Simulation on launching exhaust field of underwater missile during vertical hot launching

DOI

10.2991/emeit.2012.249How to use a DOI?

Keywords

submarine-launched launching exhaust field Injection

Abstract

The model on launching exhaust field of underwater missile was based on viscous non-stationary compressible phase flow theory. In this paper, a reasonable modeling approach of launching exhaust field was obtained by analyzing whether to consider the vaporization effect. The article also analyzed the pros and cons of water injection program. Analysis showed that the launch barrel temperature decreased significantly with injection. On the other hand, poor exhaust problems might arise with injection, so injection quantity must be controlled. This article provides guidance for the scheme of launch.

Copyright

© 2012, 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  - Ming Yang
AU  - HanPing Wang
AU  - ShiPing Zhao
PY  - 2012/09
DA  - 2012/09
TI  - Simulation on launching exhaust field of underwater missile during vertical hot launching
BT  - Proceedings of the 2nd International Conference on Electronic & Mechanical Engineering and Information Technology (EMEIT 2012)
PB  - Atlantis Press
SP  - 1142
EP  - 1145
SN  - 1951-6851
UR  - https://doi.org/10.2991/emeit.2012.249
DO  - 10.2991/emeit.2012.249
ID  - Yang2012/09
ER  -