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Aerodynamic Characteristics of Four Wings of Sweepback Angles 0 Degree, 35 Degrees, 45 Degrees, and 60 Degrees, NACA 65A006 Airfoil Section, Aspect Ratio 4, and Taper Ratio 0.6 in Combination with a Fuselage at High Subsonic Mach Numbers and Mach Num

Arvo A Luoma

Abstract

Report discussing an investigation of the effect of sweepback angle on wing-fuselage characteristics at a subsonic and a supersonic Mach number. Lift, drag, and pitching-moment coefficients, downwash-angle, and total-pressure measurements are all provided.

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Key concepts: Airfoil, Downwash, Angle of attack, Aerodynamics, Fuselage, Lift-to-drag ratio, Pitching moment, NACA airfoil