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Research on problem of deterministic stress coupling in transonic compressor

  • Civil Aviation Flight University of China

Research output: Contribution to journalArticlepeer-review

Abstract

Two-dimensional steady/unsteady, and three-dimensional unsteady calculation programs were developed based on three-dimensional steady Denton program. Researches on deterministic stress coupling were conducted on two cases: two-dimensional transonic compressor cascade and three-dimensional single-stages transonic compressor near stall point. It is found that, there are some deviations from time-averaged value of solution and unsteady solution of time-averaged equations when deterministic stresses are applied to coupling processing. The deviation of the coupling error originated from three sources: spatial difference discrete, viscosity correlation terms, mixing-plane processing. In multi-row coupling cases, the influences of mixing-plane are vital. It has a vital effect on the coupling calculation results. The simple mixing-plane processing can't get an ideal effect.

Original languageEnglish
Pages (from-to)2234-2240
Number of pages7
JournalHangkong Dongli Xuebao/Journal of Aerospace Power
Volume30
Issue number9
DOIs
StatePublished - 1 Sep 2015

Keywords

  • Compressor
  • Deterministic stress
  • Time-averaged
  • Transonic
  • Unsteady calculation

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