Proceedings of the International Conference on Computer Information Systems and Industrial Applications

The Different Chemical Reaction Model Analysis in Combustion Chamber

Authors
Y.Z Zhang, Z. Li
Corresponding Author
Y.Z Zhang
Available Online June 2015.
DOI
10.2991/cisia-15.2015.241How to use a DOI?
Keywords
solid rocket ramjet; combustion chamber; numerical simulation; chemical reaction model
Abstract

Effective mixing and rapid combustion is very important to the flow field of combustion chamber in solid rocket ramjet. The flow field of combustion chamber in solid rocket ramjet was simulated based on finite rate chemical reaction model and infinite rate chemical reaction model .The result of two kinds of chemical reaction model compared with the experimental result. The result shows that the two kinds of chemical reaction model are feasible, and the calculated result is reasonable.

Copyright
© 2015, the Authors. Published by Atlantis Press.
Open Access
This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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Volume Title
Proceedings of the International Conference on Computer Information Systems and Industrial Applications
Series
Advances in Computer Science Research
Publication Date
June 2015
ISBN
10.2991/cisia-15.2015.241
ISSN
2352-538X
DOI
10.2991/cisia-15.2015.241How to use a DOI?
Copyright
© 2015, the Authors. Published by Atlantis Press.
Open Access
This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

Cite this article

TY  - CONF
AU  - Y.Z Zhang
AU  - Z. Li
PY  - 2015/06
DA  - 2015/06
TI  - The Different Chemical Reaction Model Analysis in Combustion Chamber
BT  - Proceedings of the International Conference on Computer Information Systems and Industrial Applications
PB  - Atlantis Press
SP  - 897
EP  - 898
SN  - 2352-538X
UR  - https://doi.org/10.2991/cisia-15.2015.241
DO  - 10.2991/cisia-15.2015.241
ID  - Zhang2015/06
ER  -