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Axisymmetric equivalent of S-shaped transition duct with struts in axial compression systems

  • Xiaobin Que
  • , Anping Hou*
  • , Sheng Zhou
  • *Corresponding author for this work
  • Beihang University

Research output: Contribution to journalArticlepeer-review

Abstract

Thick struts which intersect an S-shaped transition duct in an axial compression system tend to cause blockage in the flow passage and significantly influence the performance of the duct. As there are no design rules available for them, design of a transition duct with struts involves three dimensional numerical optimization, which is rather complicated. To simplify the issue in the design phase, an axisymmetric equivalent method which can reduce the problem to two dimensional problem is established. First, the theoretical concepts of axisymmetric equivalent method are presented based on the influence of struts on the pressure field in the duct. Then, the main features of the flow field in the equivalent duct and the strutted duct are compared through numerical calculation. It is shown that the endwall pressure distribution of the two ducts agrees well, and that they exhibit similar loss variation features, which both indicate that the equivalent duct is capable of capturing the major influence of struts. Finally, the equivalent method is applied to the optimization of a baseline strutted duct with separation in the strut-hub area due to high local diffusion. The optimized duct is found to have removed the separation completely, and decreased the loss by 41.6%.

Original languageEnglish
Pages (from-to)1715-1722
Number of pages8
JournalHangkong Xuebao/Acta Aeronautica et Astronautica Sinica
Volume31
Issue number9
StatePublished - Sep 2010

Keywords

  • Axisymmetric equivalent
  • Fan/compressor
  • S-shape transition duct
  • Strut

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