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Linear and nonlinear stability of plane stagnation flow

Published online by Cambridge University Press:  21 April 2006

M. J. Lyell
Affiliation:
Department of Aerospace Engineering, University of Southern California, Los Angeles, California 90089-0192
P. Huerre
Affiliation:
Department of Aerospace Engineering, University of Southern California, Los Angeles, California 90089-0192

Abstract

Plane stagnation flow is known to be linearly stable to three-dimensional perturbations. The purpose of this theoretical study is to show that the same flow can be destabilized if fluctuation levels are sufficiently high. In the present formulation, finite-amplitude disturbances are expanded in terms of the eigenfunctions pertaining to the linear stability of potential stagnation flow and a Galerkin method is used to derive the nonlinear amplitude equations coupling the different modes. Two- and three-mode interaction models based on the least-damped eigenfunctions of linear theory indicate that three-dimensional fluctuations can be triggered to grow exponentially above a certain critical intensity. The existence of such a threshold is in qualitative agreement with experimental studies of the secondary vortices arising in flows past blunt bodies.

Type
Research Article
Copyright
© 1985 Cambridge University Press

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