High-order finite-difference schemes for numerical simulation of hypersonic boundary-layer transition

DOI10.1006/jcph.1998.6010zbMath0935.76066OpenAlexW2070780881MaRDI QIDQ1287168

Xiaolin Zhong

Publication date: 9 May 2000

Published in: Journal of Computational Physics (Search for Journal in Brave)

Full work available at URL: https://semanticscholar.org/paper/f639d492d081b4c4c35fc8079f838e981e22f0f2

zbMATH Keywords

Navier-Stokes equationsupwind schemeshypersonic boundary layerlinear wave equationfreestream acoustic disturbanceshigh-order shock-fitting finite-difference methodparabolic leading edgethermo-chemical nonequilibrium

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Direct numerical and large eddy simulation of turbulence (76F65) Reaction effects in flows (76V05) Hypersonic flows (76K05) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

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