Investigation of the Variation of Lift Coefficient with Reynolds Number at a Moderate Angle of Attack on a Low-Drag Airfoil
1942-01-01
Miscellaneous
No indication
English
PHOTOGRAPHY - AIR FLOW - AIRFOILS LAMPBLACK , BOUNDARY LAYER - VELOCITY DISTRIBUTION , AIRFOILS - ANGLE OF ATTACK , REYNOLDS NUMBER , AIRFOILS - NACA 66,2-216 - CHARACTERISTICS LOW-DRAG , LIFT COEFFICIENTS - AIRFOILS , BOUNDARY LAYER SEPARATION - AIRFOILS , PRESSURE DISTRIBUTION - AIRFOILS - NACA 66,2-216 , WIND TUNNEL TESTS - NACA - LOW-TURBULENCE (7 1/2' X 3')
PLUNGING AIRFOIL: REYNOLDS NUMBER AND ANGLE OF ATTACK EFFECTS
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