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On the stability of plane shocks

Published online by Cambridge University Press:  29 March 2006

William K. Van Moorhem
Affiliation:
Sibley School of Mechanical and Aerospace Engineering, Cornell University, Itheca, New York 14850 Present address: Department of Mechanical Engineering, The University of Utah, Salt Lake City, Utah 84112, USA.
A. R. George
Affiliation:
Sibley School of Mechanical and Aerospace Engineering, Cornell University, Itheca, New York 14850

Abstract

The stability of perturbed normal shock waves is considered. Shock perturbations depend directly upon the disturbances in the flow adjacent to the shock. In the present paper an initially stationary shock is assumed to be perturbed by acoustic waves reaching it from the downstream side. This case corresponds to the situation occurring in shock diffraction or reflexion. Two-dimensional problems of this type have been investigated previously, both analytically and experimentally. These previous analytic results have, in all cases, indicated that the perturbations of the shock decay with time as $t^{\frac{3}{2}}$, while experimentally both t½ and $t^{\frac{3}{2}}$ decays have been observed. It is demonstrated in the present investigation that, when waves are continuously generated at a point or points behind the shock, a t½ decay of the shock perturbations will occur, corresponding to the decay of the incident waves. However, when the source of waves is located only at the shock, as in a diffraction problem, $t^{-\frac{3}{2}}$ decay occurs owing to the cancellation, to lowest order, of the incident wave by its reflexion from the shock. These results explain the divergence between theory and experiment in this area, since the experiments giving the slower decay contained a source of waves behind the shock.

It is concluded that shock stability can only be considered in the context of the type of disturbances incident upon the shock.

Type
Research Article
Copyright
© 1975 Cambridge University Press

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