NASA NTRS · 19930093836
A flat wing with sharp edges in a supersonic stream
Abstract
A basic treatment is given for the approximate solution of the problem of two-dimensional supersonic flow past a thin wing at small angles of attack. The pressure distribution at the surface, the lifting force, and the wave drag are determined.
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Donov, A E. 1956-03-01. A flat wing with sharp edges in a supersonic stream. https://ntrs.nasa.gov/citations/19930093836
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