1950•NASA STI Repository (National Aeronautics and Space Administration)Requires access
Aerodynamic Characteristics of a Wing with Quarter-chord Line Swept Back 45 Degrees, Aspect Ratio 6, Taper Ratio 0.6, and NACA 65A009 Airfoil Section
Kenneth P Spreemann, William D Morrison, Thomas B Pasteur
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Abstract
From Introduction: This paper presents the results of the investigation of the wing-alone and wing-fuselage configurations employing a wing with the quarter-chord line swept back 45^o, aspect ratio 4, taper ratio 0.3, and an NACA 65A006 airfoil section parallel to the stream.