Numerical study on combustion of H2—O2in a supersonic reactive expansion in a nozzle

DOI10.1080/13647830500407665zbMath1098.80005OpenAlexW1998195084MaRDI QIDQ3378015

M. Pezeshki, N. Saraje Mehdizadeh, S. Tabe Jamaat

Publication date: 29 March 2006

Published in: Combustion Theory and Modelling (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1080/13647830500407665

zbMATH Keywords

expansionnozzlenumerical studysupersonic combustionH\(_{2}\)--O\(_{2}\)

Mathematics Subject Classification ID

Combustion (80A25)

Cites Work

• Flux vector splitting of the inviscid gasdynamic equations with application to finite-difference methods

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