An experiment investigation of the aerodynamic characteristic for a multi-wing light antitank missile

Juan Mian Lei*, Jia Sheng Wu

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

3 Citations (Scopus)

Abstract

Based on the aerodynamic configuration of New Javelin light antitank missile, a series of wind tunnel experimental model was designed with the component build-up method. Six-component force experiments were conducted for Mach numbers ranging 0.3-0.5 and angles of attack -1°~15°. The experimental results show that, while the wing number increases from four to eight, the experimental configurations are static stabilization and the normal force and normal overload increase more than 40%, but the increase of zero-lift drag is under 5%. The experimental results also indicate that eight wing configuration maybe is the best configuration.

Original languageEnglish
Pages (from-to)709-711
Number of pages3
JournalBinggong Xuebao/Acta Armamentarii
Volume26
Issue number5
Publication statusPublished - Sept 2005

Keywords

  • Aerodynamic characteristic
  • Aerodynamic configuration
  • Antitank missile
  • Fluid mechanics
  • Wind tunnel experiment

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