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Aerodynamic characteristics of a wing with unswept quarter-chord line, aspect ratio 2, taper ratio 0.78, and NACA 65A004 airfoil section: transonic-bump method

Edward C Polhamus, George S. Campbell

Abstract

From Introduction: This paper presents the results of an investigation of force and moment characteristics for a wing with an unswept quarter-chord line, aspect ratio 2, taper ratio 0.78, and an NACA 65A004 airfoil section parallel to the free stream.

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Key concepts: Airfoil, Chord (peer-to-peer), Aspect ratio (aeronautics), Wing, Aerodynamics, NACA airfoil, Transonic, Stall (fluid mechanics)