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Comparison of computation models for simulation of turbomachinery rotor-stator interactions

  • Beihang University

Research output: Contribution to journalArticlepeer-review

Abstract

Comparative study on three Fourier-based time-domain unsteady computation methods, including the shape-correction phase shift method, space-time gradient method and harmonic balance method, was carried out by simulation of two typical kinds of rotor-stator interactions, i.e.: wake-blade interactions and shock-blade interactions. Differences and relations between these computation methods were investigated in detail, and their computational accuracy and speed were also analyzed. The results indicate that three methods can resolve the unsteady flow details well. Compared with the conventional time-marching method, the computational speed of these methods can be enhanced from several to dozens of times, making these methods applicable to daily design process.

Original languageEnglish
Pages (from-to)528-537
Number of pages10
JournalHangkong Dongli Xuebao/Journal of Aerospace Power
Volume32
Issue number3
DOIs
StatePublished - 1 Mar 2017

Keywords

  • Harmonic balance method
  • Rotor-stator interactions
  • Shape-correction phase shift method
  • Space-time gradient method
  • Turbomachinery

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