Active Separation Control with Pulsed Jets in a Critically Loaded Compressor Cascade
Author:
Affiliation:
1. Berlin Institute of Technology
2. Rolls-Royce Deutschland Ltd & Co KG
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-4252
Reference22 articles.
1. Flow control opportunities in gas turbine engines
2. Highly Loaded Axial Flow Compressors: History and Current Developments
3. 3Bright, M. M., Culley, D. E., Braunscheidel, E. P., and Welch, G. E. “Closed Loop Active Flow Separation Detection and Control in a Multistage Compressor,” Tech. Rep. NASA TM-2005-213553, NASA Glenn Research Center, 2005.
4. Experimental Investigation of Flow Control in Compressor Cascades
5. Influence of Active Methods of Flow Control on Compressor Blade Cascade Flow
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1. Adaptive Control in an Axial Turbofan: Model-Free Implementation with Short Response Time;AIAA Journal;2011-07
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