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

Ming Yang; Han Ping Wang; Shi Ping Zhao

doi:10.2991/emeit.2012.249

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

Ming Yang^*, Han Ping Wang, Shi Ping Zhao

^*Corresponding author for this work

School of Aerospace Engineering

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

2 Citations (Scopus)

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.

Original language	English
Title of host publication	Proceedings of the 2nd International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2012
Publisher	Atlantis Press
Pages	1142-1145
Number of pages	4
ISBN (Print)	9789078677604
DOIs	https://doi.org/10.2991/emeit.2012.249
Publication status	Published - 2012
Event	2012 2nd International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2012 - Shenyang, Liaoning, China Duration: 26 Sept 2012 → 28 Sept 2012

Publication series

Name	Proceedings of the 2nd International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2012

Conference

Conference	2012 2nd International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2012
Country/Territory	China
City	Shenyang, Liaoning
Period	26/09/12 → 28/09/12

Keywords

Submarine-launched launching exhaust field Injection

Access to Document

10.2991/emeit.2012.249

Cite this

Yang, M., Wang, H. P., & Zhao, S. P. (2012). Simulation on launching exhaust field of underwater missile during vertical hot launching. In Proceedings of the 2nd International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2012 (pp. 1142-1145). (Proceedings of the 2nd International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2012). Atlantis Press. https://doi.org/10.2991/emeit.2012.249

Yang, Ming ; Wang, Han Ping ; Zhao, Shi Ping. / Simulation on launching exhaust field of underwater missile during vertical hot launching. Proceedings of the 2nd International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2012. Atlantis Press, 2012. pp. 1142-1145 (Proceedings of the 2nd International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2012).

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title = "Simulation on launching exhaust field of underwater missile during vertical hot launching",

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.",

keywords = "Submarine-launched launching exhaust field Injection",

author = "Ming Yang and Wang, {Han Ping} and Zhao, {Shi Ping}",

year = "2012",

doi = "10.2991/emeit.2012.249",

language = "English",

isbn = "9789078677604",

series = "Proceedings of the 2nd International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2012",

publisher = "Atlantis Press",

pages = "1142--1145",

booktitle = "Proceedings of the 2nd International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2012",

note = "2012 2nd International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2012 ; Conference date: 26-09-2012 Through 28-09-2012",

}

Yang, M, Wang, HP & Zhao, SP 2012, Simulation on launching exhaust field of underwater missile during vertical hot launching. in Proceedings of the 2nd International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2012. Proceedings of the 2nd International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2012, Atlantis Press, pp. 1142-1145, 2012 2nd International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2012, Shenyang, Liaoning, China, 26/09/12. https://doi.org/10.2991/emeit.2012.249

Simulation on launching exhaust field of underwater missile during vertical hot launching. / Yang, Ming; Wang, Han Ping; Zhao, Shi Ping.
Proceedings of the 2nd International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2012. Atlantis Press, 2012. p. 1142-1145 (Proceedings of the 2nd International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2012).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

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T1 - Simulation on launching exhaust field of underwater missile during vertical hot launching

AU - Yang, Ming

AU - Wang, Han Ping

AU - Zhao, Shi Ping

PY - 2012

Y1 - 2012

N2 - 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.

AB - 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.

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DO - 10.2991/emeit.2012.249

M3 - Conference contribution

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SN - 9789078677604

T3 - Proceedings of the 2nd International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2012

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BT - Proceedings of the 2nd International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2012

PB - Atlantis Press

T2 - 2012 2nd International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2012

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Yang M, Wang HP, Zhao SP. Simulation on launching exhaust field of underwater missile during vertical hot launching. In Proceedings of the 2nd International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2012. Atlantis Press. 2012. p. 1142-1145. (Proceedings of the 2nd International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2012). doi: 10.2991/emeit.2012.249

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

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