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Effects of Mach number up to 0.34 and Reynolds number up to 8,000,000 on the maximum lift coefficient of a wing of NACA 66-series airfoil sections

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

NACA 65-series compressor rotor performance with varying annulus-area ratio, solidity, blade angle, and Reynolds number and comparison with cascade results

Published Year

• 1950-1959 (3)

Subject

• Reynolds number (3) *
• Aerodynamics, Supersonic (1)
• Aerofoils (1)
• Airplanes--Models--Wings (1)
• Axial flow compressors--Blades (1)
• Base flow (Aerodynamics) (1)
• Body of revolution (1)
• Cascades (Fluid dynamics) (1)
• Compressors--Performance (1)
• Drag (Aerodynamics) (1)
• Lift (Aerodynamics) (1)
• Mach number (1)

Author

• Ashby, George C. (1)
• Bromm, August F. (1)
• Coletti, Donald E. (1)
• Erwin, John R. (1)
• Fitzpatrick, James E. (1)
• Furlong, G. Chester. (1)
• Love, Eugene S. (1)
• Schulze, Wallace M. (1)

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