MATEC Web Conf.
Volume 139, 20172017 3rd International Conference on Mechanical, Electronic and Information Technology Engineering (ICMITE 2017)
|Number of page(s)||4|
|Published online||05 December 2017|
Numerical simulation of transverse jet flow field under supersonic inflow
1 State Key Laboratory of Laser Propulsion & Application, Space Engineering University, Beijing 101416, China
2 Xichang Satellite Launch Center of China, Xichang Sichuan, 615606
3 Jiuquan Satellite Launch Center of China, Jiuquan Gansu, 732750
* Corresponding author: firstname.lastname@example.org
Transverse jet flow field under supersonic inflow is simulated numerically for studying the characteristic of fuel transverse jet and fuel mixing in scramjet combustion chamber. Comparison is performed between simulated results and the results of references and experiments. Results indicate that the CFD code in this paper is applicable for simulation of transverse jut flow field under supersonic inflow, but in order to providing more effective numerical predictive method, CFD code should be modified through increasing mesh density and adding LES module.
Key words: supersonic inflow; / transverse jet; / fuel mixing; / numerical simulation
© The Authors, published by EDP Sciences, 2017
This is an Open Access article distributed under the terms of the Creative Commons Attribution License 4.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited. (http://creativecommons.org/licenses/by/4.0/).
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