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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
- Characteristics of thin triangular wings with constant-chord partial-span control surfaces at supersonic speeds
- The flexible rectangular wing in roll at supersonic flight 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