The dsign of jet vane of thrust vector control system

Liu Min Wang, Bo Mo

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

3 Citations (Scopus)

Abstract

According to the thrust vector control requirements of fast turn of the missile vertical launching, this design carries out the force analysis of the jet vane which is in the high temperature and high speed jet stream, and calculates the normal force which is generated by the vane, thus calculates the area of the jet vane. At the same time, according to the aerodynamic theory and engineering experience, this design analyzes and calculates the aerodynamic shape of the jet vane. As a result, two types of jet vane are designed. On this basis, through the use of a fluid analysis software FLUENT, both of the two jet vane are simulated and get a jet vane which is more suitable for the practical applications.

Original languageEnglish
Title of host publicationManufacturing Engineering and Automation II
Pages1743-1747
Number of pages5
DOIs
Publication statusPublished - 2012
Event2012 International Conference on Manufacturing Engineering and Automation, ICMEA 2012 - Guangzhou, China
Duration: 16 Nov 201218 Nov 2012

Publication series

NameAdvanced Materials Research
Volume591-593
ISSN (Print)1022-6680

Conference

Conference2012 International Conference on Manufacturing Engineering and Automation, ICMEA 2012
Country/TerritoryChina
CityGuangzhou
Period16/11/1218/11/12

Keywords

  • Engineering calculation
  • Fluid analysis
  • Jet vane
  • Thrust vector control

Fingerprint

Dive into the research topics of 'The dsign of jet vane of thrust vector control system'. Together they form a unique fingerprint.

Cite this