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Wing load distribution on a swept wing airplane in flight at Mach numbers up to 1.11, and comparison with theory

Linda Rolls, Frederick H Matteson

Abstract

Report presenting flight tests to determine the pressure distribution over the wing of a swept-wing jet-propelled airplane over the flight range of lift coefficients for Mach numbers up to 1.11. Results regarding the section characteristics, load distribution, and trailing-edge loads are provided.

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Key concepts: Wing, Airplane, Mach number, Wing loading, Aerospace engineering, Wing configuration, Wing twist, Trailing edge