E-Book, Englisch, Band 95, 442 Seiten
Reihe: Notes on Numerical Fluid Mechanics and Multidisciplinary Design
King Active Flow Control
1. Auflage 2007
ISBN: 978-3-540-71439-2
Verlag: Springer Berlin Heidelberg
Format: PDF
Kopierschutz: 1 - PDF Watermark
Papers contributed to the Conference "Active Flow Control 2006", Berlin, Germany, September 27 to 29, 2006
E-Book, Englisch, Band 95, 442 Seiten
Reihe: Notes on Numerical Fluid Mechanics and Multidisciplinary Design
ISBN: 978-3-540-71439-2
Verlag: Springer Berlin Heidelberg
Format: PDF
Kopierschutz: 1 - PDF Watermark
This book contains contributions presented at the Active Flow Control 2006 conference, held September 2006, at the Technische Universität Berlin, Germany. It contains a well balanced combination of theoretical and experimental state-of-the-art results of Active Flow Control. Coverage combines new developments in actuator technology, sensing, robust and optimal open- and closed-loop control and model reduction for control.
Autoren/Hrsg.
Weitere Infos & Material
1;Preface;6
2;Table of Contents;10
3;The Taming of the Shrew: Why Is It so Difficult to Control Turbulence?;13
4;Actuators;37
4.1;Electromagnetic Control of Separated Flows Using Periodic Excitation with Different Wave Forms;38
4.2;Pulsed Plasma Actuators for Active Flow Control at MAV Reynolds Numbers;53
4.3;Experimental and Numerical Investigations of Boundary- Layer Influence Using Plasma- Actuators;67
4.4;Designing Actuators for Active Separation Control Experiments on High- Lift Configurations;80
4.5;Closed-Loop Active Flow Control Systems: Actuators;96
5;State Estimation and Feature Extraction;114
5.1;State Estimation of Transient Flow Fields Using Double Proper Orthogonal Decomposition ( DPOD);115
5.2;A Unified Feature Extraction Architecture;129
6;Air Foils;144
6.1;Control of Wing Vortices;145
6.2;Towards Active Control of Leading Edge Stall by Means of Pneumatic Actuators;160
6.3;Computational Investigation of Separation Control for High- Lift Airfoil Flows;181
6.4;Steady and Oscillatory Flow Control Tests for Tilt Rotor Aircraft;198
7;Cavities;216
7.1;Reduced-Order Model-Based Feedback Control of Subsonic Cavity Flows – An Experimental Approach;217
7.2;Supersonic Cavity Response to Open-Loop Forcing;236
8;Bluff Bodies;250
8.1;Active Drag Control for a Generic Car Model;251
8.2;Continuous Mode Interpolation for Control-Oriented Models of Fluid Flow;264
9;Turbomachines and Combustors;283
9.1;Active Management of Entrainment and Streamwise Vortices in an Incompressible Jet;284
9.2;Active Control to Improve the Aerodynamic Performance and Reduce the Tip Clearance Noise of Axial Turbomachines with Steady Air Injection into the Tip Clearance Gap;296
10;Optimal Flow Control and Numerical Studies;310
10.1;Drag Minimization of the Cylinder Wake by Trust- Region Proper Orthogonal Decomposition;311
10.2;Flow Control on the Basis of a FEATFLOW-MATLAB Coupling;327
10.3;On the Choice of the Cost Functional for Optimal Vortex Reduction for Instationary Flows;341
10.4;Flow Control with Regularized State Constraints;355
11;Closed-Loop Flow Control;369
11.1;Feedback Control Applied to the Bluff Body Wake;370
11.2;Active Blade Tone Control in Axial Turbomachines by Flow Induced Secondary Sources in the Blade Tip Regime;392
11.3;Phase-Shift Control of Combustion Instability Using ( Combined) Secondary Fuel Injection and Acoustic Forcing;409
11.4;Vortex Models for Feedback Stabilization of Wake Flows;423
12;Keyword Index;438




