Abstract
SummaryThe solution to the problem of the loading generated on a two-dimensional thin aerofoil by an incompressible flow whose normal velocity component is of the general form exp [i(λx+/μy — ωt)] is calculated. The method used extends the two-dimensional integral equation solution for the induced vorticity by means of a Chebyshev expansion of part of the kernel function. Thin aerofoil approximations are made throughout, but no collocation procedure, as such, is required.
Publisher
Cambridge University Press (CUP)
Reference6 articles.
1. Söhngen H. Die Lösungen der Integralgleichung und deren Anwendung in der Trag-flügeltheorie. Mathematische Zeitschrift, Band 45 p.245, 1939.
2. Murrow H. N. , Pratt K. G. , Drischler J. A. An application of a numerical technique to lifting-surface theory for calculation of unsteady aerodynamic forces due to continuous sinusoidal gusts on several wing planforms at subsonic speeds. NASA TN D-1501, 1963.
Cited by
80 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献