Reduced order modeling of limit-cycle oscillation for aeroelastic systems

ASME International Mechanical Engineering Congress and Exposition, Proceedings

Volumn , Issue , 2002, Pages 13-24

  Beran, Philip S ^a   Lucia, David J ^a   Pettit, Chris L ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; EULER EQUATIONS; MECHANICAL ENGINEERING; NONLINEAR EQUATIONS; TECHNICAL PRESENTATIONS;

AEROELASTIC MODELS; AEROELASTIC SYSTEM; COMPUTATIONAL COSTS; COUPLED SYSTEMS; DEGREES OF FREEDOM; GALERKIN APPROXIMATIONS; JACOBIANS; LIMIT CYCLE OSCILLATIONS; LOW RANK; NONLINEAR PANELS; ORDER ANALYSIS; ORDER FORMS; PROPER ORTHOGONAL DECOMPOSITIONS; RAPID ANALYSIS; REDUCED ORDER; REDUCED ORDER MODELS; REDUCED-ORDER MODELING; SECOND ORDERS; TIME STEP;

AEROELASTICITY;

EID: 78249242089     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (28)

1. Bendiksen, O. O. and Davis, G. A., "Nonlinear Traveling Wave Flutter of Panels in Transonic Flow," AIAA Paper 1995-1486, 1995.
2. Beran, P. S. and Morton, S. A., "Continuation Method for Calculation of Transonic Airfoil Flutter Boudnaries," Journal of Guidance, Control and Dynamics, Vol. 20, No. 6, December 1997, pp. 1165-1171.
3. Beran, P. S., "A Domain-Decomposition Method for Airfoil Flutter Analysis," AIAA Paper 99-0098, January 1998.
4. Beran, P. S., "Computation of Limit-Cycle Oscillation Using a Direct Method," AIAA Paper 99-1462, April 1999.
5. Beran, P. S., Huttsell, L. J., Buxton, B. J., Noll, C., and Osswald, G., "Computational Aeroelasticity Techniques for Viscous Flow," CEAS/AIAA/ICASE/NASA Langley International Forum on Aeroelasticity and Structural Dynamics, Williamsburg, VA, June 1999.
6. Beran, P. and Silva, W., "Reduced-Order Modeling: New Approaches for Computational Physics," January 2001.
7. Beran, P. S. and Pettit, C. L., "Prediction of Nonlinear Panel Response Using Proper Orthogonal Decomposition," AIAA Paper 2001-1292, April 2001.
8. Cunningham, A. M., "The Role of Non-Linear Aerodynamics in Fluid-Structure Interactions," AIAA Paper 98-2423, 1998.
9. Dobbs, S. K., Miller, G. D., and Stevenson, J. R., "Self Induced Oscillation Wind Tunnel Test of a Variable Sweep Wing," Proceedings of the AIAA/ASME/ASCE/AHS 26th Structures, Structural Dynamics and Materials Conference, Orlando, FL, April 15-17, AIAA Paper 85-0739-CP, 1985.
10. Dowell, E. H., "Nonlinear Oscillations of a Fluttering Plate," AIAA Journal, Vol. 4, No. 7, July 1966, pp. 1267-1275.
11. Dowell, E. H., "Nonlinear Oscillations of a Fluttering Plate. II." AIAA Journal, Vol. 5, October 1967, pp. 1856-1862.
12. Gordnier, R. E. and Melville, R. B., "Accuracy Issues for Transonic Wing Flutter Using 3-D Navier-Stokes," Proceedings of the 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Long Beach, CA, AIAA Paper 98-1729-CP, April 1998.
13. Gordnier, R. E. and Visbal, M. R., "Development of a Three-Dimensional Viscous Aeroelastic Solver for Nonlinear Panel Flutter," AIAA Paper 2000-2337, June 2000.
14. Hall, K. C., Thomas, J. P., and Dowell, E. H., "Proper Orthogonal Decomposition Technique for Transonic Unsteady Aerodynamic Flows," AIAA Journal (also AIAA Paper 99-0655), Vol. 38, No. 10, October 2000, pp. 1853-1862.
15. Holmes, P., Lumley, J. L., and Berkooz, G., Turbulence, Coherent Structures, Dynamical Systems and Symmetry, Cambridge University Press, 1996.
16. LeGresley, P. A. and Alonso, J. J., "Airfoil Design Optimization Using Reduced Order Models Based on Proper Orthogonal Decomposition," AIAA Paper 2000-2545, June 2000.
17. LeGresley, P. A. and Alonso, J. J., "Investigation of Non-Linear Projection for POD Based Reduced Order Models for Aerodynamics," AIAA Paper 2001-0926, January 2001.
18. Lucia, D.J., Beran, P.S., and King, P.K., "Reduced Order Modeling of an Elastic Panel in Transonic Flow", AIAA Paper 2002-1594, April 2002 (also, to appear in the Journal of Aircraft).
19. Mortara, S. A. and Beran, P. S., "A Proper Orthogonal Decomposition Technique for the Computation of Nonlinear Panel Response," AIAA Paper 2000-1936, 2000.
20. Morton, S. A. and Beran, P. S., "Hopf-Bifurcation Analysis of Airfoil Flutter at Transonic Speeds," Journal of Aircraft, Vol. 36, No. 2, 1999, pp. 421-429.
21. Newman, A. J., "Model Reduction Via the Karhunen-Loeve Expansion Part 1: An Exposition," Tech. Rep. T.R. 96-32, Institute for Systems Research, University of Maryland, 1996.
22. Romanowski, M. C., "Reduced Order Unsteady Aerodynamic and Aeroelastic Models Using Karhunen-Loeve Eigenmodes," 6th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Bellevue WA, AIAA 96-3981-CP, September 1996, pp. 7-13.
23. Park, H. M. and Lee, M. W., "An Efficient Method of Solving the Navier-Stokes Equation for Flow Control," International Journal for Numerical Methods in Engineering, Vol. 41, 1998, pp. 1133-1151.
24. Pettit, C. L. and Beran, P. S., "Reduced-Order Modeling for Flutter Prediction," 41st AIAA/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Atlanta, GA, AIAA Paper 2000-1446-CP, April 2000 (also, to appear in IJNME Vol. 55, Issue 4, pp. 479-497).
25. Rediniotis, O. K., Ko, J., Yue, X., and Kurdila, A. J., "Synthetic Jets, their Reduced Order Modeling and Applications to Flow Control," 37th Aerospace Sciences Meeting and Exhibit, Reno, N.V., AIAA Paper 99-1000, January 1999.
26. Sankar, L. N., Ruo, S. Y., and Malone, J. B., "Application of Surface Transpiration in Computational Aerodynamics," AIAA 24th Aerosapce Sciences Meeting, Reno, NV, AIAA Paper 86-0511, January 1986.
27. Selvam, R. P. and Morton, S. A., "Computation of Nonlinear Viscous Panel Flutter Using a Fully Implicit Aeroelastic Solver," AIAA Paper 98-1844.
28. Thomas, J. P., Dowell, E. H., and Hall, K. C., "Three- Dimensional Transonic Aeroelasticity Using Proper Orthogonal Decomposition Based Reduced Order Models," AIAA Paper 2001-1526, April 2001.