Research on vertical launching missile jet flow with jet vane

DOI

10.2991/icmcm-16.2016.22How to use a DOI?

Keywords

Jet vane; jet flow; computational fluid dynamic; deflector.

Abstract

In order to research the impact on the surrounding environment of the high temperature and high pressure jet flow produced in the process of missile vertical launching with jet vane, the structured grids was built, and the computational fluid dynamic model was used to simulate the launching vehicle jet flow. The temperature and pressure contour of the deflector and baffle was obtained. The results shows that the ablation on the deflector was obvious, and the high temperature area was distributed by X shape. By comparing the actual experiment, we found the calculation of the simulation was reasonable, and it provided a reference for the follow study.

Copyright

© 2016, 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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TY  - CONF
AU  - Yongyue Li
AU  - Aolin Zhang
AU  - Chengde Wang
PY  - 2016/12
DA  - 2016/12
TI  - Research on vertical launching missile jet flow with jet vane
BT  - Proceedings of the 2016 7th International Conference on Mechatronics, Control and Materials (ICMCM 2016)
PB  - Atlantis Press
SP  - 108
EP  - 111
SN  - 2352-5401
UR  - https://doi.org/10.2991/icmcm-16.2016.22
DO  - 10.2991/icmcm-16.2016.22
ID  - Li2016/12
ER  -