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Scale and Turbulence Effects on the Lift and Drag Characteristics of the NACA 65(Sub 3)-418, A=1.0 Airfoil Section

Scale-effect tests in a turbulent tunnel of the NACA 65(sub 3)-418, a = 1.0 airfoil section with 0.20-airfoil-chord split flap

Preliminary Tests of a Buffet Stall-Warning Device on a 1/5-Scale Model of the Republic XP-84 Airplane

Drag characteristics of rectangular and swept-back NACA 65-009 airfoils having various aspect ratios as determined by flight tests at supersonic speeds

The flexible rectangular wing in roll at supersonic flight speeds

Characteristics of thin triangular wings with constant-chord partial-span control surfaces at supersonic speeds

Theoretical characteristics in supersonic flow of constant-chord partial-span control surfaces on rectangular wings having finite thickness

The effect of torsional flexibility on the rolling characteristics at supersonic speeds of tapered unswept wings

Theoretical characteristics in supersonic flow of two types of control surfaces on triangular wings

A Method for Estimating the Components of Lift of Wing-Body Combinations at Supersonic Speeds


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