Theoretical study of air forces on an oscillating or steady thin wing in a supersonic main stream
Description:
From Summary: "A theoretical study, based on the linearized equations of motion for small disturbance, is made of the air forces on wings of general plan forms moving forward at a constant supersonic speed. The boundary problem is set up for both the harmonically oscillating and the steady conditions. Two types of boundary conditions are distinguished, which are designated "purely supersonic" and "mixed supersonic." the method is illustrated by applications to a number of examples for both the …
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Date:
June 4, 1947
Creator:
Garrick, I. E. & Rubinow, S. I.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department