Charts and approximate formulas for the estimation of aeroelastic effects on the loading of swept and unswept wings

Franklin W. Diederich, Kenneth A. Foss
naca-report-1140
1953


Charts and approximate formulas are presented for the estimation of aeroelastic effects on the spanwise lift distribution, lift-curve slope, aerodynamic center, and damping in roll of swept and unswept wings at subsonic and supersonic speeds. Some design considerations brought out by the results of this report are discussed.

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http://naca.central.cranfield.ac.uk/reports/1953/naca-report-1140.pdf