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Numerical study on inlet angle of guide vane in recess vaned casing treatment

  • Published:2019-10 Issue: Volume:93 Page:105323
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Chen Xiangyi,Chu Wuli,Zhang Haoguang,Li Xiangjun

Funder

National Natural Science Foundation of China

NPU's Exchange Funding

National Science and Technology Major Project

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference39 articles.

1. Flow phenomena in compressor casing treatment;Smith;J. Eng. Gas Turbines Power,1984

2. Stall margin improvement by casing treatment—its mechanism and effectiveness;Takata;J. Eng. Power,1977

3. A fundamental criterion for the application of rotor casing treatment;Greitzer;J. Fluids Eng.,1979

4. Self-recirculating casing treatment concept for enhanced compressor performance;Hathaway,2002

5. Stall margin enhancement of a novel casing treatment subjected to circumferential pressure distortion;Dong;Aerosp. Sci. Technol.,2018
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