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Aerodynamic characteristics of a delta wing with leading edge swept back 45 degrees, aspect ratio 4, and NACA 65A006 airfoil section.Transonic-bump method
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Published Year
1940-1949 (1)
Subject
Aerofoils--Testing (1)
Airplanes--Wings, Swept-back (1)
Airplanes--Wings, Triangular (1)
Charts, diagrams, etc (1) *
Drag (Aerodynamics) (1)
Lift (Aerodynamics) (1)
Pitching (Aerodynamics) (1)
Wind tunnel testing (1)
Author
Becht, Robert E. (1) *
Sleeman, William C. (1)
