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← Airfoil Catalog
IST-MT1-21
Filename
ist-mt1-21.dat
t/c
21.0%
Max Camber
5.7%
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Reynolds Number
i
Include Mach Number
i
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Errors & Warnings
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GOE 386
t/c 20.3% · Max Camber 5.4%
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t/c 22.0% · Max Camber 6.0%
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t/c 20.2% · Max Camber 5.0%
NACA 6-H-20
t/c 20.0% · Max Camber 6.1%
