Simulation and optimize design for deflector plate of the Vehicle mounted Vertically Thermal Launched missile

Shao Zhen Yu*, Yi Jiang, Yan Li Ma, Yan Yan Ma, Bo Wei Liu

*Corresponding author for this work

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

1 Citation (Scopus)

Abstract

In this dissertation, academic analysis of the influence to deflector plate in gas jet field of a Vehicle-mounted Vertically Thermal Launched missile as well as simulation study. The finite volume method, a fully structured grid, three-dimensional N-S equation is used for the numerical simulation of the process during the missile launching. The two main factors: temperature and forces on the launcher is the standard we test a launching system. The temperature on the position we test will rise with the decreasing length of the deflector. Especially, when the length is near to the potential core, the temperature changed greatly. Also, the angles of the deflector under the same length have less impacted on the temperature field. However, the force on the deflector would be change greater than the temperature with the change of angles.

Original languageEnglish
Title of host publicationIISME2012
Pages579-583
Number of pages5
DOIs
Publication statusPublished - 2012
Event2012 2nd International Conference on Industry, Information System and Material Engineering, IISME 2012 - Wuhan, China
Duration: 17 Mar 201218 Mar 2012

Publication series

NameAdvanced Materials Research
Volume459
ISSN (Print)1022-6680

Conference

Conference2012 2nd International Conference on Industry, Information System and Material Engineering, IISME 2012
Country/TerritoryChina
CityWuhan
Period17/03/1218/03/12

Keywords

  • Coupled numerical simulation
  • Deflector plate
  • Finite volume method
  • Gas jet
  • Vehicle-mounted missile

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