Aerodynamic Characteristics of the NACA 8-H-12 Airfoil Section at Six Reynolds Numbers from 1.8 x 10(exp 6) to 11.0 x 10(exp 6).
1949-12-01
Miscellaneous
No indication
English
AIRFOILS - NACA 8-H-12 - CHAR , A C , MOMENTS & ORDINATES LOW-DRAG , AIRFOILS - CHARACTERISTICS EFFECT OF SURFACE ROUGHNESS , AIRFOILS - NACA 0012 - CHARACTERISTICS , AIRFOILS - NACA 23012 - CHARACTERISTICS , REYNOLDS NUMBER , ROTOR BLADE , WIND TUNNEL TESTS - NACA - PRESSURE, LOW-TURBULENCE ( 7 1/2'X 3')
Engineering Index Backfile | 1949
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