898648 + 0.92829218 0.02772077 + 0.89956132 0.03753655 + 0.86691136 0.04827937 + 0.83087727 0.05966726 + 0.79197587 0.07136829 + 0.75069934 0.08303447 + 0.70752493 0.09431152 + 0.66290785 0.10483599 + 0.61722787 0.11424445 + 0.57079623 0.12228128 + 0.52396079 0.12878840 + 0.47709646 0.13364568 + 0.43058995 0.13677292 + 0.38483958 0.13811951 + 0.34024152 0.13766085 + 0.29718995 0.13539236 + 0.25604833 0.13132100 + 0.21714499 0.12549098 + 0.18077094 0.11797452 + 0.14716671 0.10890207 + 0.11656500 0.09846885 + 0.08919680 0.08689463 + 0.06526129 0.07441188 + 0.04491583 0.06128609 + 0.02828712 0.04781828 + 0.01547607 0.03434589 + 0.00654829 0.02121442 + 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0.00018251 + 1.00000000 0.00000000 diff --git a/airfoil/data/mh120.dat b/airfoil/data/mh120.dat new file mode 100644 index 0000000..2291f89 --- /dev/null +++ b/airfoil/data/mh120.dat @@ -0,0 +1,62 @@ +MH 120 11.57% + 1.00000000 0.00000000 + 0.99657719 0.00137690 + 0.98685087 0.00402821 + 0.97139506 0.00734876 + 0.95028213 0.01142090 + 0.92396594 0.01633315 + 0.89296043 0.02204560 + 0.85780483 0.02840960 + 0.81908793 0.03525874 + 0.77729819 0.04226202 + 0.73286713 0.04927267 + 0.68630523 0.05615183 + 0.63825561 0.06277069 + 0.58927764 0.06882005 + 0.53990087 0.07410860 + 0.49058966 0.07836275 + 0.44179403 0.08144146 + 0.39389925 0.08314630 + 0.34727098 0.08342625 + 0.30221961 0.08220339 + 0.25902829 0.07958612 + 0.21804994 0.07573212 + 0.17975005 0.07080805 + 0.14451023 0.06483273 + 0.11261875 0.05792996 + 0.08433629 0.05022699 + 0.05990560 0.04191067 + 0.03950438 0.03313028 + 0.02321643 0.02413907 + 0.01111339 0.01529771 + 0.00331128 0.00708273 + 0.00000653 0.00027180 + 0.00274905 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b/airfoil/data/mh20.dat @@ -0,0 +1,69 @@ +MH 20 9.01% + 1.00000000 0.00000000 + 0.99663722 -0.00000502 + 0.98661979 0.00015827 + 0.97016021 0.00083998 + 0.94762865 0.00232279 + 0.91954306 0.00478393 + 0.88649448 0.00827457 + 0.84911235 0.01276792 + 0.80805809 0.01815911 + 0.76400822 0.02428373 + 0.71763596 0.03091656 + 0.66960153 0.03779462 + 0.62054465 0.04463611 + 0.57116423 0.05108921 + 0.52197689 0.05654881 + 0.47303495 0.06058278 + 0.42440107 0.06327690 + 0.37650891 0.06484632 + 0.32990396 0.06532833 + 0.28507654 0.06470811 + 0.24245961 0.06294654 + 0.20241194 0.06004635 + 0.16525807 0.05604350 + 0.13126736 0.05103062 + 0.10070840 0.04515568 + 0.07383715 0.03858238 + 0.05087461 0.03148085 + 0.03197380 0.02406597 + 0.01728446 0.01663089 + 0.00695149 0.00951360 + 0.00230137 0.00483181 + 0.00108635 0.00304916 + 0.00030031 0.00141854 + 0.00003307 0.00043894 + 0.00003397 -0.00041277 + 0.00037497 -0.00121038 + 0.00103088 -0.00204638 + 0.00246899 -0.00334802 + 0.00439569 -0.00470397 + 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0.98651517 -0.00101933 + 0.99654701 -0.00019154 + 1.00000000 0.00000000 diff --git a/airfoil/data/mh24.dat b/airfoil/data/mh24.dat new file mode 100644 index 0000000..fe30073 --- /dev/null +++ b/airfoil/data/mh24.dat @@ -0,0 +1,69 @@ +MH 24 9.01% + 1.00000000 0.00000000 + 0.99653760 0.00038212 + 0.98634807 0.00161986 + 0.96996782 0.00405471 + 0.94809733 0.00783396 + 0.92150372 0.01284763 + 0.89093983 0.01878857 + 0.85708606 0.02507311 + 0.82017551 0.03093875 + 0.78003746 0.03611152 + 0.73686505 0.04077694 + 0.69117051 0.04497972 + 0.64343680 0.04866890 + 0.59419119 0.05183220 + 0.54398634 0.05440522 + 0.49335709 0.05634183 + 0.44284668 0.05759688 + 0.39299531 0.05814083 + 0.34433221 0.05793405 + 0.29736125 0.05695943 + 0.25256823 0.05519914 + 0.21040406 0.05265352 + 0.17128388 0.04932135 + 0.13556438 0.04523095 + 0.10356891 0.04042923 + 0.07556060 0.03498993 + 0.05176450 0.02901142 + 0.03232942 0.02263045 + 0.01738015 0.01604395 + 0.00697118 0.00951717 + 0.00187861 0.00446207 + 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index 0000000..72d8276 --- /dev/null +++ b/airfoil/data/mh25.dat @@ -0,0 +1,68 @@ +MH 25 9.98% + 1.00000000 0.00000000 + 0.99635051 0.00044823 + 0.98573137 0.00204140 + 0.96894107 0.00519871 + 0.94688038 0.00993961 + 0.92037370 0.01596838 + 0.89011954 0.02282430 + 0.85669024 0.02985118 + 0.82021659 0.03629489 + 0.78049149 0.04193268 + 0.73771056 0.04697095 + 0.69238447 0.05145822 + 0.64499206 0.05534558 + 0.59605623 0.05862203 + 0.54612430 0.06122491 + 0.49572697 0.06311117 + 0.44540326 0.06423869 + 0.39569004 0.06458276 + 0.34711360 0.06410878 + 0.30017618 0.06280648 + 0.25536234 0.06066464 + 0.21312332 0.05769242 + 0.17387529 0.05389664 + 0.13797800 0.04931573 + 0.10575823 0.04400481 + 0.07748459 0.03804852 + 0.05338824 0.03155294 + 0.03362650 0.02466585 + 0.01833367 0.01758842 + 0.00757463 0.01059496 + 0.00186535 0.00470621 + 0.00082048 0.00288211 + 0.00018458 0.00120135 + 0.00000512 0.00018681 + 0.00008206 -0.00069576 + 0.00049731 -0.00151394 + 0.00123711 -0.00236167 + 0.00281860 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0.98701228 0.00012533 + 0.99669738 0.00004969 + 1.00000000 0.00000000 diff --git a/airfoil/data/mh38.dat b/airfoil/data/mh38.dat new file mode 100644 index 0000000..133bb7f --- /dev/null +++ b/airfoil/data/mh38.dat @@ -0,0 +1,69 @@ +MH 38 9.68% + 1.00000000 0.00000000 + 0.99681503 0.00052829 + 0.98744069 0.00206411 + 0.97219660 0.00461800 + 0.95140806 0.00820800 + 0.92548959 0.01281789 + 0.89490506 0.01838273 + 0.86016416 0.02479642 + 0.82181533 0.03191761 + 0.78043788 0.03956173 + 0.73663624 0.04751042 + 0.69102740 0.05547946 + 0.64418318 0.06313426 + 0.59661875 0.07011860 + 0.54875352 0.07607236 + 0.50090364 0.08072602 + 0.45336696 0.08391210 + 0.40640999 0.08556514 + 0.36036364 0.08573940 + 0.31562154 0.08448700 + 0.27256521 0.08186533 + 0.23156049 0.07795837 + 0.19296831 0.07288249 + 0.15714479 0.06675919 + 0.12440457 0.05971034 + 0.09500846 0.05189461 + 0.06919502 0.04351376 + 0.04717790 0.03479969 + 0.02915078 0.02601488 + 0.01528686 0.01746260 + 0.00575479 0.00948521 + 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0000000..44cbda6 --- /dev/null +++ b/airfoil/data/mh42.dat @@ -0,0 +1,68 @@ +MH 42 8.94% + 1.00000000 0.00000000 + 0.99671790 0.00016926 + 0.98700940 0.00079075 + 0.97118399 0.00206867 + 0.94961088 0.00410466 + 0.92271713 0.00693938 + 0.89098323 0.01055988 + 0.85494028 0.01490369 + 0.81513644 0.01984787 + 0.77212854 0.02525776 + 0.72649451 0.03097509 + 0.67882987 0.03682941 + 0.62973821 0.04261901 + 0.57982463 0.04810928 + 0.52961801 0.05301399 + 0.47956385 0.05711715 + 0.43009344 0.06025277 + 0.38161098 0.06231306 + 0.33451717 0.06323570 + 0.28920489 0.06300426 + 0.24606176 0.06162637 + 0.20545865 0.05914305 + 0.16774944 0.05560875 + 0.13325496 0.05110894 + 0.10227480 0.04574473 + 0.07506830 0.03963971 + 0.05185866 0.03292798 + 0.03280341 0.02578006 + 0.01802697 0.01840363 + 0.00756618 0.01109486 + 0.00190360 0.00492574 + 0.00084948 0.00303906 + 0.00019917 0.00130025 + 0.00000820 0.00024733 + 0.00007034 -0.00067752 + 0.00045908 -0.00154337 + 0.00115602 -0.00244115 + 0.00264982 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--- /dev/null +++ b/airfoil/data/mh64.dat @@ -0,0 +1,69 @@ +MH 64 8.59% + 1.00000000 0.00000000 + 0.99677882 -0.00001741 + 0.98710222 0.00007686 + 0.97112117 0.00061269 + 0.94919338 0.00180715 + 0.92172048 0.00378243 + 0.88920839 0.00666283 + 0.85230568 0.01046738 + 0.81167214 0.01507212 + 0.76794901 0.02030702 + 0.72177737 0.02595115 + 0.67378586 0.03173522 + 0.62451989 0.03733285 + 0.57443366 0.04248661 + 0.52396327 0.04699723 + 0.47352260 0.05074736 + 0.42356875 0.05368619 + 0.37459982 0.05577096 + 0.32710703 0.05694621 + 0.28156946 0.05716210 + 0.23841873 0.05635245 + 0.19802650 0.05449350 + 0.16073193 0.05158876 + 0.12682611 0.04768368 + 0.09657874 0.04285847 + 0.07022520 0.03720997 + 0.04794175 0.03084017 + 0.02980596 0.02392029 + 0.01588864 0.01672252 + 0.00622672 0.00960304 + 0.00199243 0.00486572 + 0.00090014 0.00302044 + 0.00022004 0.00132032 + 0.00001234 0.00029269 + 0.00006096 -0.00060685 + 0.00044110 -0.00144891 + 0.00113432 -0.00232546 + 0.00262979 -0.00368490 + 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0.97053611 -0.00126532 + 0.98671769 -0.00043308 + 0.99664775 -0.00007690 + 1.00000000 0.00000000 diff --git a/airfoil/data/mh82.dat b/airfoil/data/mh82.dat new file mode 100644 index 0000000..ccefd29 --- /dev/null +++ b/airfoil/data/mh82.dat @@ -0,0 +1,69 @@ +MH 82 13.31% + 1.00000000 0.00000000 + 0.99661459 0.00010716 + 0.98648759 0.00057417 + 0.96976242 0.00167959 + 0.94674359 0.00367565 + 0.91787545 0.00675919 + 0.88371761 0.01105153 + 0.84491677 0.01659048 + 0.80217789 0.02332527 + 0.75623764 0.03112511 + 0.70784007 0.03978495 + 0.65771739 0.04904355 + 0.60657341 0.05859424 + 0.55507239 0.06810553 + 0.50383005 0.07723291 + 0.45340892 0.08563711 + 0.40431563 0.09299494 + 0.35700062 0.09901144 + 0.31186073 0.10342997 + 0.26924218 0.10603084 + 0.22944828 0.10664471 + 0.19275386 0.10507496 + 0.15919742 0.10111480 + 0.12865471 0.09486478 + 0.10114620 0.08660842 + 0.07670830 0.07665259 + 0.05541508 0.06541510 + 0.03742189 0.05331020 + 0.02286177 0.04072192 + 0.01180557 0.02807192 + 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b/airfoil/data/mh83.dat new file mode 100644 index 0000000..501237a --- /dev/null +++ b/airfoil/data/mh83.dat @@ -0,0 +1,62 @@ +MH 83 13.29% + 1.00000000 0.00000000 + 0.99672899 0.00023531 + 0.98692015 0.00105909 + 0.97067687 0.00270324 + 0.94828399 0.00539362 + 0.92017987 0.00930135 + 0.88692215 0.01451151 + 0.84915122 0.02101885 + 0.80755444 0.02872112 + 0.76283812 0.03744000 + 0.71570277 0.04692639 + 0.66682923 0.05689064 + 0.61686578 0.06700863 + 0.56642450 0.07695042 + 0.51607614 0.08638244 + 0.46635061 0.09498995 + 0.41773609 0.10247569 + 0.37067945 0.10857433 + 0.32558827 0.11305067 + 0.28282991 0.11570049 + 0.24273788 0.11635457 + 0.20561919 0.11479920 + 0.17152651 0.11078192 + 0.14030239 0.10437574 + 0.11194905 0.09588278 + 0.08651914 0.08562563 + 0.06410720 0.07401037 + 0.04487146 0.06144195 + 0.02895817 0.04829127 + 0.01643834 0.03496114 + 0.00738178 0.02194452 + 0.00186084 0.00980901 + 0.00001234 -0.00071636 + 0.00251705 -0.00820350 + 0.01097300 -0.01311972 + 0.02576247 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a/airfoil/data/mh94.dat b/airfoil/data/mh94.dat new file mode 100644 index 0000000..37a8d3c --- /dev/null +++ b/airfoil/data/mh94.dat @@ -0,0 +1,69 @@ +MH 94 16.03% + 1.00000000 0.00000000 + 0.99614372 0.00075299 + 0.98517671 0.00333401 + 0.96830215 0.00791992 + 0.94649402 0.01402570 + 0.92026080 0.02095000 + 0.88973146 0.02820043 + 0.85508517 0.03563506 + 0.81672309 0.04314656 + 0.77508519 0.05056529 + 0.73062549 0.05773357 + 0.68381258 0.06451128 + 0.63516360 0.07079345 + 0.58523861 0.07644452 + 0.53457659 0.08131354 + 0.48369158 0.08527460 + 0.43309941 0.08823799 + 0.38331241 0.09012917 + 0.33483473 0.09089917 + 0.28815954 0.09051388 + 0.24376407 0.08895853 + 0.20210913 0.08623149 + 0.16363849 0.08232026 + 0.12870704 0.07719396 + 0.09757690 0.07091355 + 0.07057780 0.06364984 + 0.04819402 0.05539707 + 0.03057188 0.04577057 + 0.01719105 0.03470861 + 0.00764984 0.02283091 + 0.00189225 0.01087021 + 0.00009267 0.00224978 + 0.00001765 -0.00095529 + 0.00032505 -0.00396814 + 0.00075957 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Not Found

+

The requested URL /ads/coord/naca001034a08cli0.dat was not found on this server.

+

Additionally, a 404 Not Found +error was encountered while trying to use an ErrorDocument to handle the request.

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Not Found

+

The requested URL /ads/coord/naca001264a08cli0.dat was not found on this server.

+

Additionally, a 404 Not Found +error was encountered while trying to use an ErrorDocument to handle the request.

+ diff --git a/airfoil/data/naca0015.dat b/airfoil/data/naca0015.dat new file mode 100644 index 0000000..449700a --- /dev/null +++ b/airfoil/data/naca0015.dat @@ -0,0 +1,36 @@ +NACA 0015 +1.0000 0.00158 +0.9500 0.01008 +0.9000 0.01810 +0.8000 0.03279 +0.7000 0.04580 +0.6000 0.05704 +0.5000 0.06617 +0.4000 0.07254 +0.3000 0.07502 +0.2500 0.07427 +0.2000 0.07172 +0.1500 0.06682 +0.1000 0.05853 +0.0750 0.05250 +0.0500 0.04443 +0.0250 0.03268 +0.0125 0.02367 +0.0000 0.00000 +0.0125 -0.02367 +0.0250 -0.03268 +0.0500 -0.04443 +0.0750 -0.05250 +0.1000 -0.05853 +0.1500 -0.06682 +0.2000 -0.07172 +0.2500 -0.07427 +0.3000 -0.07502 +0.4000 -0.07254 +0.5000 -0.06617 +0.6000 -0.05704 +0.7000 -0.04580 +0.8000 -0.03279 +0.9000 -0.01810 +0.9500 -0.01008 +1.0000 -0.00158 diff --git a/airfoil/data/naca0018.dat b/airfoil/data/naca0018.dat new file mode 100644 index 0000000..d8e59c6 --- /dev/null +++ b/airfoil/data/naca0018.dat @@ -0,0 +1,36 @@ +NACA 0018 +1.0000 0.00189 +0.9500 0.01210 +0.9000 0.02172 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a/airfoil/data/rg14a147.dat b/airfoil/data/rg14a147.dat new file mode 100644 index 0000000..1c3b78e --- /dev/null +++ b/airfoil/data/rg14a147.dat @@ -0,0 +1,68 @@ +RG 14A-1.4/7.0 AIRFOIL + 32. 32. + + 0.0000000 0.0000000 + 0.0016300 0.0043300 + 0.0080100 0.0097600 + 0.0190500 0.0155400 + 0.0343100 0.0212800 + 0.0539200 0.0267800 + 0.0777200 0.0318700 + 0.1055800 0.0364400 + 0.1372900 0.0403900 + 0.1725800 0.0436300 + 0.2111900 0.0461300 + 0.2527700 0.0478300 + 0.2969800 0.0487400 + 0.3434000 0.0488500 + 0.3916300 0.0482000 + 0.4411800 0.0468400 + 0.4915800 0.0448300 + 0.5423100 0.0422500 + 0.5928500 0.0391800 + 0.6426700 0.0357200 + 0.6912300 0.0319800 + 0.7280000 0.0286000 + 0.7824100 0.0240500 + 0.8239200 0.0200800 + 0.8620700 0.0162500 + 0.8963600 0.0126400 + 0.9263600 0.0093400 + 0.9516200 0.0063800 + 0.9718900 0.0037500 + 0.9870500 0.0016400 + 0.9966700 0.0003800 + 1.0000000 0.0000000 + + 0.0000000 0.0000000 + 0.0031000 -.0033200 + 0.0095000 -.0061900 + 0.0215700 -.0096400 + 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a/airfoil/data/s1221.dat b/airfoil/data/s1221.dat new file mode 100644 index 0000000..73d5657 --- /dev/null +++ b/airfoil/data/s1221.dat @@ -0,0 +1,158 @@ +S1221 w/o flap + 1.00182 0.01052 + 1.00010 0.01125 + 0.99539 0.01347 + 0.98834 0.01676 + 0.97911 0.02033 + 0.96725 0.02380 + 0.95255 0.02730 + 0.94744 0.02839 + 0.87368 0.04200 + 0.79952 0.05285 + 0.72514 0.06224 + 0.65074 0.07145 + 0.64181 0.07259 + 0.60457 0.07717 + 0.56677 0.08157 + 0.52865 0.08577 + 0.49051 0.08975 + 0.45264 0.09349 + 0.41537 0.09693 + 0.37902 0.09992 + 0.34385 0.10232 + 0.31005 0.10396 + 0.27776 0.10469 + 0.24715 0.10447 + 0.21836 0.10298 + 0.19125 0.10011 + 0.16569 0.09601 + 0.14166 0.09077 + 0.11918 0.08461 + 0.09838 0.07771 + 0.07937 0.07022 + 0.06223 0.06222 + 0.04705 0.05386 + 0.03388 0.04528 + 0.02281 0.03663 + 0.01391 0.02808 + 0.00733 0.01969 + 0.00297 0.01152 + 0.00065 0.00384 + 0.00037 -0.00287 + 0.00271 -0.00774 + 0.00859 -0.01117 + 0.01809 -0.01422 + 0.03068 -0.01687 + 0.04619 -0.01910 + 0.06442 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diff --git a/airfoil/data/usa25.dat b/airfoil/data/usa25.dat new file mode 100644 index 0000000..30f3d93 --- /dev/null +++ b/airfoil/data/usa25.dat @@ -0,0 +1,38 @@ +USA 25 AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0123100 0.0178300 + 0.0246900 0.0292600 + 0.0495300 0.0445300 + 0.0743700 0.0559400 + 0.0993100 0.0652500 + 0.1491800 0.0777800 + 0.1990900 0.0863100 + 0.2990100 0.0933700 + 0.3990600 0.0887300 + 0.4991400 0.0814900 + 0.5992300 0.0723500 + 0.6993600 0.0603100 + 0.7995300 0.0446700 + 0.8997300 0.0259400 + 0.9498500 0.0137700 + 1.0000000 0.0000000 + + 0.0000000 0.0000000 + 0.0126300 -.0121700 + 0.0251500 -.0138300 + 0.0501600 -.0152700 + 0.0751400 -.0135000 + 0.1001100 -.0105400 + 0.1500300 -.0032100 + 0.1999600 0.0036200 + 0.2998800 0.0113800 + 0.3999000 0.0097400 + 0.4999600 0.0042000 + 0.6000300 -.0026400 + 0.7000800 -.0070800 + 0.8000801 -.0073200 + 0.9000500 -.0042600 + 0.9500200 -.0019300 + 1.0000000 0.0000000 diff --git a/airfoil/data/usa26.dat b/airfoil/data/usa26.dat new file mode 100644 index 0000000..1db33ae --- /dev/null +++ b/airfoil/data/usa26.dat @@ -0,0 +1,38 @@ +USA 26 AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0123000 0.0181400 + 0.0246800 0.0290700 + 0.0495100 0.0445400 + 0.0743800 0.0564200 + 0.0992800 0.0650900 + 0.1491500 0.0774400 + 0.1990500 0.0861900 + 0.2989900 0.0913900 + 0.3990300 0.0883900 + 0.4991100 0.0810900 + 0.5992100 0.0721900 + 0.6993400 0.0599900 + 0.7995099 0.0443900 + 0.8997200 0.0252000 + 0.9498500 0.0132500 + 1.0000000 0.0000000 + + 0.0000000 0.0000000 + 0.0126400 -.0125600 + 0.0251600 -.0151200 + 0.0501700 -.0158500 + 0.0751700 -.0159700 + 0.1001800 -.0166000 + 0.1501700 -.0150500 + 0.2001300 -.0120000 + 0.3000500 -.0049000 + 0.4000200 -.0016000 + 0.5000500 -.0042000 + 0.6000900 -.0086000 + 0.7001000 -.0090000 + 0.8000900 -.0084000 + 0.9000700 -.0063000 + 0.9500400 -.0032500 + 1.0000000 0.0000000 diff --git a/airfoil/data/usa27.dat b/airfoil/data/usa27.dat new file mode 100644 index 0000000..46fb03f --- /dev/null +++ b/airfoil/data/usa27.dat @@ -0,0 +1,38 @@ +USA 27 AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0125000 0.0204400 + 0.0250000 0.0325800 + 0.0500000 0.0518600 + 0.0750000 0.0651400 + 0.1000000 0.0754200 + 0.1500000 0.0889800 + 0.2000000 0.0985400 + 0.3000000 0.1056600 + 0.4000000 0.1037800 + 0.5000000 0.0969000 + 0.6000000 0.0850200 + 0.7000000 0.0711400 + 0.8000000 0.0522600 + 0.9000000 0.0293800 + 0.9500000 0.0159400 + 1.0000000 0.0002000 + + 0.0000000 0.0000000 + 0.0125000 -.0125600 + 0.0250000 -.0138200 + 0.0500000 -.0152400 + 0.0750000 -.0158600 + 0.1000000 -.0163800 + 0.1500000 -.0150200 + 0.2000000 -.0118600 + 0.3000000 -.0050400 + 0.4000000 -.0018200 + 0.5000000 -.0046000 + 0.6000000 -.0081800 + 0.7000000 -.0092600 + 0.8000000 -.0086400 + 0.9000000 -.0064200 + 0.9500000 -.0037600 + 1.0000000 0.0000000 diff --git a/airfoil/data/usa27m2.dat b/airfoil/data/usa27m2.dat new file mode 100644 index 0000000..51ed698 --- /dev/null +++ b/airfoil/data/usa27m2.dat @@ -0,0 +1,38 @@ +USA 27 mod. AIRFOIL + 17. 17. + + 0.0000000 0.0008300 + 0.0125000 0.0237100 + 0.0250000 0.0372400 + 0.0500000 0.0585800 + 0.0750000 0.0732700 + 0.1000000 0.0846300 + 0.1500000 0.0994000 + 0.2000000 0.1096100 + 0.3000000 0.1167600 + 0.4000000 0.1143700 + 0.5000000 0.1070700 + 0.6000000 0.0943600 + 0.7000000 0.0792000 + 0.8000000 0.0583600 + 0.9000000 0.0329700 + 0.9500000 0.0179100 + 1.0000000 0.0002200 + + 0.0000000 0.0008300 + 0.0125000 -.0159000 + 0.0250000 -.0184600 + 0.0500000 -.0219600 + 0.0750000 -.0239600 + 0.1000000 -.0255600 + 0.1500000 -.0254400 + 0.2000000 -.0229100 + 0.3000000 -.0161200 + 0.4000000 -.0123900 + 0.5000000 -.0147700 + 0.6000000 -.0175200 + 0.7000000 -.0173100 + 0.8000000 -.0147400 + 0.9000000 -.0100100 + 0.9500000 -.0057300 + 1.0000000 -.0000200 diff --git a/airfoil/data/usa28.dat b/airfoil/data/usa28.dat new file mode 100644 index 0000000..1c5a285 --- /dev/null +++ b/airfoil/data/usa28.dat @@ -0,0 +1,38 @@ +USA 28 AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0123300 0.0173200 + 0.0247400 0.0263400 + 0.0496000 0.0404900 + 0.0745000 0.0514300 + 0.0994100 0.0604700 + 0.1492700 0.0743600 + 0.1991700 0.0844500 + 0.2990600 0.0954300 + 0.3990600 0.0960100 + 0.4990900 0.0925900 + 0.5992000 0.0815700 + 0.6993400 0.0675500 + 0.7995200 0.0490400 + 0.8997200 0.0290200 + 0.9498300 0.0175100 + 1.0000000 0.0000000 + + 0.0000000 0.0000000 + 0.0126700 -.0171800 + 0.0252300 -.0233500 + 0.0503000 -.0306100 + 0.0753500 -.0355600 + 0.1003900 -.0394200 + 0.1504100 -.0416300 + 0.2004100 -.0416400 + 0.3003500 -.0361600 + 0.4002400 -.0249800 + 0.5001700 -.0175000 + 0.6001400 -.0144200 + 0.7001200 -.0118400 + 0.8000900 -.0094600 + 0.9000800 -.0084800 + 0.9500500 -.0054900 + 1.0000000 0.0000000 diff --git a/airfoil/data/usa29.dat b/airfoil/data/usa29.dat new file mode 100644 index 0000000..dcd86e2 --- /dev/null +++ b/airfoil/data/usa29.dat @@ -0,0 +1,38 @@ +USA 29 AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0120100 0.0178300 + 0.0242400 0.0274700 + 0.0487800 0.0441500 + 0.0734000 0.0580300 + 0.0980800 0.0695100 + 0.1475900 0.0874700 + 0.1972300 0.1003400 + 0.2968500 0.1140900 + 0.3968200 0.1152500 + 0.4970300 0.1075200 + 0.5974100 0.0937900 + 0.6978800 0.0767600 + 0.7985000 0.0544400 + 0.8992100 0.0286200 + 0.9496100 0.0142100 + 1.0000000 0.0000000 + + 0.0000000 0.0000000 + 0.0129600 -.0166400 + 0.0256200 -.0224900 + 0.0507400 -.0269000 + 0.0758300 -.0299100 + 0.1008400 -.0305200 + 0.1508400 -.0303400 + 0.2007600 -.0273600 + 0.3004800 -.0175100 + 0.4001100 -.0041600 + 0.5000700 -.0026000 + 0.6001400 -.0049400 + 0.7002700 -.0096700 + 0.8003200 -.0116100 + 0.9002500 -.0090500 + 0.9501700 -.0062800 + 1.0000000 0.0000000 diff --git a/airfoil/data/usa31.dat b/airfoil/data/usa31.dat new file mode 100644 index 0000000..51152f3 --- /dev/null +++ b/airfoil/data/usa31.dat @@ -0,0 +1,38 @@ +USA 31 AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0118100 0.0342200 + 0.0240000 0.0514400 + 0.0485600 0.0758800 + 0.0732700 0.0923200 + 0.0980200 0.1057700 + 0.1476700 0.1256700 + 0.1974200 0.1395600 + 0.2971700 0.1543600 + 0.3971400 0.1561600 + 0.4972800 0.1489600 + 0.5975600 0.1337700 + 0.6979500 0.1125700 + 0.7984900 0.0833700 + 0.8991800 0.0451900 + 0.9496200 0.0211000 + 1.0000000 0.0000000 + + 0.0000000 0.0000000 + 0.0126900 -.0147700 + 0.0252200 -.0165500 + 0.0502500 -.0181000 + 0.0752700 -.0186500 + 0.1002500 -.0182000 + 0.1501300 -.0144000 + 0.2005900 -.0085400 + 0.2999200 0.0122800 + 0.3993900 0.0311900 + 0.4994200 0.0299900 + 0.5995200 0.0248000 + 0.6996601 0.0176000 + 0.7998200 0.0094000 + 0.8999500 0.0022000 + 0.9500100 -.0009000 + 1.0000000 0.0000000 diff --git a/airfoil/data/usa32.dat b/airfoil/data/usa32.dat new file mode 100644 index 0000000..168d5f9 --- /dev/null +++ b/airfoil/data/usa32.dat @@ -0,0 +1,38 @@ +USA 32 AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0120700 0.0391300 + 0.0243700 0.0572700 + 0.0491100 0.0805400 + 0.0739400 0.0968100 + 0.0987900 0.1100900 + 0.1485700 0.1296300 + 0.1984100 0.1441800 + 0.2982600 0.1582800 + 0.3982500 0.1593800 + 0.4983300 0.1514800 + 0.5985200 0.1345800 + 0.6987400 0.1146900 + 0.7990700 0.0847900 + 0.8994800 0.0468900 + 0.9497200 0.0254500 + 1.0000000 0.0000000 + + 0.0000000 0.0000000 + 0.0126100 -.0098600 + 0.0251300 -.0117200 + 0.0501500 -.0134500 + 0.0751600 -.0141700 + 0.1001500 -.0139000 + 0.1501100 -.0103500 + 0.2000300 -.0028000 + 0.2998400 0.0143000 + 0.3997000 0.0274000 + 0.4997300 0.0245000 + 0.5998100 0.0176000 + 0.6999400 0.0057000 + 0.8000400 -.0032000 + 0.9000599 -.0051000 + 0.9500400 -.0035500 + 1.0000000 0.0000000 diff --git a/airfoil/data/usa33.dat b/airfoil/data/usa33.dat new file mode 100644 index 0000000..6217720 --- /dev/null +++ b/airfoil/data/usa33.dat @@ -0,0 +1,38 @@ +USA 33 AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0120700 0.0361400 + 0.0243800 0.0512900 + 0.0491900 0.0675900 + 0.0740200 0.0813900 + 0.0988900 0.0921900 + 0.1487300 0.1057800 + 0.1986300 0.1143800 + 0.2985700 0.1195800 + 0.3986100 0.1157800 + 0.4987600 0.1029900 + 0.5989700 0.0861900 + 0.6992000 0.0663900 + 0.7994600 0.0445900 + 0.8997100 0.0238000 + 0.9498300 0.0124000 + 1.0000000 0.0000000 + + 0.0000000 0.0000000 + 0.0127900 -.0238500 + 0.0253700 -.0307000 + 0.0504100 -.0344000 + 0.0754300 -.0360900 + 0.1004300 -.0357900 + 0.1503700 -.0312000 + 0.2003100 -.0256000 + 0.3002700 -.0224000 + 0.4002900 -.0242000 + 0.5003200 -.0270000 + 0.6003500 -.0288000 + 0.7003300 -.0276000 + 0.8002600 -.0214000 + 0.9001500 -.0122000 + 0.9500800 -.0066000 + 1.0000000 0.0000000 diff --git a/airfoil/data/usa34.dat b/airfoil/data/usa34.dat new file mode 100644 index 0000000..2c6b91a --- /dev/null +++ b/airfoil/data/usa34.dat @@ -0,0 +1,38 @@ +USA 34 AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0110100 0.0433500 + 0.0229800 0.0597400 + 0.0472500 0.0825200 + 0.0717500 0.0983100 + 0.0963100 0.1121000 + 0.1456900 0.1316700 + 0.1952200 0.1462600 + 0.2947200 0.1624500 + 0.3947000 0.1636500 + 0.4950200 0.1538600 + 0.5955700 0.1370700 + 0.6964400 0.1103000 + 0.7974700 0.0785300 + 0.8985900 0.0437600 + 0.9492100 0.0243800 + 1.0000000 0.0000000 + + 0.0000000 0.0000000 + 0.0128600 -.0145900 + 0.0255600 -.0211900 + 0.0508600 -.0303800 + 0.0759500 -.0330800 + 0.1009900 -.0337800 + 0.1509000 -.0311800 + 0.2007900 -.0275800 + 0.3004800 -.0173900 + 0.4002300 -.0091900 + 0.5001000 -.0050000 + 0.6000400 -.0028000 + 0.7000500 -.0026000 + 0.8000801 -.0034000 + 0.9001300 -.0042000 + 0.9501400 -.0046000 + 1.0000000 0.0000000 diff --git a/airfoil/data/usa35.dat b/airfoil/data/usa35.dat new file mode 100644 index 0000000..8008e5a --- /dev/null +++ b/airfoil/data/usa35.dat @@ -0,0 +1,38 @@ +USA 35 AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0109300 0.0380500 + 0.0228000 0.0534400 + 0.0468400 0.0769300 + 0.0710700 0.0954200 + 0.0955000 0.1094300 + 0.1447100 0.1286500 + 0.1941600 0.1418900 + 0.2937000 0.1530900 + 0.3937700 0.1515000 + 0.4943000 0.1386400 + 0.5950500 0.1202900 + 0.6960300 0.0965400 + 0.7971900 0.0683000 + 0.8984800 0.0369700 + 0.9491900 0.0196600 + 1.0000000 0.0021500 + + 0.0000000 0.0000000 + 0.0135900 -.0265400 + 0.0263500 -.0327200 + 0.0515200 -.0369800 + 0.0765600 -.0379500 + 0.1015700 -.0381200 + 0.1515300 -.0370600 + 0.2014200 -.0344100 + 0.3011700 -.0284100 + 0.4009200 -.0224000 + 0.5006900 -.0167000 + 0.6004900 -.0118900 + 0.7003300 -.0079800 + 0.8002000 -.0048700 + 0.9001300 -.0030600 + 0.9500901 -.0023000 + 1.0000000 -.0021500 diff --git a/airfoil/data/usa35a.dat b/airfoil/data/usa35a.dat new file mode 100644 index 0000000..a4714d1 --- /dev/null +++ b/airfoil/data/usa35a.dat @@ -0,0 +1,38 @@ +USA 35 A AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0109300 0.0380500 + 0.0228000 0.0534400 + 0.0468400 0.0769300 + 0.0710700 0.0954200 + 0.0955000 0.1094300 + 0.1447100 0.1286500 + 0.1941600 0.1418900 + 0.2937000 0.1530900 + 0.3937700 0.1515000 + 0.4943000 0.1386400 + 0.5950500 0.1202900 + 0.6960300 0.0965400 + 0.7971900 0.0683000 + 0.8984800 0.0369700 + 0.9491900 0.0196600 + 1.0000000 0.0021500 + + 0.0000000 0.0000000 + 0.0135900 -.0265400 + 0.0263400 -.0326200 + 0.0515200 -.0369800 + 0.0765600 -.0379500 + 0.1015700 -.0380200 + 0.1515300 -.0370600 + 0.2014100 -.0342100 + 0.3011700 -.0284100 + 0.4009200 -.0224000 + 0.5006700 -.0162000 + 0.6005000 -.0120900 + 0.7003300 -.0079800 + 0.8001800 -.0044700 + 0.9001300 -.0030600 + 0.9500901 -.0023000 + 1.0000000 -.0021500 diff --git a/airfoil/data/usa35b.dat b/airfoil/data/usa35b.dat new file mode 100644 index 0000000..5034671 --- /dev/null +++ b/airfoil/data/usa35b.dat @@ -0,0 +1,38 @@ +USA-35B AIRFOIL + 17.0 17.0 + + 0.0000000 0.0000000 + 0.0125000 0.0239000 + 0.0250000 0.0335000 + 0.0500000 0.0476000 + 0.0750000 0.0589000 + 0.1000000 0.0669000 + 0.1500000 0.0780000 + 0.2000000 0.0852000 + 0.3000000 0.0900000 + 0.4000000 0.0866000 + 0.5000000 0.0757000 + 0.6000000 0.0605000 + 0.7000000 0.0432000 + 0.8000000 0.0226000 + 0.9000000 -.0004000 + 0.9500000 -.0126000 + 1.0000000 -.0251000 + + 0.0000000 0.0000000 + 0.0125000 -.0173000 + 0.0250000 -.0213000 + 0.0500000 -.0248000 + 0.0750000 -.0262000 + 0.1000000 -.0269000 + 0.1500000 -.0276000 + 0.2000000 -.0270000 + 0.3000000 -.0261000 + 0.4000000 -.0250000 + 0.5000000 -.0237000 + 0.6000000 -.0231000 + 0.7000000 -.0234000 + 0.8000000 -.0241000 + 0.9000000 -.0256000 + 0.9500000 -.0264000 + 1.0000000 -.0276000 diff --git a/airfoil/data/usa40.dat b/airfoil/data/usa40.dat new file mode 100644 index 0000000..059ac95 --- /dev/null +++ b/airfoil/data/usa40.dat @@ -0,0 +1,38 @@ +USA 40 AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0125100 0.0263000 + 0.0250100 0.0360000 + 0.0500100 0.0562900 + 0.0750100 0.0686900 + 0.1000200 0.0789800 + 0.1500200 0.0935700 + 0.2000200 0.1019600 + 0.3000200 0.1071400 + 0.4000200 0.1035200 + 0.5000200 0.0949000 + 0.6000200 0.0815800 + 0.7000100 0.0655600 + 0.8000100 0.0465400 + 0.9000100 0.0251200 + 0.9500000 0.0135100 + 1.0000000 0.0005000 + + 0.0000000 0.0000000 + 0.0125000 -.0190000 + 0.0250000 -.0240100 + 0.0499900 -.0287100 + 0.0749900 -.0307200 + 0.0999900 -.0320200 + 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a/airfoil/data/usa48.dat b/airfoil/data/usa48.dat new file mode 100644 index 0000000..6892485 --- /dev/null +++ b/airfoil/data/usa48.dat @@ -0,0 +1,38 @@ +USA 48 AIRFOIL + 17. 17. + + 0.0000000 0.0000000 + 0.0125000 0.0220000 + 0.0250000 0.0320000 + 0.0500000 0.0480000 + 0.0750000 0.0610000 + 0.1000000 0.0690000 + 0.1500000 0.0828000 + 0.2000000 0.0922000 + 0.3000000 0.1010000 + 0.4000000 0.1015000 + 0.5000000 0.0948000 + 0.6000000 0.0836000 + 0.7000000 0.0683000 + 0.8000000 0.0507000 + 0.9000000 0.0287000 + 0.9500000 0.0160000 + 1.0000000 0.0000000 + + 0.0000000 0.0000000 + 0.0125000 -.0140000 + 0.0250000 -.0200000 + 0.0500000 -.0270000 + 0.0750000 -.0343000 + 0.1000000 -.0383000 + 0.1500000 -.0453000 + 0.2000000 -.0480000 + 0.3000000 -.0480000 + 0.4000000 -.0440000 + 0.5000000 -.0390000 + 0.6000000 -.0320000 + 0.7000000 -.0197000 + 0.8000000 -.0110000 + 0.9000000 -.0057000 + 0.9500000 -.0027000 + 1.0000000 0.0000000 diff --git a/airfoil/data/usa49.dat b/airfoil/data/usa49.dat new 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