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Load Distribution over a Fuselage in Combination with a Swept Wing at Small Angles of Attack and Transonic Speeds

Maurice D White, B. C. Look

Abstract

Report presenting free-fall tests of a wing-body configuration with a 45 degree sweptback cambered and twisted wing of aspect ratio 6 on a fuselage of fineness ratio 12.4. Results regarding the load and pitching moments and load-coefficient distribution are provided.

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Available abstract

Key concepts: Fuselage, Wing, Transonic, Structural engineering, Angle of attack, Swept wing, Engineering, Aerospace engineering