Impulsive Injection for Compressor Stator Separation Control
Author:
Publisher
American Institute of Aeronautics and Astronautics
Reference7 articles.
1. Turbine Separation Control Using Pulsed Vortex Generator Jets
2. The Fluid Dynamics of LPT Blade Separation Control Using Pulsed Jets
3. Active Flow Separation Control of a Stator Vane Using Embedded Injection in a Multistage Compressor Experiment
4. The Influence of Shrouded Stator Cavity Flows on Multistage Compressor Performance
Cited by 3 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. Stability Improvement of a High-Pressure Ratio Centrifugal Compressor by Flow Injection;Journal of Aerospace Engineering;2020-11
2. Closed-loop active flow control of repetitive disturbances in a linear stator cascade;2018 Flow Control Conference;2018-06-24
3. Separation control with endwall corner jet in a high-speed compressor cascade;Journal of Thermal Science and Technology;2017
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