A Lifting-Surface Theory for the Rectangular Wing in Non-Stationary Flow

Author:

Graham J. M. R.

Abstract

SummaryA method of obtaining the load distribution on thin rectangular wings in non-stationary incompressible flow is presented, with particular reference to the problem of gust-induced loading. The method utilises solutions to a Fourier transform of the downwash integral equation, enabling the problem to be expressed in the form of a set of dual integral equations having a series solution. Some values of the overall lift coefficient are computed and compared with values of lift coefficient obtained by collocation methods. The method is easily extendable to subsonic compressible flows.

Publisher

Cambridge University Press (CUP)

Subject

General Engineering

Reference9 articles.

1. Murrow H. N. , Pratt K. G. and 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.

2. Garner H. C. Private Communication.

3. Similarity rules for thin aerofoils in non-stationary subsonic flows

4. Watkins C. E. , Runyan H. L. and Woolston D. S. On the kernel function of the integral equation relating the lift and downwash distributions of oscillating finite wings in subsonic flow. NACA Report 1234, 1955.

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