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- Calculation of the chordwise load distribution over airfoil sections with plain, split, or serially hinged trailing-edge flaps
- A simplified method for the calculation of airfoil pressure distribution
- Experimental Investigation of a New Type of Low-Drag Wing-Nacelle Combination
- A method for calculating heat transfer in the laminar flow region of bodies
- Notes on the Effect of Surface Distortions on the Drag and Critical Mach Number of Airfoils
- The Effect of Compressibility on the Growth of the Laminar Boundary Layer on Low-Drag Wings and Bodies
- Wall interference in a two-dimensional-flow wind tunnel, with consideration of the effect of compressibility
- An Experimental Investigation of Several Low-Drag Wing-Nacelle Combinations with Internal Air Flow
- General theory of airfoil sections having arbitrary shape or pressure distribution
- The interaction of boundary layer and compression shock and its effect upon airfoil pressure distributions
- The Effect of Compressibility on the Growth of the Laminar Boundary Layer on Low-Drag Wings and Bodies
- Estimation of the forces and moments acting on inclined bodies of revolution of high fineness ratio
- Characteristics of flow over inclined bodies of revolution
- A study of effects of viscosity on flow over slender inclined bodies of revolution
- The asymmetric adjustable supersonic nozzle for wind-tunnel application
- A Study of the Motion and Aerodynamic Heating of Missiles Entering the Earth's Atmosphere at High Supersonic Speeds
- A study of the motion and aerodynamic heating of ballistic missiles entering the earth's atmosphere at high supersonic speeds
- A comparative analysis of the performance of long-range hypervelocity vehicles
- A comparative analysis of the performance of long-range hypervelocity vehicles
- Problems of performance and heating of hypersonic vehicles
- Motion of a ballistic missile angularly misaligned with the flight path upon entering the atmosphere and its effect upon aerodynamic heating, aerodynamic loads, and miss distance
- Motion of a ballistic missile angularly misaligned with the flight path upon entering the atmosphere and its effect upon aerodynamic heating, aerodynamic loads, and miss distance
- A Study of the Motion and Aerodynamic Heating of Missiles Entering the Earth's Atmosphere at High Supersonic Speeds