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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
- Lift and pitching-moment interference between a pointed cylindrical body and triangular wings of various aspect ratios at Mach numbers of 1.50 and 2.02
- Method for estimating lift interference of wing-body combinations at supersonic speeds
- Method for Estimating Lift Interference of Wing-Body Combinations at Supersonic Speeds
- Wing-body interference at supersonic speeds with an application to combinations with rectangular wings
- Comparison between prediction and experiment for all-movable wing and body combinations at supersonic speeds: Lift, pitching moment, and hinge moment
- Lift and center of pressure of wing-body-tail combinations at subsonic, transonic, and supersonic speeds
- Comparison between theory and experiment for interference pressure field between wing and body at supersonic speeds
- Quasi-Cylindrical Theory of Wing-Body Interference at Supersonic Speeds and Comparison with Experiment
- General theory of wave-drag reduction for combinations employing quasi-cylindrical bodies with an application to swept-wing and body combinations
- Lift and pitching-moment interference between a pointed cylindrical body and triangular wings of various aspect ratios at Mach numbers of 1.50 and 2.02
- Tables of Characteristic Functions for Solving Boundary-Value Problems of the Wave Equation with Application to Supersonic Interference
- The Effects of Body Vortices and the Wing Shock-Expansion Field on the Pitch-Up Characteristics of Supersonic Airplanes
- The Effects of Body Vortices and the Wing Shock-Expansion Field on the Pitch-Up Characteristics of Supersonic Airplanes