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Investigations at supersonic speeds of 22 triangular wings representing two airfoil sections for each of 11 apex angles

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 (2) *

Subject

• Airplanes--Wings, Triangular (2) *
• Charts, diagrams, etc (2)
• Aerodynamics, Supersonic (1)
• Aerofoils--Testing (1)
• Airplanes--Models--Testing (1)
• Airplanes--Models--Wings (1)
• Airplanes--Wings, Swept-back (1)
• Drag (Aerodynamics) (1)
• Leading edges (Aerodynamics) (1)
• Lift (Aerodynamics) (1)
• Pitching (Aerodynamics) (1)
• Wind tunnel testing (1)

Author

• Becht, Robert E. (1)
• Love, Eugene S. (1)
• Sleeman, William C. (1)

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