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An NACA Flight and Wind Tunnel Investigation of Maximum Lift as Affected By Variations of Mach and Reynolds Numbers
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SPREITER, J. and STEFFEN, P., "An NACA Flight and Wind Tunnel Investigation of Maximum Lift as Affected By Variations of Mach and Reynolds Numbers," SAE Technical Paper 460118, 1946, https://doi.org/10.4271/460118.Also In
References
- Spreiter, John R. Steffen, Paul J. Effect of Mach and Reynolds Numbers on the Maximum Lift Coefficient April 1946
- Jacobs, Eastman N. Sherman, Albert Airfoil Section Characteristics as Affected by Variations of the Reynolds Number 1937
- von Karman, Th. Tsien, H. S. Boundary Layer in Compressible Fluids Journal of the Aeronautical Sciences V 6 April 1938 227 232
- von Karman, Th. Millikan, C. B. A Theoretical Investigation of the Maximum Lift Coefficient Journal of Applied Mechanics II 1 March 1935 A-21 A-27
- Goldstein, S. Modern Developments in Fluid Dynamics II Oxford University Press 1938 478 489
- Jacobs, Eastman N. Clay, William C. Characteristics of the NACA 23012 Airfoil from Tests in the Full-Scale and Variable-Density Tunnels 1935
- Platt, Robert C. Turbulence Factors of NACA Wind Tunnels as Determined by Sphere Tests 1936
- Goett, Harry J. Bullivant, W. Kenneth Tests of NACA 0009, 0012, and 0018 Airfoils in the Full-Scale Tunnel 1939
- Doetsch, H. Kramer, M. Systematic Airfoil Tests in the Large Wind Tunnel of the DVL. March 1938
- Richter, G. Sept. 1940