Jr.: Aerodynamic Characteristics at Mach Numbers of 2.30, 2.60, and 2.96 of a Supersonic Transport Model With a Blended Wing-Body (1963)

by A Warner Robins, M Leroy Spearman, Roy V Harris
Venue:Variable-Sweep Auxiliary Wing Panels, Outboard Tail Surfaces, and a Design Mach Number of 2.6. NASA TM X-815