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Investigation of the Aerodynamic Characteristics in Pitch and Sideslip of a 45 Degree Sweptback-wing Airplane Model with Various Vertical Locations of the Wing and Horizontal Tail : Effect of Wing Location and Geometric Dihedral for the Wing-body Com

M Leroy Spearman

Abstract

Memorandum presenting an investigation conducted in the 4- by 4-foot supersonic pressure tunnel to determine the effects of wing vertical location and geometric dihedral on the aerodynamic characteristics in pitch and sideslip of a wing-body configuration at Mach number 2.01. The configurations investigated included a high-wing, midwing, and a low-wing arrangement.

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Key concepts: Wing, Wing twist, Wing loading, Aerodynamics, Wing configuration, Airplane, Angle of attack, Aerospace engineering