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Dual-code solution procedure for efficient computing equilibrium hypersonic axisymmetric laminar flows

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Publication:2853482
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DOI10.1016/j.ast.2007.03.007zbMath1273.76256OpenAlexW2069365871MaRDI QIDQ2853482

Ramin Kamali-Moghadam, Vahid Esfahanian, Kazem Hejranfar

Publication date: 22 October 2013

Published in: Aerospace Science and Technology (Search for Journal in Brave)

Full work available at URL: http://www.sciencedirect.com/science/article/pii/S1270963807000788


zbMATH Keywords

dual codeshock fitting techniqueblunt-body configurationsequilibrium hypersonic flows


Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Finite difference methods applied to problems in fluid mechanics (76M20) Hypersonic flows (76K05)


Related Items (3)

Application of a shock-fitted spectral collocation method for computing transient high-speed inviscid flows over a blunt nose ⋮ Deneb: an open-source high-performance multi-physical flow solver based on high-order DRM-DG method ⋮ Numerical study of shock-disturbances interaction in hypersonic inviscid flows with real gas effects using high-order WENO scheme






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