1975•NASA STI Repository (National Aeronautics and Space Administration)Open access

Aerodynamic characteristics of a tandem wing configuration of a Mach number of 0.30

W. P. Henderson, J. K. Huffman

Abstract

An investigation was conducted to determine the aerodynamic characteristics of a tandem wing configuration. The configuration had a low forward mounted sweptback wing and a high rear mounted sweptforward wing jointed at the wing tip by an end plate. The investigation was conducted at a Mach number of 0.30 at angles of attack up to 20 deg. A comparison of the experimentally determined drag due to lift characteristics with theoretical estimates is also included.

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Key concepts: Wing, Wing twist, Wing configuration, Mach number, Aerodynamics, Wing loading, Lift-induced drag, Drag