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Wind tunnel free-flight test for multi-bodies separation

  • Zenghui Jiang*
  • , Wei Song
  • , Quyao Jia
  • , Nong Chen
  • *Corresponding author for this work
  • China Aerospace Science and Technology Corporation

Research output: Contribution to journalArticlepeer-review

Abstract

The technique of wind tunnel free-flight test for multi-bodies separation, a more complicated wind tunnel special test technique, has been developed. With this new technique, the multi-bodies separation process of the aircraft can be simulated more accurately, and the whole separation process can be recorded by the high-speed camera. The technique is introduced in detail, include the principle, characteristic, test model design, similarity criteria, and test apparatus. Based on the different characteristic and application fields, the technique of wind tunnel free-flight test for multi-bodies separation can be classified as stage separation, submunition separating from dispenser and multi-bodies separation with additional constraints. Detailed specification is given for each type. The test images and flight path curves of each separated-body are presented. According to the above presentation, the technique of wind tunnel free-flight test for multi-bodies separation, can be well understand and easily adopted by more researchers engaged in wind tunnel test.

Original languageEnglish
Pages (from-to)581-586
Number of pages6
JournalKongqi Donglixue Xuebao/Acta Aerodynamica Sinica
Volume34
Issue number5
DOIs
StatePublished - 1 Oct 2016
Externally publishedYes

Keywords

  • Multi-bodies separation
  • Stage separation
  • Submunition disperse
  • Wind tunnel free-flight test

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