Reduced order modeling for closed-loop control of three dimensional wakes

Collection of Technical Papers - 3rd AIAA Flow Control Conference

Volumn 2, Issue , 2006, Pages 1101-1118

  Cohen, Kelly ^a,b,c   Siegel, Stefan ^a,b,c   Seidel, Jürgen ^a,b   McLaughlin, Thomas ^a,c,d  

^a UNITED STATES AIR FORCE ACADEMY   (United States)

^b Department of Aeronautics ^*

^c AIAA   (United States)

^d Aeronautics Research Center   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; CLOSED LOOP CONTROL SYSTEMS; COMPUTATIONAL METHODS; FLOW CONTROL; NAVIER STOKES EQUATIONS; OPTIMAL CONTROL SYSTEMS; SENSORS; STOCHASTIC CONTROL SYSTEMS;

COMPUTATIONAL CAPABILITY; OPEN LOOP TECHNIQUES; ORTHOGONAL DECOMPOSITION METHOD;

WAKES;

EID: 33845265034     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-3356     Document Type: Conference Paper

References (42)

1. Gad-el-Hak, M., "Modern Developments in Flow Control", Applied Mechanics Reviews, vol. 49, 1996, pp. 365-379.
2. Cattafesta III, L.N., Williams, D.R., Rowley, C.W., and Alvi, F.S., "Review of Active Control of Flow-Induced Cavity Resonance", AIAA Paper 2003-3567, June 2003.
3. Samimy, M., Debiasi, M., Caraballo, E., E.G., Ozbay, H., Efe, M.O., Yuan, X., DeBonis, J., and Myatt, J.H., "Development of Closed-loop Control for Cavity Flows", AIAA Paper 2003-4258, June 2003.
4. Rapoport, D., Fono, I., Cohen, K., and Seifert, A., "Closed-loop Vectoring Control of a Turbulent Jet Using Periodic Excitation", Journal of Propulsion and Power, Vol. 19, No. 4, 2003, pp. 646-654.
5. Glauser, M., Young, M., Higuchi, H., Tinney, C.E., and Carlson, H., "POD Based Experimental Flow Control on a NACA-4412 Airfoil (Invited), 42nd AIAA Aerospace Sciences Meeting, Reno, Jan. 5-8 2004, AIAA Paper 2004-0574.
6. Tadmor, G., and Banaszuk, A., "Observation feedback control of vortex motion in a recirculation region, IEEE TransControl Sys. Tech., Vol. 10, pp. 749-755.
7. Gillies, E. A., "Low-dimensional Control of the Circular Cylinder Wake", Journal of Fluid Mechanics, Vol. 371, 1998, pp. 157-178.
8. Gerhard, J., Pastoor, M., King, R., Noack, B.R., Dillmann, A., Morzynski, M., Tadmor, G., "Model-based Control of Vortex Shedding using Low-dimensional Galerkin Models", AIAA Paper2003-4262, June 2003.
9. Cohen, K., Siegel S., McLaughlin T., Gillies E., and Myatt, J.,"Closed-loop approaches to control of a wake flow modeled by the Ginzburg-Landau equation", Computers and Fluids, Volume 34, Issue 8, September 2005, pp. 927-949.
10. Cohen, K., Siegel, S., Wetlesen, D., Cameron, J., and Sick, A., "Effective Sensor Placements for the Estimation of Proper Orthogonal Decomposition Mode Coefficients in von Kármán Vortex Street", Journal of Vibration and Control, Vol. 10, No. 12, 1857-1880, December 2004.
11. Cohen, K., D., Siegel, S., Luchtenburg, M., and McLaughlin, T., Seifert, A., "Sensor Placement for Closed-loop Flow control of a 'D' Shaped Cylinder Wake", 2nd AIAA Flow Control Conference, 28 June - 1 July 2004, Portland, Oregon, AIAA-2004-2523.
12. Cohen, K., Siegel S., and McLaughlin T.,"A Heuristic Approach to Effective Sensor Placement for Modeling of a Cylinder Wake", Computers and Fluids, Volume 35, Issue 1, January 2006, pp. 103-120.
13. Siegel S., Cohen, K. and McLaughlin T., 2003, "Feedback Control of a Circular Cylinder Wake in Experiment and Simulation", AIAA Paper 2003-3569, June 2003.
14. Siegel S., Cohen, K., and McLaughlin T., " Low-Dimensional Feedback Control of the von Kármán Vortex Street at a Reynolds number of 100", IUTAM Symposium: Fluid-Structure Interactions, Piscataway, USA, 2-6 June 2003.
15. Cohen K., Siegel S., McLaughlin T., and Gillies E., 2003, "Feedback Control of a Cylinder Wake Low-Dimensional Model", AIAA Journal, Vol. 41, No. 8, August 2003.
16. rd Aerospace Sciences Meeting & Exhibit, Reno NV, AIAA Paper 2005-0141.
17. Enloe, C.L., McLaughlin, T.E., VanDyken, R.D., Kachner, K.D., Jumper, E.J., and Corke, T.C., "Mechanisms and Responses of a Single Dielectric Barrier Plasma Actuator: Plasma Morphology", AIAA Journal, Vol. 42, No. 3, March 2004
18. List, J., McLaughlin, T.E., Byerley, A.R., and Van Dyken, R.D., "Using Plasma to Control Separation on a Linear Cascade Turbine Blade," 41st Aerospace Sciences Meeting & Exhibit, Reno NV, AIAA Paper 2003-1026.
19. Asghar, A., and Jumper, E.J., "Phase Synchronization of Vortex Shedding from Multiple Cylinders using Plasma Actuators," AIAA Paper 2003-1028.
20. Bevan, B., Locke, E., Siegel, S., McLaughlin, T.E., and Cohen, K., "Flow Visualization of Three Dimensional Effects in a Cylinder Wake Flow," APS / DFD Meeting East Rutherford, NJ, 2003
21. Holmes, P., Lumley, J.L., and Berkooz, G., "Turbulence, Coherent Structures, Dynamical Systems and Symmetry", Cambridge University Press, Cambridge, 1996.
22. Sirovich, L., "Turbulence and the Dynamics of Coherent Structures Part I: Coherent Structures", Quarterly of Applied Mathematics, Vol. 45, No. 3, 1987, pp. 561-571.
23. Noack, B.R., Tadmor, G., and Morzynski, M., "Low-dimensional models for feedback flow control. Part I: Empirical Galerkin models", 2nd AIAA Flow Control Conference, 28 Jun -1 Jul 2004, Portland, Oregon, AIAA-2004-2408.
24. Taylor, J.A. and Glauser, M.N., "Towards Practical Flow Sensing and Control via POD and LSE Based Low-Dimensional Tools", Journal of Fluids Engineering, Vol. 126, May 2004, pp.337-345.
25. Stalnov, O., Palei, V., Fono, I., Cohen, K., and Seifert, A., "Experimental Validation of Sensor Placement for Control of a "D" Shaped Cylinder Wake", AIAA-2005-5260, 35th AIAA Fluid Dynamics Conference and Exhibit, Toronto, Canada, June 6-9, 2005.
26. nd Fluid Dynamics Conference and Exhibit, 24-26 June 2002, St. Louis, MO, AIAA Paper 2002-2866.
27. th AIAA Aerospace Meeting and Exhibit, 9-12 January 2006, Reno, Nevada, AIAA Paper 2006-1251.
28. Koopmann, G., "The Vortex Wakes of Vibrating Cylinders at Low Reynolds Numbers", Journal of Fluid Mechanics, Vol. 28 Part 3, 1967, pp. 501-512.
29. McLaughlin, T., B. Felker, J. Avery and C. Enloe, "Further Experiments in Cylinder Wake Modification With Dielectric Barrier Discharge Forcing", 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 9-12, 2006, AIAA-2006-1409.
30. th AIAA Aerospace Sciences Meeting, Reno, Jan. 9-12 2006.
31. rd AIAA Aerospace Sciences Meeting, Reno, Jan. 10-13 2005.
32. th AIAA Aerospace Sciences Meeting, Reno, Nevada, January 9-12, 2006.
33. Gillies, E. A., "Low-Dimensional Characterization and Control of Non-Linear Wake Flows," Ph.D. Dissertation, Faculty of Engineering, Univ. of Glasgow, Glasgow, Scotland, U.K., June 1995.
34. Noack, B.R., Afanasiev, K., Morzynski, M., and Thiele, F., "A hierarchy of low-dimensional models for the transient and post-transient cylinder wake" J. Fluid Mechanics, vol. 497, 2003, pp. 335-363.
35. Cybenko, G.V., "Approximation by Superpositions of a Sigmoidal function", Mathematics of Control, Signals and Systems, Vol. 2, 1989, pp. 303-314.
36. Haykin, S., Neural Networks - A comprehensive foundation. Second Edition, Prentice Hall, New Jersey, USA, 1999.
37. Nørgaard, M, Ravn, O., Poulsen, N. K., and Hansen, L. K., "Neural Networks for Modeling and Control of Dynamic Systems", Springer-Verlag, London, UK, 2000.
38. Seidel, J., Siegel, S., Cohen, K., and McLaughlin, T., "Simulations of Flow Control of the Wake behind an Axisymmetric Bluff Body", 3rd AIAA Flow Control Conference. San Francisco, California, 5-8 June 2006, AIAA-2006-3490.
39. Cohen, K., Siegel, S., Seidel, J., and McLaughlin, T., "Neural Network Estimator for Low-Dimensional Modeling of a Cylinder Wake", 3rd AIAA Flow Control Conference, San Francisco, California, 5-8 June 2006, AIAA-2006-3491.
40. Siegel, S., Cohen, K., and McLaughlin, T, "Experimental Variable Gain Feedback Control of a Circular Cylinder Wake", 2nd AIAA Flow Control Conference, 28 June - 1 July 2004, Portland, Oregon, AIAA-2004-2611.
41. Siegel S., Cohen K., Seidel, J., and McLaughlin T, "Two Dimensional Simulations of a Feedback Controlled D-Cylinder Wake", AIAA-2005-5019, 35th AIAA Fluid Dynamics Conference and Exhibit, Toronto, Canada, June 6-9, 2005.
42. th AIAA Aerospace Sciences Meeting, Reno, Nevada, January 9-12, 2006.