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- Effect of Turbulence on Air-Flow Measurements Behind Orifice Plates
- Analysis of the High-Altitude Cooling of the Ranger SGV-770 D-4 Engine in the Bell XP-77 Airplane
- High-Altitude Cooling 3: Radiators
- Compressibility Effects on Heat Transfer and Pressure Drop in Smooth Cylindrical Tubes
- Investigation of wing characteristics at a Mach number of 1.53 1: triangular wings of aspect ratio 2
- Effect of Aspect Ratio and Taper on the Pressure Drag at Supersonic Speeds of Unswept Wings at Zero Lift
- Charts for the conical part of the downwash field of swept wings at supersonic speeds
- Investigation of wing characteristics at a Mach number of 1.53 3: unswept wings of differing aspect ratio and taper ratio
- Calculative method for estimating the interference pressure field at zero lift on a symmetrical swept-back wing mounted on a circular cylindrical body