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

Investigation of the variation with Reynolds number of the base, wave, and skin-friction drag of a parabolic body of revolution (NACA RM-10) at Mach numbers of 1.62, 1.93, and 2.41 in the Langley 9-inch supersonic tunnel

Published Year

• 1940-1949 (1)
• 1950-1959 (1)

Subject

• Aerodynamics, Supersonic (2) *
• Airplanes--Models--Testing (1)
• Airplanes--Models--Wings (1)
• Airplanes--Wings, Triangular (1)
• Base flow (Aerodynamics) (1)
• Body of revolution (1)
• Charts, diagrams, etc (1)
• Drag (Aerodynamics) (1)
• Leading edges (Aerodynamics) (1)
• Reynolds number (1)

Author

• Love, Eugene S. (2) *
• Bromm, August F. (1)
• Coletti, Donald E. (1)

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