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Aerodynamic Characteristics of a Wing with Quarter-chord Line Swept Back 45 Degrees, Aspect Ratio 4, Taper Ratio 0.6, and NACA 65A006 Airfoil Section : Transonic-bump Method

Kenneth W Goodson, Joseph Weil

Abstract

Report discussing a particular wing-body combination that is part of a larger investigation to determine the lift, drag, pitching moment, and root bending moments for various configurations. Information about the aerodynamic characteristics at the tail plane is also provided.

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Available abstract

Key concepts: Airfoil, Chord (peer-to-peer), Wing, Pitching moment, Aerodynamic center, Aerodynamics, Aspect ratio (aeronautics), Lift-to-drag ratio