Viswanath, PR (1988) Shock-wave-turbulent-boundary-layer interaction and its control - A survey of recent developments. In: IN: Developments in fluid mechanics and space technology (A89-50001 22-34, Bangalore,India.
Full text not available from this repository.Abstract
This paper presents an overview of some of the recent developments that have taken place in the understanding, prediction and control of two- dimensional shock-wave-turbulent-boundary-layer interaction at high speeds. Following a brief description of the upstream influence phenomena, detailed discussions of incipient and fully separated flows at supersonic and transonic speeds are presented. A brief account of certain gross unsteady features of shock-separated flows is given next. Typical examples demonstrating the current ability to predict these complex flows are also included. Finally, a review of techniques using suction and tangential blowing for controlling shock-separated flows is presented. (Author)
Item Type: | Conference or Workshop Item (Paper) |
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Uncontrolled Keywords: | Vacuum; Fluid mechanics; Dimensions; Blowing;Boundary layer control;Separated flow;Shock wave interaction;supersonic flow; Transonics;Airfoils;Control surfaces;suction;Turbomachinery |
Subjects: | AERONAUTICS > Aerodynamics |
Depositing User: | M/S ICAST NAL |
Date Deposited: | 17 Oct 2006 |
Last Modified: | 24 May 2010 04:21 |
URI: | http://nal-ir.nal.res.in/id/eprint/3002 |
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