John A. Axelson, W. P. Nelms
Abstract
Wing elevation, incidence, and chamber effects on aerodynamic characteristics of representative hypersonic cruise configuration at Mach numbers from 0.65 to 10.70
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Wing elevation, incidence, and chamber effects on aerodynamic characteristics of representative hypersonic cruise configuration at Mach numbers from 0.65 to 10.70
Key concepts: Camber (aerodynamics), Aerodynamics, Mach number, Wing, Hypersonic speed, Cruise, Aerospace engineering, Elevation (ballistics)