Simplified approach for control of rotating stall. I - Theoretical development

Author:

Badmus O. O.1,Chowdhury S.1,Eveker K. M.1,Nett C. N.1,Rivera C. J.1

Affiliation:

1. Georgia Institute of Technology, Atlanta, Georgia 30332

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

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

Cited by 13 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. Robust Surge Avoidance Control for a Low Pressure Compressor of a Turbojet Engine;Journal of Intelligent & Robotic Systems;2012-08-01

2. Stall inception and its control in an axial flow fan under dynamic inflow distortion;Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy;2009-12-28

3. Benefits of Active Compressor Stability Management on Turbofan Engine Operability;Journal of Engineering for Gas Turbines and Power;2009-04-14

4. A Stochastic Model for a Compressor Stability Measure;Journal of Engineering for Gas Turbines and Power;2006-11-17

5. Compressor Surge: A Limit Detection and Avoidance Problem;AIAA Guidance, Navigation, and Control Conference and Exhibit;2005-06-19

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