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

Effects of two leading-edge modifications on the aerodynamic characteristics of a thin low-aspect-ratio delta wing at transonic speeds

Transonic investigation of aerodynamic characteristics of a swept-wing fighter-airplane model with leading-edge droop in combination with outboard chord-extensions and notches

Effects of wing-tip droop on the longitudinal characteristics of two highly swept wing-body combinations at Mach numbers from 0.6 to 1.4

A buffet investigation at high subsonic speeds of wing-fuselage-tail combinations having sweptback wings with NACA 64A thickness distributions, fences, a leading-edge extension, and body contouring

Published Year

• 1940-1949 (1)
• 1950-1959 (4)

Subject

• Charts, diagrams, etc (5)
• Leading edges (Aerodynamics) (5) *
• Airplanes--Models--Testing (4)
• Airplanes--Wings, Swept-back (3)
• Aerodynamics, Transonic (2)
• Airplanes--Models--Wings (2)
• Airplanes--Wings, Triangular (2)
• Wind tunnel testing (2)
• Aerodynamics, Supersonic (1)
• Aeronautics--Research (1)
• Airplanes--Fuselage (1)
• Airplanes--Tail surfaces (1)
• Angle of attack (Aerodynamics) (1)
• Butteting (Aerodynamics) (1)
• Drag (Aerodynamics) (1)
• Fighter planes (1)
• Flaps (Airplanes) (1)
• Stability of airplanes, Longitudinal (1)

Author

• Knechtel, Earl D. (1)
• Lautenberger, J. Walter, (1)
• Lee, George. (1)
• Love, Eugene S. (1)
• Mugler, John P. (1)
• Norton, Harry T., (1)
• Sutton, Fred B. (1)
• Whitcomb, Charles F. (1)

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