A linearized solution for time-dependent velocity potentials near three-dimensional wings at supersonic speeds

John C. Evvard
naca-tn-1699
Sep 1948


A source-distribution method is applied to derive a solution for the time-dependent surface velocity potential of thin finite wings at supersonic speeds. The solution is illustrated by evaluating the upwash over the tip of the arbitrary-plan-boundary wing having a supersonic and subsonic leading edge.

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