Simulation and optimization of flow control strategies for novel high-lift configurations

AIAA Journal

Volumn 47, Issue 5, 2009, Pages 1145-1157

  Meunier, M ^a,b  

^a ONERA   (France)

^b Applied Aerodynamics Department   (France)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC EFFICIENCY; DESIGN VARIABLES; DIMENSIONAL REDUCTION; EFFICIENT CONTROL; FLOW CONTROL STRATEGY; HIGH-LIFT AIRFOILS; IN-DEPTH ANALYSIS; KRIGING; LANDING CONDITIONS; OPTIMIZATION ALGORITHMS; PROBLEM FORMULATION; SIMULATION AND OPTIMIZATION;

AIRFOILS; FLOW CONTROL; OPTIMIZATION; REGRESSION ANALYSIS;

FLOW SIMULATION;

EID: 67649233173     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.38245     Document Type: Article

References (59)

1. Gad-el-Hak, M., Flow Control: Passive, Active and Reactive Flow Management, Cambridge Univ. Press, Cambridge, England, U.K., 2000.
2. Kral, L. D., "Active Flow Control Technology," American Society of Mechanical Engineers, Fluids Engineering Div., http://files.asme.org/ Divisions/FED/16309.pdf [retrieved 26 Feb. 2009].
3. Greenblatt, D., and Wygnanski, I., "The Control of Flow Separation by Periodic Excitation," Progress in Aerospace Sciences, Vol. 36, No. 7, 2000, pp. 487-545. doi:10.1016/S0376-0421(00)00008-7
4. McLean, J. D., Crouch, J. D., Stoner, R. C., Sakurai, S., and Seidel, G. E., "Study of the Application of Separation Control by Unsteady Excitation to Civil Transport Aircraft," NASA Langley Research Center, CR-1999-209338, Hampton, VA, 1999.
5. Meunier, M., and Brunet, V., "High-Lift Devices Performance Enhancement Using Mechanical and Air-Jet Vortex Generators," Journal of Aircraft, Vol. 45, No. 6, 2008, pp. 2049-2061. doi:10.2514/1.36836
6. Seifert, A., Bachar, T., Koss, D., Shepshelovich, M., and Wygnanski, I., "Oscillatory Blowing: A Tool to Delay Boundary-Layer Separation," AIAA Journal, Vol. 31, No. 11, Nov. 1993, pp. 2052-2060. doi:10.2514/3.49121
7. Nishri, B., and Wygnanski, I., "Effects of Periodic Excitation on Turbulent Flow Separation from a Flap," AIAA Journal, Vol. 36, No. 4, Apr. 1998, pp. 547-556. doi:10.2514/2.428
8. Darabi, A., and Wygnanski, I., "Active Management of Naturally Separated Flow over a Solid Surface. Part 1. The Forced Reattachment Process," Journal of Fluid Mechanics, Vol. 510, 2004, pp. 105-129. doi: 10.1017/S0022112004009231
9. Darabi, A., and Wygnanski, I., "Active Management of Naturally Separated Flow over a Solid Surface. Part 2. The Separation Process," Journal of Fluid Mechanics, Vol. 510, 2004, pp. 131-144. doi:10.1017/S0022112004009243
10. Becker, R., King, R., Petz, R., andNitsche, W.,"AdaptiveClosed-Loop Separation Control on a High-Lift Configuration Using Extremum Seeking," AIAA Journal, Vol. 45, No. 6, June 2007, pp. 1382-1392. doi:10.2514/1.24941
11. Hassan, A., "Improving Flap Aerodynamics Using Oscillatory Jet Control," 21 st AIAA Applied Aerodynamics Conference, Orlando, FL, AIAA Paper 2003-3664, June 2003.
12. Dandois, J., Garnier, E., and Sagaut, P., "Numerical Simulation of Active Separation Control by Synthetic Jet," Journal of Fluid Mechanics, Vol. 574, Mar. 2007, pp. 25-58. doi:10.1017/S0022112006003995
13. Greenblatt, D., "Dual Location Separation Control on a Semi-Span Wing," 23rd AIAA Applied Aerodynamics Conference, Toronto, CAN, AIAA Paper 2005-5085, June 2005.
14. Greenblatt, D., and Washburn, A. E., "Influence of Finite Span and Sweep on Active Flow Control Efficacy," AIAA Paper 2007-4275, 25th AIAA Applied Aerodynamics Conference, Miami, FL, 25-28 June 2007.
15. Galbraith, M., "Numerical Simulations of a High-Lift Airfoil Employing Active Flow Control," 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, AIAA Paper 2006-0147, 9-12 Jan. 2006.
16. Kiedaisch, J., Nagib, H., and Demanett, B., "Active Flow Control Applied to High-Lift Airfoils Utilizing Simple Flaps," 3rd AIAA Flow Control Conference, San Francisco, AIAA Paper 2006-2856, June 2006.
17. Shmilovich, A., and Yadlin, Y., "Flow Control for the Systematic Buildup of High Lift Systems," 3rd AIAA Flow Control Conference, San Francisco, AIAA Paper 2006-2855, June 2006.
18. Nagib, H., Kiedaisch, J., Reinhard, P., and Demanett, B., "Control Techniques for Flows with Large Separated Regions: A New Look at Scaling Parameters," 3rd AIAA Flow Control Conference, San Francisco, AIAA Paper 2006-2857, June 2006.
19. Seifert, A., and Pack, L., "Effects of Sweep on Active Separation Control at High Reynolds Numbers," Journal of Aircraft, Vol. 40, No. 1, Jan.-Feb. 2003, pp. 120-126. doi:10.2514/2.3066
20. Nagib, H., Kiedaisch, J., Reinhard, P., and Demanett, B., "Active Flow Control for High Lift Airfoils: Separation versus Circulation Control," 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, AIAA Paper 2007-1119, Jan. 2007.
21. Kiedaisch, J., Demanett, B., Reinhard, Paul, and Nagib, H., "Active Flow Control for High Lift Airfoils: Dynamic Flap Actuation," 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, AIAA Paper 2007-1120, Jan. 2007.
22. Pack Melton, L., Schaeffler, N. W., Yao, C.-S., and Seifert, A., "Active Control of Flow Separation from Supercritical Airfoil Leading-Edge Flap Shoulder," Journal of Aircraft, Vol. 42, No. 5, Sept.-Oct. 2005, pp. 1142-1149. doi:10.2514/l.10294
23. Pack Melton, L., Yao, C.-S., and Seifert, A., "Active Control of Separation from the Flap of a Supercritical Airfoil," AIAA Journal, Vol. 44, No. 1, Jan. 2006, pp. 34-41. doi:10.2514/l.12225
24. Pack Melton, L., Yao, C.-S., and Seifert, A., "Application of Excitation from Multiple Locations on a Simplified High-Lift System," 2nd AIAA Flow Control Conference, Portland, OR, AIAA Paper 2004-2324, 2004.
25. Khodadoust, A., and Washburn, A., "Active Control of Flow Separation on a High-Lift System with Slotted Flap at High Reynolds Number," 25th Applied Aerodynamics Conference, Miami, FL, AIAA Paper 2007-4424, June 2007.
26. Khodadoust, A., and Shmilovich, A., "High Reynolds Number Simulations of Distributed Active Flow Control for a High-Lift System," 25th Applied Aerodynamics Conference, Miami, FL, AIAA Paper 2007-4423, June 2007.
27. Smith, A. M. O., "High-Lift Aerodynamics," Journal of Aircraft, Vol. 12, No. 6, 1975, pp. 501-530. doi: 10.2514/3.59830
28. Duvigneau, R., and Visonneau, M., "Simulation and Optimization of Stall Control for an Airfoil with a Synthetic Jet," Aerospace Science and Technology, Vol. 10, Feb. 2006, pp. 279-287. doi:10.1016/j.ast.2006.01. 002
29. Huang, L., Huang, P., LeBeau, R., and Hauser, T., "Optimization of Airfoil Flow Control Using a Genetic Algorithm with Diversity Control," Journal of Aircraft, Vol. 44, No. 4, July-Aug. 2007, pp. 1337-1349. doi:10.2514/1.27020
30. Jeong, S., Murayama, M., and Yamamoto, K., "Efficient Optimization Design Method Using Kriging Model," Journal of Aircraft, Vol. 42, No. 2, Mar.-Apr. 2005, pp. 413-419. doi:10.2514/1.6386
31. Jouhaud, J.-C., Sagaut, P., Montagnac, M., and Laurenceau, J., "A Surrogate-Model Based Multidisciplinary Shape Optimization Method with Application to a 2D Subsonic Airfoil," Computers and Fluids, Vol. 36, No. 3, Mar. 2007, pp. 520-529. doi:10.1016/j.compfluid.2006.04.001
32. Meunier, M., "Simulation and Optimization of Flow Control Strategies for Novel High-Lift Configurations," 25th AIAA Applied Aerodynamics Conference, Miami, FL, AIAA Paper 2007-4276, 2007.
33. McKay, M. D., Beckman, R. J., and Conover, W. J., "A Comparison of Three Methods for Selecting Values of Input Variables in the Analysis of Output from a Computer Code," Technometrics, Vol. 21, No. 2, May 1979, pp. 239-245. doi: 10.2307/1268522
34. Swiler, L., Slepoy, R., and Giunta, A., "Evaluation of Sampling Methods in Constructing Response Surface Approximations," 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Newport, RI, AIAA Paper 2006-1827, May 2006.
35. Cambier, L., and Veuillot, J.-P., "Status of the elsA CFD Software for Flow Simulation and Multidisciplinary Applications," 46th AIAA Aerospace Sciences Meeting and Exhibits, Reno, NV, AIAA Paper 2008-0664, Jan. 2008.
36. Jameson, A., Schmidt, W., and Turkel, E., "Numerical Simulation of the Euler Equation by Finite Volume Methods Using Runge-Kutta Time Stepping Schemes," 14th AIAA Fluid and Plasma Dynamics Conference, Palo-Alto, CA, AIAA Paper 1981-1259, June 1981.
37. Spalart, P., and Allmaras, S., "A One Equation Turbulence Model for Aerodynamic Flows," La Recherche Aerospatiale, Vol. l, No. 5,1994, pp. 5-21.
38. Moens, F., "ONERA-RANS Activities Carried Out for Eurolift W. P. 2.1," ONERA Rept. RT 81/03631 DAAP, Feb. 2003.
39. Orr, M. J. L., "Recent Advances in Radial Basis Function Networks," Inst. for Adaptive and Neural Computation, Edinburgh Univ., Edinburgh, Scotland, U.K., http://www.anc.ed.ac.uk/rbf/papers/re-cad.ps
40. Sacks, J., Welch, W. J., Mitchell, T. J., and Wynn, H. P., "Design and Analysis of Computer Experiments," Statistical Science, Vol. 4, No. 4, 1989, pp. 409-435. doi:10.1214/ss/l177012413
41. Liu, J.-L., "Novel Taguchi-Simulated Annealing Method Applied to Airfoil and Wing Planform Optimization," Journal of Aircraft, Vol. 43, No. 1, Jan.-Feb. 2006, pp. 102-109. doi:10.2514/l.13234
42. Rasheed, K., "GADO: A Genetic Algorithm for Continuous Design Optimization," Ph.D. Thesis, Department of Computer Science, Rutgers Univ., New Brunswick, NJ, 1998.
43. Dargel, G., and Schnieder, H., "GARTEUR AD (AG08) Final Report," GARTEUR High Lift Action Group, Rept. TP043 Nov. 1989.
44. Jones, D., Schonlau, M., and Welch, W., "Efficient Optimization of Expensive Black-Box Functions," Journal of Global Optimization, Vol. 13, No. 4, 1998, pp. 455-492. doi:10.1023/A:1008306431147
45. Manie, F., Piccin, O., and Ray, J.-P., "Test Report of the 2D Model Ml in the ONERA F1 Wind Tunnel," GARTEUR High Lift Action Group, Rept. TP041, Oct. 1989.
46. Wilcox, D., Turbulence Modeling for CFD, 2nd ed., DCW Industries, La Cañada, CA, 2004.
47. Jones, W. P., and Launder, B. E., "The Prediction of Laminarization with a 2-Equation Model of Turbulence," International Journal of Heat andMass Transfer, Vol. 15, No. 2, 1971, pp. 301-314.
48. Menter, F. R., "Two-Equation Eddy-Viscocity Turbulence Models for Engineering Applications," 23rd Fluid Dynamics, Plasmadynamics and Laser Conference, Orlando, FL, AIAA Paper 1993-2906, July 1993.
49. Gear, C. W., Numerical Initial Value Problems in Ordinary Differential Equations, Prentice-Hall, Upper Saddle River, NJ, 1971.
50. Lawrence, C., Zhou, J., and Tits, A., "User's Guide for CFSQP Ver. 2.5: A C Code for Solving (Large Scale) Constrained Nonlinear (Minimax) Optimization Problems, Generating Iterates Satisfying All Inequality Constraints," Inst. for Systems Research, Univ. of Maryland, TR-94-16rl, College Park, MD, 1997.
51. Carrier, G., Single and Multi-Point Aerodynamic Optimizations of a Supersonic Transport Aircraft Wing Using Optimization Strategies Involving Adjoint Method and Genetic Algorithm, European Research Community on Flow Turbulence and Combustion, Las Palmas, Spain, Apr. 2006.
52. Meckesheimer, M., Booker, A., Barton, R., and Simpson, T., "Computationally Inexpensive Metamodel Assessment Strategies," AIAA Journal, Vol. 40, No. 10, Oct. 2002, pp. 2053-2060. doi:10.2514/2.1538
53. Joslin, R. D., and Jones, G. S., Applications of Circulation Control Technology, Progress in Astronautics and Aeronautics Series, Vol. 214, AIAA, Reston, VA, 2006.
54. Abramson, J., and Rogers, E., "High Speed Characteristics of Circulation Control Airfoils," 21st Aerospace Sciences Meeting and Exhibit, Reno, NV, AIAA Paper 1983-0265, Jan. 1983.
55. Sobol', I. M., "Global Sensitivity Indices for Non Linear Mathematical Models and Their Monte Carlo Estimates," Mathematics and Computers in Simulation, Vol. 55, No. 1-3, 2001, pp. 271-280. doi:10.1016/S0378-4754(00)00270-6
56. Nash, J. F., "Non-Cooperative Games," Annals of Mathematics and Artificial Intelligence, Vol. 54, No. 2, Sept. 1951, pp. 286-295.
57. Wang, J., Wu, Y., and Periaux, J., "Combinatorial Optimization Using Genetic Algorithms and Game Theory for High Lift Configuration in Aerodynamics," 41st Aerospace Sciences Meeting and Exhibit, Reno, NV, AIAA Paper 2003-0295, Jan. 2003.
58. Wygnanski, I., Chen, C., and Zakharin, B., "On the Parameters Governing Fluidic Control of Separation and Circulation," 46th Aerospace Sciences Meeting and Exhibit, Reno, NV, AIAA Paper 2008-0629, Jan. 2008.
59. Loth, J. L., "Applications of Circulation Control Technology: Advantages of Combining BLC Suction with Circulation Control High-Lift Generation," Progress in Astronautics and Aeronautics, Vol. 214, AIAA, Reston, VA, 2006, pp. 3-21.