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Aerodynamic characteristics of a wing with quarter-chord line swept back 35©�, aspect ratio 6, taper ratio 0.6, and NACA 65A006 airfoil section.Transonic-bump method

Published Year

• 1940-1949 (1)

Subject

• Aerodynamics, Transonic (1)
• Airplanes--Fuselage (1)
• Airplanes--WIngs (1)
• Airplanes--Wings (1)
• Drag (Aerodynamics) (1)
• Lift (Aerodynamics) (1)
• Pitching (Aerodynamics) (1)

Author

• Morrison, William D. (1) *
• Sleeman, William C. (1)

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