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Aerodynamic characteristics of a 55 deg clipped-delta-wing orbiter model at Mach numbers from 1.60 to 4.63

A. B. Blair, J. W. Grow

Abstract

Wind tunnel tests to determine the supersonic aerodynamic characteristics of a delta wing space shuttle orbiter model were conducted. The model was tested at Mach numbers from 1.60 to 4.63, at nominal angles of attack from minus 2 degrees to plus 30 degrees, nominal sideslip angles of minus 4 degrees to plus 10 degrees, and Reynolds numbers from 1.8 to 2.5 times one million per foot.

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Key concepts: Orbiter, Mach number, Aerodynamics, Supersonic speed, Wing, Space Shuttle, Delta wing, Angle of attack