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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
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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)
