Notes on the Effect of Surface Distortions on the Drag and Critical Mach Number of Airfoils
Description:
"The effect of two-dimensional bumps and surface waviness on the pressure distribution over airfoils is considered. It is shown that the results of the analysis may be useful in evaluating the effects of accidental or intended surface distortions on the drag and critical Mach number of airfoils" (p. 1).
Date:
September 1943
Creator:
Allen, H. Julian
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department