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Recovery Process from Rotating Stall in a Fan

  • Published:2011-11 Issue:6 Volume:27 Page:1161-1168
  • ISSN:0748-4658
  • Container-title:Journal of Propulsion and Power
  • language:en
  • Short-container-title:Journal of Propulsion and Power

Author:

Choi Minsuk1,Vahdati Mehdi1

Affiliation:

1. Imperial College London, London, England SW7 2AZ, United Kingdom

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Cited by 14 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Analysis on spike-type rotating stall in transonic axial compressor by dynamic mode decomposition;Aerospace Science and Technology;2022-12

2. Numerical investigations on the key contributing factor and flow features of compressor stall hysteresis;Aerospace Science and Technology;2022-02

3. A Method of Stall and Surge Prediction in Axial Compressors Based on Three-Dimensional Body-Force Model;Journal of Engineering for Gas Turbines and Power;2022-01-04

4. Numerical analysis of the effects of circumferential groove casing suction in a counter-rotating axial flow compressor;Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy;2020-09-10

5. Investigation of stall recovery potential in a transonic compressor rotor;Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy;2020-04-04
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