38 lines
791 B
Text
38 lines
791 B
Text
CLARK V AIRFOIL
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17. 17.
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0.0000000 0.0000000
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0.0125000 0.0195000
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0.0250000 0.0289100
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0.0500000 0.0424100
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0.0750000 0.0522200
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0.1000000 0.0601300
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0.1500000 0.0715500
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0.2000000 0.0795600
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0.3000000 0.0885900
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0.4000000 0.0914200
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0.5000000 0.0886500
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0.6000000 0.0809800
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0.7000000 0.0688100
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0.8000000 0.0519400
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0.9000000 0.0299700
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0.9500000 0.0163800
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1.0000000 0.0014000
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0.0000000 0.0000000
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0.0125000 -.0138000
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0.0250000 -.0182900
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0.0500000 -.0230900
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0.0750000 -.0255800
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0.1000000 -.0273700
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0.1500000 -.0289500
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0.2000000 -.0294400
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0.3000000 -.0278100
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0.4000000 -.0241800
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0.5000000 -.0201500
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0.6000000 -.0161200
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0.7000000 -.0120900
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0.8000000 -.0080600
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0.9000000 -.0040300
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0.9500000 -.0020100
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1.0000000 0.0000000
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