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Flow measurements near the open surfaces of single circumferential grooves in a low-speed axial compressor

  • Published:2018-07 Issue: Volume:78 Page:531-541
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Liu Le,Nan Xi,Lin Feng

Funder

National Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference23 articles.

1. Passive Endwall Treatments for Enhancing Stability;Hathaway,2007

2. Interaction of Rotor and Casing Treatment Flow in an Axial Single-Stage Transonic Compressor with Circumferential Grooves;Müller,2008

3. Flow mechanism for stall margin improvement due to circumferential casing grooves on axial compressors;Shabbir;J. Turbomach.,2005

4. A novel approach to evaluate the benefits of casing treatment in axial compressors;Legras;Int. J. Rotating Mach.,2012

5. A CFD Study of Circumferential Groove Casing Treatment in a Transonic Axial Compressor;Chen,2010

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