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Control of Transonic Shock Positions
Published online by Cambridge University Press: 15 August 2002
Abstract
We wish to show how the shock position in a nozzle could be controlled. Optimal control theory and algorithm is applied to the transonic equation. The difficulty is that the derivative with respect to the shock position involves a Dirac mass. The one dimensional case is solved, the two dimensional one is analyzed .
Keywords
- Type
- Research Article
- Information
- ESAIM: Control, Optimisation and Calculus of Variations , Volume 8: A tribute to JL Lions , 2002 , pp. 907 - 914
- Copyright
- © EDP Sciences, SMAI, 2002
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