A computational study of leading-edge wall cooling effect on shock wave–boundary layer interaction in forward-facing step
Vinoth Kumar P,
Jayaprakash N Murugan
Abstract:A computational study has been done to understand the effect of leading-edge wall cooling on shock wave–boundary layer interaction. Shock wave–boundary layer interaction is studied over a forward-facing step at supersonic Mach 2.5. The study was carried out using Ansys. The work aims to explore the implementation of wall cooling at the leading edge as a separation control strategy for supersonic forward-facing step-induced flow separation. We use a finite-volume method based on upwind flux difference splitting… Show more
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