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1958•Unpublished venueRequires access

Investigation of aerodynamic characteristics of an airplane configuration having tail surfaces outboard of the wing tips at Mach numbers of 2.30, 2.97, and 3.51

James D. Church, W. C. Hayes, William C. Sleeman

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Abstract

Aerodynamic characteristics of aircraft configuration having tail surfaces outboard of wing tips at supersonic speeds - wind tunnel stability test

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What this paper is about

Aerodynamic characteristics of aircraft configuration having tail surfaces outboard of wing tips at supersonic speeds - wind tunnel stability test

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Available abstract

Aerodynamic characteristics of aircraft configuration having tail surfaces outboard of wing tips at supersonic speeds - wind tunnel stability test

Key concepts: Airplane, Wing, Mach number, Aerodynamics, Aerospace engineering, Wing configuration, Wing loading, Aeronautics

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Investigation of aerodynamic characteristics of an airplane configuration having tail surfaces outboard of the wing tips at Mach numbers of 2.30, 2.97, and 3.51 — Research Paper | ScholarLens