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- Investigation of Slipstream Effects on a Wing-Inlet Oil-Cooler Ducting System of a Twin-Engine Airplane in the Ames 40- by 80-Foot Wind Tunnel
- Experimental investigation of the effects of viscosity on the drag of bodies of revolution at a Mach number 1.5
- Experimental investigation of the effects of viscosity on the drag and base pressure of bodies of revolution at a Mach number 1.5
- Laminar mixing of a compressible fluid
- Reduction of profile drag at supersonic velocities by the use of airfoil sections having a blunt trailing edge
- Laminar mixing of a compressible fluid
- An analysis of base pressure at supersonic velocities and comparison with experiment
- An analysis of base pressure at supersonic velocities and comparison with experiment
- Experimental investigation of base pressure on blunt-trailing-edge wings at supersonic velocities
- Aerodynamic Characteristics of Bodies at Supersonic Speeds: A Collection of Three Papers
- Airfoil profiles for minimum pressure drag at supersonic velocities -- general analysis with application to linearized supersonic flow
- Effect of trailing edge thickness on lift at supersonic velocities
- Airfoil profiles for minimum pressure drag at supersonic velocities: Application of shock-expansion theory, including consideration of hypersonic range
- Turbulent boundary-layer and skin-friction measurements in axial flow along cylinders at Mach numbers between 0.5 and 3.6
- Effect of trailing-edge thickness on lift at supersonic velocities
- Reduction of profile drag at supersonic velocities by the use of airfoil sections having a blunt trailing edge
- Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition
- Some possibilities of using gas mixtures other than air in aerodynamic research
- Preliminary report on a study of separated flows in supersonic and subsonic streams
- A theoretical analysis of heat transfer in regions of separated flow
- Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition
- An approximate analytical method for studying entry into planetary atmospheres