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Author

R. C. Mehta

Bio: R. C. Mehta is an academic researcher from Vikram Sarabhai Space Centre. The author has contributed to research in topics: Mach wave & Boundary layer. The author has co-authored 1 publications.

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Journal ArticleDOI
01 Mar 1988
TL;DR: In this paper, the unsteady, compressible Navier-Stokes equations in Reynolds-averaged variables are solved for a shock wave turbulent boundary layer interaction for the free stream Mach number 37 and Reynolds number 8202×106 computation is performed using MacCormack's explicit-implicit finite difference scheme with 42×42 grid points.
Abstract: The unsteady, compressible Navier-Stokes equations in Reynolds-averaged variables are solved for a shock wave turbulent boundary layer interaction For the free stream Mach number 37 and Reynolds number 8202×106 computation is performed using MacCormack's explicit-implicit finite difference scheme with 42×42 grid points It is found that the peak heating amplification correlation agrees well with computational results