Theoretical Prediction of Pressure Distributions on Nonlifting Airfoils at High Subsonic Speeds
Description:
"Theoretical pressure distributions on nonlifting circular-arc airfoils in two-dimensional flows with high subsonic free-stream velocity are found by determining approximate solutions, through an iteration process, of an integral equation for transonic flow proposed by Oswatitsch. The integral equation stems directly from the small-disturbance theory for transonic flow. This method of analysis possesses the advantage of remaining in the physical, rather than the hodograph, variable and can be a…
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Date:
November 19, 1953
Creator:
Spreiter, John R. & Alksne, Alberta
Item Type:
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Partner:
UNT Libraries Government Documents Department