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Effect of Mach and Reynolds Numbers on Maximum Lift Coefficient
Report presenting an investigation of the effects of Mach and Reynolds numbers on the maximum lift coefficient of aircraft. Flight testing was conducted on six airplanes outfitted with measuring tools and flow at various Mach and Reynolds numbers.
Date:
March 28, 1946
Creator:
Spreiter, John R. & Steffen, Paul J.
System:
The UNT Digital Library