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An investigation of several NACA 1-series nose inlets with and without protruding central bodies at high-subsonic Mach numbers and at a Mach number of 1.2
An investigation of three transonic fuselage air inlets at Mach numbers from 0.4 to 0.94 and at a Mach number of 1.19
The effects of wing incidence on the aerodynamic loading characteristics of a sweptback wing-body combination at transonic speeds
Pressures and Associated Aerodynamic and Load Characteristics for Two Bodies of Revolution at Transonic Speeds
The Effect of Canopy Location on the Aerodynamic Characteristics of a Sweptback Wing-Body Configuration at Transonic Speeds