The effects of amount and type of camber on the variation with Mach number of the aerodynamic characteristics of a 10-percent-thick NACA 64A- series airfoil section
1950-05-01
Sonstige
Keine Angabe
Englisch
AIRFOILS, CAMBERED , WIND TUNNEL TESTS - AAL - HIGH-SPEED (3 1/2'X1') , AIRFOILS - NACA 64A310(A=0 4) - CHAR , MOMENTS & ORDINATES LOW-DRAG , AIRFOILS - NACA 64A010 - CHAR , MOMENTS & ORDINATES LOW-DRAG , PRESSURE DISTRIBUTION - AIRFOILS , AIRFOILS - NACA 641610(A=0 4) - CHAR , MOMENTS & ORDIANTES LOW-DRAG , AIRFOILS - NACA 64A310 - CHAR , MOMENTS & ORDINATES LOW-DRAG , PRESSURE DISTRIBUTION - AIRFOILS - NACA 64A010 , AIRFOILS - NACA 64A910 - CHAR , MOMENTS & ORDINATES LOW-DRAG , AIRFOILS - NACA 64A610 - CHAR , MOMENTS & ORDINATES LOW-DRAG