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- NACA Investigation of a Jet-Propulsion System Applicable to Flight
- A method for the calculation of external lift, moment, and pressure drag of slender open-nose bodies of revolution at supersonic speeds
- Theoretical lift and drag of thin triangular wings at supersonic speeds
- Internal and external aerodynamics of ducted bodies at supersonic speeds
- Theoretical lift and drag of thin triangular wings at supersonic speeds
- Damping in pitch and roll of triangular wings at supersonic speeds
- Damping in pitch and roll of triangular wings at supersonic speeds
- Investigation of Minimum Drag and Maximum Lift-Drag Ratios of Several Wing-Body Combinations Including a Cambered Triangular Wing at Low Reynolds Numbers and at Supersonic Speeds
- On slender delta wings with leading-edge separation
- Investigation of Minimum Drag and Maximum Lift-Drag Ratios of Several Wing-Body Combinations Including a Cambered Triangular Wing at Low Reynolds Numbers and at Supersonic Speeds