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← Airfoil Catalog
NASA NLF(1)-1015
Filename
nlf1015.dat
t/c
15.0%
Max Camber
4.7%
Download Selig Coordinates
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Quick Analysis
Reynolds Number
i
Include Mach Number
i
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No
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Errors & Warnings
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t/c 15.2% · Max Camber 4.5%
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t/c 15.2% · Max Camber 4.9%
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