A general theory of planar disturbances in inviscid parallel shear flows, analogous to thin-wing theory in potential flows, has been developed. Integral relations between surface pressure and deformation are obtained that are similar to, and can be solved by the same numerical methods as those of potential flow. Computed results are shown that illustrate the effects of a model turbulent boundary layer on various lifting and nonlifting surfaces, including an elastic panel in low supersonic flow and airfoil control surface in subsonic flow.
Aerodynamic effects of inviscid parallel shear flows
Aerodynamische Einfluesse auf reibungsfreie, parallele Scherstroemung
AIAA Journal ; 15 , 8 ; 1159-1166
1977
8 Seiten, 21 Bilder, 14 Quellen
Article (Journal)
English
Aerodynamic Effects of Inviscid Parallel Shear Flows
AIAA | 1977
|Modelling Propellers in Inviscid Flows
Online Contents | 2001
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