Extensions of Extremum-Seeking Control to Improve the Aerodynamic Performance of Axial Turbomachines

Author:

Wiederhold Olaf1,King Rudibert1,Noack Bernd1,Neuhaus Lars2,Neise Wolfgang3,Enghardt Lars2,Swoboda Marius4

Affiliation:

1. Berlin Institute of Technology

2. DLR, German Aerospace Research Center

3. German Aerospace Center DLR

4. Rolls Royce Deutschland Ltd & Co

Publisher

American Institute of Aeronautics and Astronautics

Reference29 articles.

1. Robust and Adaptive Closed-loop Control of Separated Shear Flows

2. 4Braunscheidel, E. P., Culley, D.E., Zaman, K.B.M.Q. "Application of Synthetic Jets to Reduce Stator flow Separation in a LowSpeed Axial Compressor",46thAIAAAerospaceSciencesMeetingandExhibit,Reno,Nevada,2008.

3. 5McLean, J., Crouch, J., Stoner, R., Sakurai, S., Seidel, G., Feifel, W., Rush, H. "Study of the Application of Separation ControlbyUnsteadyExcitation to Civil TransportAircraft", Technical Report NASA/CR-1999-209338, 1999.

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