Generalized Indical Forces on Deforming Rectangular Wings in Supersonic Flight
Description:
"A method is presented for determining the time-dependent flow over a rectangular wing moving with a supersonic forward speed and undergoing small vertical distortions expressible as polynomials involving spanwise and chordwise distances. The solution for the velocity potential is presented in a form analogous to that for steady supersonic flow having the familiar "reflected area" concept discovered by Evvard. Particular attention is paid to indicial-type motions and results are expressed in te…
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Date:
June 30, 1954
Creator:
Lomax, Harvard; Fuller, Franklyn B. & Sluder, Loma
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department