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Finite Span Wings in Compressible Flow
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.
Date:
September 1956
Creator:
Krasilschchikova, E. A.
System:
The UNT Digital Library