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Numerical investigation on starting performance of zero-secondary flow ejectors

  • Ling Zhi Xu*
  • , Xu Xu
  • *Corresponding author for this work
  • Beihang University

Research output: Contribution to journalArticlepeer-review

Abstract

To investigate how the geometry parameters can influence starting performance in zero-secondary flow ejector, flow field of different ejectors were solved by CFD. The numerical simulation results were also applied to analyze ejector typical operation modes, ranging from on-design to off-design point. Results suggest that Ad/At(area ratio of diffuser entrance to nozzle throat) and Ast/Ad(second-throat contraction ratio) are the most important parameters on the ejector performance, and Lst/Dst(ratio of length to diameter second-throat) and Ld/Dd(second-throat location) also greatly influence the performance. The critical starting pressure ratio is increased by increasing Ad/At. When Ast/Ad is higher than second-throat critical contraction ratio, its decrease benefits starting the ejector.

Original languageEnglish
Pages (from-to)204-209+225
JournalTuijin Jishu/Journal of Propulsion Technology
Volume31
Issue number2
StatePublished - Apr 2010

Keywords

  • Ejector
  • Numerical simulation
  • Pressure recovery
  • Shrouded nozzle
  • Starting performance
  • Structure parameter

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