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Aerodynamic characteristics of a wing with quarter-chord line swept back 35 degrees, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil section : transonic-bumb method

William C. Sleeman, Robert E Becht

Abstract

From Introduction: This paper presents the results of the investigation of wing-alone and wing-fuselage combinations employing a wing with the quarter-chord line swept back 35^o, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil section.

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Available abstract

Key concepts: Airfoil, Chord (peer-to-peer), Aspect ratio (aeronautics), Wing, Fuselage, Transonic, NACA airfoil, Lift-to-drag ratio