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- Transonic Aerodynamic and Trim Characteristics of 1/15-Scale Models of the Convair MX-1964 Airplane With Indented Fuselage
- Pressure Distributions on Three Bodies of Revolution to Determine the Effect of Reynolds Number Up to and Including the Transonic Speed Range
- Wake Surveys in the Slipstream of a Full-Scale Supersonic-Type Three-Blade Propeller at Mach Numbers to 0.96
- Transonic Aerodynamic Characteristics of a 1/15-Scale Model of the Convair B-58 Airplane
- Transonic Aerodynamic and Trim Characteristics of a Multi-Engine Delta-Wing Airplane Model
- Transonic Aerodynamic Characteristics of a 1/15-Scale Model of the Convair B-58 Airplane
- Effect of Blade-Section Camber on Aerodynamic Characteristics of Full-Scale Supersonic-Type Propellers at Mach Numbers to 1.04
- Steady loads due to jet interference on wings, tails, and fuselages at transonic speeds
- Transonic Loads Characteristics of a 3-Percent-Thick 60 Degree Delta-Wing-Body Combination
- Performance of multiple jet-exit installations
- Performance of Multiple Jet-Exit Installations
- Effect of Target-Type Thrust Reverser on Transonic Aerodynamic Characteristics of a Single-Engine Fighter Model