Experimental development of a reduced-order model for flow separation control

Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting

Volumn 20, Issue , 2006, Pages 15136-15143

  Ausseur, Julie M ^a,c,d   Pinier, Jeremy T ^a,c,d   Glauser, Mark N ^a,c,d   Higuchi, Hiroshi ^a,c,d   Carlson, Henry ^a,b,d,e  

^a SYRACUSE UNIVERSITY   (United States)

^b Clear Science Corp   (United States)

^c Syracuse University   (United States)

^d AIAA   (United States)

^e Clear Science Corp   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

LINEAR STOCHASTIC ESTIMATION (LSE); PROPER ORTHOGONAL DECOMPOSITION;

AIRFOILS; DYNAMICAL SYSTEMS; PRESSURE MEASUREMENT; TURBULENT FLOW; VELOCITY MEASUREMENT;

FLOW CONTROL;

EID: 34250902889     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (17)

1. Lumley, J. L., "The Structure of Inhomogeneous Turbulent Flows.", Atm. Turb. And Radio Wave Prop., Nauka, Moscow and Toulouse, France, eds. Yaglom and Tatarsky, 1967, pp. 166-178.
2. Ausseur, J., Pinier, J., Glauser, M., Higuchi, H., Tinney, C., "Proportional Closed-loop Feedback Control of Separation", AIAA Journal paper in preparation.
3. Aubry, N., Holmes, P., Lumley, J. L. & Stone, E., "The dynamics of coherent structures in the wall region of a turbulent boundary layer", J. Fluid Mech., 1988, vol. 192, pp. 115-173.
4. Ukeiley, L. S., Cordler, L., Manceau, R., Delville, J, Glauser, M. N., Bonnet, J-P., "Examination of large-scale structures in a turbulent plane mixing layer. Part 2. Dynamical system model", J. Fluid Mech., 2001, vol. 441, pp 67-108.
5. Ricaud, F., "Study of acoustic sources Identification from the coupling between the near field pressure and the instantaneous organization of the mixing layer jet", Ph.D. thesis, Faculté des Sciences Fondamentales et Appliquées, University of Poitiers, France, 2003, pp. 137-139.
6. Ausseur, J., Pinier, J., "Towards Closed-Loop Feedback Control of the Flow over NACA-4412 Airfoil", 43rd AIAA Aerospace Sciences Meeting and Exhibit, AIAA 2005-0343, Reno, NV, 2005.
7. Glauser, M. N., Higuchi, H., Ausseur, J. M. & Pinier, J. T., "Feedback Control of Separated Flows (Invited).", 2nd AIAA Flow Control Conference, AIAA 2004-2521, Portland, OR, 2004.
8. Carlson, H., "Linear Estimators for Controller Design", Clear Science Corp., 2004.
9. Adrian, R. J., "On the Role of Conditional Averages in Turbulence Theory", Turbulence in Liquids: Proceedings of the Fourth Biennial Symposium on Turbulence in Liquids (1975), Science Press, eds. Zakin, J. & Patterson, G., 1977, pp. 323-332.
10. Cole, D. R., Glauser, M. N. & Guezennec, Y. G., "An Application of Stochastic Estimation to the Jet Mixing Layer.", Phys. Fluids, Vol. 4, No. 1, 1991, pp. 192-194.
11. Bonnet, J. P., Cole, D. R., Delville, J., Glauser, M. N. & Ukeiley, L. S., "Stochastic Estimation and Proper Orthogonal Decomposition: Complementary Techniques for Identifying Structure.", Experiments in Fluids, Vol. 17, 1994, pp. 307-314.
12. Taylor, J. A. & Glauser, M. N., "Towards Practical Flow Sensing arid Control via POD and LSE Based Low-Dimensional Tools.", ASME Fluids Engineering Division Summer Meeting, Montreal, ASME Paper FEDSM2002-31416, 2002, and J. Fluids Eng., Vol. 126, No. 3, 2004, pp. 337-345.
13. a.
14. Sirovich, L., "Turbulence and the dynamics of coherent structures. Parts 1, 2 & 3", Quarterly of Applied Mathematics, XLV, 3, 1987, pp. 561-590.
15. Naguib, A., Wark, C. & Juckenhoefel, O., "Stochastic Estimation and Flow Sources Associated with Surface Pressure Events in a Turbulent Boundary Layer.", Physics of Fluids, Vol. 13, No. 9, 2001, pp. 2611-2616.
16. N. Murray & L. Ukeiley, "Estimating the Shear Layer Velocity Field Above an Open Cavity from Surface Pressure Measurements", AIAA 2002-2866, 2002.
17. Glauser, M., Young, M., Higuchi, H., Tinney, C. & Carlson, H., "POD Based Experimental Flow Control on a NACA-4412 Airfoil (Invited).", 42nd AIAA Aerospace Sciences Meeting and Exhibit, AIAA 2004-0575, Reno, NV, 2004.