Flexible multi-body dynamics simulation of cold state axial-symmetric vectoring exhaust nozzle

Han Ping Wang*, Yu Bing Zhang, Ming Yang

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

5 Citations (Scopus)

Abstract

The crucial parts of axial-symmetric vectoring exhaust nozzle(AVEN) were meshed into flexible bodies with solid-shell elements. A flexible multi-body dynamics model of AVEN was built based on MSC.ADAMS command batch processing technique and tree-shape parametric technique. A part of contact constraints in the dynamics model were simplified with point-curve constraints to reduce the computational size. By means of simulation of shaking and swinging movement of the AVEN on normal temperature condition, the loading and dynamic characteristics of the mechanism were achieved. Provided an important reference for virtual design and virtual experiment of AVEN.

Original languageEnglish
Pages (from-to)2427-2432
Number of pages6
JournalHangkong Dongli Xuebao/Journal of Aerospace Power
Volume26
Issue number11
Publication statusPublished - Nov 2011

Keywords

  • Aero-engine
  • Axial-symmetric vectoring exhaust nozzle(AVEN)
  • MSC.ADAMS software
  • Multi-body dynamics
  • Virtual prototype

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