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/).
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 -