NASA NTRS · 19930093847
Finite Span Wings in Compressible Flow
Abstract
Equations are developed using the source distribution method for the velocity potential function and pressure on thin wings in steady and unsteady motion. Closed form solutions are given for harmonically oscillating wings of general plan form including the effect of the wing wake. Some useful examples are presented in an appendix for arrow, semielliptical, and hexagonal plan form wings.
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Krasilschchikova, E A. 1956-09-01. Finite Span Wings in Compressible Flow. https://ntrs.nasa.gov/citations/19930093847
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