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Transonic Wind-tunnel Investigation of the Aerodynamic Loading Characteristics of a 60 Degree Delta Wing in the Presence of a Body with and Without Indentation

John P. Mugler

Abstract

Report presenting an investigation in the transonic pressure tunnel to determine the aerodynamic loading characteristics of a 60 degree delta wing in the presence of a body with and without body indentation in accordance with the transonic-area-rule concept. Tests covered a range of angles of attack and Mach numbers. Results regarding force and moment coefficients and curves are provided.

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Available abstract

Key concepts: Transonic, Aerodynamics, Delta wing, Wind tunnel, Mach number, Wing, Indentation, Degree (music)