Edge matching for unsteady design of turbomachinery (I) Theory and implementation

  • Lu Cheng Ji*
  • , Jiang Chen
  • *Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

Abstract

The edge matching (EM) concerns the spatial relation between a blade trailing edge and the leading edge of the sequent blade row. EM theory and its implementation methods was presented. While EM theory is described first. Two methods of implementing EM, namely spanwise integration and full optimization, are described. Theoretical analysis indicates that EM may improve the aerodynamic, aeroelastic, aeroacoustic and heat transfer performances of turbomachinery by matching phase angles of unsteady flow along the whole span. EM provides a new degree of freedom for turbomachinery design.

Original languageEnglish
Pages (from-to)307-312
Number of pages6
JournalTuijin Jishu/Journal of Propulsion Technology
Volume26
Issue number4
StatePublished - Aug 2005

Keywords

  • Aerodynamic design
  • Blade
  • Edge matching
  • Fluid mechanics
  • Unsteady flow

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