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Wing-fuselage interference comparison of conventional and airfoil-type-fuselage combinations

Albert Sherman

Abstract

Report presenting tests of wing-fuselage combinations employing an airfoil-type fuselage in the variable-density wind tunnel as part of a wing-fuselage program. The models were designed to simulate an existing moderate-size transport airplane of that type. Results regarding some general comparisons, lift distribution and induced drag, and drag in high-speed flight are provided.

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Available abstract

Key concepts: Fuselage, Airplane, Airfoil, Wing, Lift-to-drag ratio, Structural engineering, Aerodynamics, Wind tunnel