Abstract
Passive control shock-boundary layer studies, both theoretical and experimental, are reviewed in this paper. The first paper in this area was published in 1983. Since then there have been programmes of research in U.S.A., Germany and U.K. to understand the concept of passive shock wave boundary layer control and to predict the effect of such a control on the aerodynamic forces on an aerofoil. This review shows that the application of passive control in transonic flow can reduce drag, increase lift and reduce unsteady pressures on an aerofoil.
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