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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


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