Method for calculating the aerodynamic loading on an oscillating finite wing in subsonic and sonic flow

Harry L. Runyan, Donald S. Woolston
naca-report-1322
Jan 1957


A method is presented for calculating the loading on a finite wing oscillating in subsonic or sonic flow. The method is applicable to any plan form and may be used for determining the loading on deformed wings. The procedure is approximate and requires numerical integration over the wing surface.

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