Numerical calculation on the influence of missile exhaust plume with mechanical properties to the double-launch box

Jing Li, Yi Jiang

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

Abstract

The adverse impact of the exhaust plume on the inner wall of the vertical launch box and the former friable lid of the adjacent launch box is a common phenomenon, which causes the deformation or damage of the launch container. By using the three-dimensional unsteady numerical simulation, discrete phase model and multicomponent model, the change of the pressure and temperature with time on many monitoring sites are analyzed. The results show that the pressure and the temperature on the edge of the inner wall significantly rise over time after 0.2s. The pressure on the centerline of the inner wall rises over time after 0.2s but the temperature gradually decreases. The maximum pressure on the former friable lid of the adjacent launch box peaks at 0.54s. The conclusion can be regarded as a theoretical reference for engineering application.

Original languageEnglish
Title of host publicationAdvanced Research on Mechanical and Electronic Information Engineering II
PublisherTrans Tech Publications Ltd.
Pages101-105
Number of pages5
ISBN (Print)9783038351702
DOIs
Publication statusPublished - 2014
Event2nd International Conference on Mechanical and Electronic Engineering, ICMEE 2014 - Wuhan, China
Duration: 21 Jun 201422 Jun 2014

Publication series

NameAdvanced Materials Research
Volume978
ISSN (Print)1022-6680
ISSN (Electronic)1662-8985

Conference

Conference2nd International Conference on Mechanical and Electronic Engineering, ICMEE 2014
Country/TerritoryChina
CityWuhan
Period21/06/1422/06/14

Keywords

  • Exhaust plume
  • Former friable lid
  • Internal wall of launching container
  • Numerical simulation

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