Graphical method of obtaining theoretical lift distributions on thin wings at supersonic speeds

Clarence B. Cohen, John C. Evvard
naca-tn-1676
Aug 1948


A graphical method is presented for calculating the linearized lift distribution on thin wings at supersonic speed. The technique may be applied to all wing regions except those influenced by interacting flow fields off the wing-plan boundaries.

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http://naca.central.cranfield.ac.uk/reports/1948/naca-tn-1676.pdf