A method for the determination of the spanwise load distribution of a flexible swept wing at subsonic speeds

Richard B. Skoog, Harvey H. Brown
naca-tn-2222
Mar 1951


A method is presented for the determination of the spanwise load distribution of a flexible swept wing at subsonic speed. The method is based on a relaxation approach utilizing aerodynamic loadings obtained from previously published work (NACA Rep. 921, 1948) based on Weissinger's simplified lifting-surface theory together with simple beam theory.

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