Computational flowfield analyses of hypersonic problems with reacting boundary layer

A mathematical model able to deal with high temperature gas effects in hypersonic flow fields is presented. In order to assess this model, four typical hypersonic applications are considered. The numerical results are presented and compared with experimental data. The effects of the catalyticity of the materials on the heat fluxes are also highlighted.

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Year of publication:	2010
Authors:	Bucchignani, Edoardo ; Pezzella, Giuseppe
Published in:	Mathematics and Computers in Simulation (MATCOM). - Elsevier, ISSN 0378-4754. - Vol. 81.2010, 3, p. 656-669
Publisher:	Elsevier
Subject:	Computational fluid dynamics \| Aerospace \| Aerothermodynamics

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Type of publication:	Article
Source:	RePEc - Research Papers in Economics

Persistent link: https://www.econbiz.de/10010749303