38 lines
792 B
Text
38 lines
792 B
Text
NACA M11 AIRFOIL
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17. 17.
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0.0000000 0.0000000
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0.0125000 0.0145700
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0.0250000 0.0210300
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0.0500000 0.0297700
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0.0750000 0.0363100
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0.1000000 0.0415400
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0.1500000 0.0494100
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0.2000000 0.0547800
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0.3000000 0.0595200
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0.4000000 0.0586600
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0.5000000 0.0535000
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0.6000000 0.0454400
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0.7000000 0.0351800
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0.8000000 0.0239200
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0.9000000 0.0120600
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0.9500000 0.0059300
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1.0000000 0.0000000
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0.0000000 0.0000000
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0.0125000 -.0120300
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0.0250000 -.0146700
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0.0500000 -.0175300
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0.0750000 -.0191900
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0.1000000 -.0200600
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0.1500000 -.0208900
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0.2000000 -.0214200
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0.3000000 -.0219800
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0.4000000 -.0221400
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0.5000000 -.0219000
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0.6000000 -.0207600
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0.7000000 -.0185200
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0.8000000 -.0146800
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0.9000000 -.0093400
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0.9500000 -.0062700
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1.0000000 0.0000000
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