Numerical Simulation of Gas Flow Field with Public Exhaust System of Shipborne Missile

DOI

10.2991/iiicec-15.2015.284How to use a DOI?

Keywords

Vertically Launching; Public Exhaust System; Jet; Numerical Simulation

Abstract

The mathematical model of a vertical launching device was established by simplifying its physical model. Through the method of solving Navier-Stokes equation , the complex internal flow of the exhaust was simulated when the missile keep still in the Vertical Launching System, and the changes of the various parameters of the flow field were analyzed. A deepen understanding of the unsteady flow can be made through the analysis. The work of this paper may offer some reference and gist for research on the public exhaust system of jet flow in a vertical launching system.

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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TY  - CONF
AU  - Mo Liang
AU  - Yi Jiang
PY  - 2015/03
DA  - 2015/03
TI  - Numerical Simulation of Gas Flow Field with Public Exhaust System of Shipborne Missile
BT  - Proceedings of the 2015 International Industrial Informatics and Computer Engineering Conference
PB  - Atlantis Press
SP  - 1287
EP  - 1290
SN  - 2352-538X
UR  - https://doi.org/10.2991/iiicec-15.2015.284
DO  - 10.2991/iiicec-15.2015.284
ID  - Liang2015/03
ER  -