Aerodynamic Characteristics at Mach Numbers from 1.61 to 2.86 of a Supersonic Transport Model with a Blended Wing-body, Variable- Sweep Auxiliary Wing Panels, Outboard Tail Surfaces, and a Design Mach Number of 2.2

Aerodynamic Characteristics at Mach Numbers from 1.61 to 2.86 of a Supersonic Transport Model with a Blended Wing-body, Variable- Sweep Auxiliary Wing Panels, Outboard Tail Surfaces, and a Design Mach Number of 2.2
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Total Pages: 66
Release: 1963
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