NASA NTRS · 19930074004
Methods for direct simulation of transition in hypersonic boundary layers
Abstract
An implicit numerical algorithm for the time accurate solution of the compressible Navier-Stokes equations is described. Results for steady flow past a finite flat plate are presented, together with preliminary results for the temporal simulation of second mode instability in a flat plate boundary layer at Mach 4.5.
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Vandervegt, J. J. W., Ferziger, J. H.. 1991-02-01. Methods for direct simulation of transition in hypersonic boundary layers. https://ntrs.nasa.gov/citations/19930074004
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