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Aerodynamic characteristics of a wing with quarter-chord line swept back 45 degrees, aspect ratio 4, taper ratio 0.3, and NACA 65A006 airfoil section.Transonic-bump method

Published Year

• 1940-1949 (1)

Subject

• Airplane--Wings, Swept-back (1)
• Charts, diagrams, etc (1)
• Drag (Aerodynamics) (1)
• Lift (Aerodynamics) (1)
• Pitching (Aerodynamics) (1)

Author

• King, Thomas J. (1)
• Myers, Boyd C. (1) *

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