Standard data from literature incorporated into program. Comprehensive and easily-accessible data bank of aerodynamic characteristics of NACA 16series airfoils incorporated into AIRFOIL program for use in propeller performance research. Low-drag, high-critical-speed airfoils effective in advanced turbo-prop designs currently under investigation. AIRFOIL written in FORTRAN IV for batch execution.
Aerodynamic Characteristics of NACA 16-Series Airfoils
NASA Tech Briefs ; 10 , 2
1986-06-01
Miscellaneous
No indication
English
Aerodynamic characteristics of 24 NACA 16-series airfoils at Mach numbers between 0.3 and 0.8
Engineering Index Backfile | 1948
|Preliminary report on characteristics of NACA 4400r series airfoils
Engineering Index Backfile | 1949
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