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Active Control of Compressor Instability and Surge by Stator Blades Adjustment

  • Published:2003-03 Issue:2 Volume:19 Page:312-317
  • ISSN:0748-4658
  • Container-title:Journal of Propulsion and Power
  • language:en
  • Short-container-title:Journal of Propulsion and Power

Author:

Schobeiri M. T.1,Attia M.1

Affiliation:

1. Texas A&M University, College Station, Texas 77843-3123

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

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

Cited by 8 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. Study of Vibrational and Mechanical Properties of Pre-Tensioned Banded Stator Blades of an Axial Compressor;Proceedings of Higher Educational Institutions. Маchine Building;2022-03

2. Control method of adaptive delay wind tunnel based on total pressure characteristics;2021 China Automation Congress (CAC);2021-10-22

3. The Effect of Trailing Edge Clearance in Suppressing Hub-Corner Stall;Energies;2019-01-15

4. Modeling the Compressor Component, Design and Off-Design;Gas Turbine Design, Components and System Design Integration;2017-06-07

5. Modeling the Compressor Component, Design and Off-Design;Turbomachinery Flow Physics and Dynamic Performance;2012
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