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Investigation of a simple device for preventing separation due to shock and boundary-layer interaction

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

Two-dimensional low-speed cascade investigation of NACA compressor blade sections having a systematic variation in mean-line loading

Factors affecting the maximum lift-drag ratio at high supersonic speeds

Flutter at very high speeds

Published Year

• 1950-1959 (5) *

Subject

• Aerofoils (5) *
• Charts, diagrams, etc (3)
• Lift (Aerodynamics) (2)
• Aerodynamic heating (1)
• Aerodynamics, Hypersonic (1)
• Aerodynamics, Supersonic (1)
• Aeroelasticity (1)
• Airplanes--Models--Wings (1)
• Axial flow compressors--Blades (1)
• Boundary layer (1)
• Cascades (Fluid dynamics) (1)
• Compressors--Blades (1)
• Drag (Aerodynamics) (1)
• Flutter (Aerodynamics) (1)
• Mach number (1)
• Mathematics (1)
• Reynolds number (1)
• Shock waves (1)
• Turbulence (1)
• Vortex generators (1)

Author

• Donaldson, Coleman duP. (1)
• Dunning, Robert W. (1)
• Emery, James C. (1)
• Erwin, John R. (1)
• Fitzpatrick, James E. (1)
• Furlong, G. Chester. (1)
• McLellan, Charles H. (1)
• Morgan, Homer G. (1)
• Runyan, Harry L. (1)
• Savage, Melvyn. (1)

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