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Test of NACA 66,2-116, a =0.6 airfoil section fitted with pressure balanced and slotted flaps for the wing of the XP-63 airplane

Aerodynamic characteristics of a delta wing with leading edge swept back 45 degrees, aspect ratio 4, and NACA 65A006 airfoil section.Transonic-bump method

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

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 (4) *

Subject

• Drag (Aerodynamics) (4) *
• Lift (Aerodynamics) (4)
• Charts, diagrams, etc (3)
• Pitching (Aerodynamics) (3)
• Aerofoils--Testing (2)
• Wind tunnel testing (2)
• Aerodynamic load (1)
• Aerodynamics, Transonic (1)
• Airplane--Wings, Swept-back (1)
• Airplanes--Fuselage (1)
• Airplanes--WIngs (1)
• Airplanes--Wings (1)
• Airplanes--Wings, Swept-back (1)
• Airplanes--Wings, Triangular (1)
• Flaps (Aerodynamics) (1)
• Hinge moments (Aerodynamics) (1)

Author

• Sleeman, William C. (2)
• Abbott, Frank T. (1)
• Becht, Robert E. (1)
• King, Thomas J. (1)
• Morrison, William D. (1)
• Myers, Boyd C. (1)
• Underwood, William J. (1)

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