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Further verification of nonlinear harmonic method

  • Jun Zhao*
  • , Bao Jie Liu
  • *Corresponding author for this work
  • Beihang University

Research output: Contribution to journal › Article › peer-review

Abstract

A two-dimensional steady, unsteady and nonlinear harmonic method (NHM) RANS code was developed based on Denton steady code. Then the code was used to simulate a two-dimensional transonic compressor cascade by the above three methods and the results were compared on deterministic stress fields, blade surface velocity and other aspects. The comparison indicates that NHM presents high precision on modeling deterministic stresses and mixing-plane treating plays an important role in the simulations. The shortcomings of NHM were also discussed, including main unconquerable origins of modeling error and long computational time.

Original languageEnglish
Pages (from-to)680-686
Number of pages7
JournalHangkong Dongli Xuebao/Journal of Aerospace Power
Volume23
Issue number4
StatePublished - Apr 2008

Keywords

  • Aerospace propulsion system
  • Deterministic stresses
  • Nonlinear harmonic method
  • Unsteady simulation

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