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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 several 6-percent-thick airfoils at angles of attack from 0 to 20 degrees at high subsonic speeds

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

Published Year

• 1940-1949 (3) *

Subject

• Aerofoils--Testing (3) *
• Charts, diagrams, etc (3)
• Wind tunnel testing (3)
• Drag (Aerodynamics) (2)
• Lift (Aerodynamics) (2)
• Aerodynamic load (1)
• Airplanes--Wings, Swept-back (1)
• Airplanes--Wings, Triangular (1)
• Angle of attack (Aerodynamics) (1)
• Flaps (Aerodynamics) (1)
• Hinge moments (Aerodynamics) (1)
• Pitching (Aerodynamics) (1)
• Schlieren photography (1)

Author

• Abbott, Frank T. (1)
• Becht, Robert E. (1)
• Daley, Bernard N. (1)
• Lord, Douglas R. (1)
• Sleeman, William C. (1)
• Underwood, William J. (1)

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