Some recent advances in nonlinear aeroelasticity: Fluid-structure interaction in the 21 st Century

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn , Issue , 2010, Pages

  Dowell, Earl H ^a  

^a Duke University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ABRUPT WING STALL; AERODYNAMIC FORCES; EIGEN MODES; ELASTIC STRUCTURES; FREEPLAY; HARMONIC BALANCE; HIGH-DIMENSIONAL; LIFTING SURFACES; LIMIT CYCLE OSCILLATIONS; NONLINEAR AEROELASTICITY; PANEL FLUTTER; REDUCED-ORDER MODELING; STRUCTURAL DEFORMATION; SYNCHRONOUS VIBRATION; TRANSONIC FLUTTER; UNSTEADY AERODYNAMICS;

AERODYNAMIC STALLING; COMPUTATIONAL FLUID DYNAMICS; CONTROL NONLINEARITIES; DEFORMATION; DYNAMIC RESPONSE; ELASTIC WAVES; FLUID STRUCTURE INTERACTION; FLUIDS; FLUTTER (AERODYNAMICS); HOPF BIFURCATION; STRUCTURAL DYNAMICS;

AEROELASTICITY;

EID: 84855624332     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (94)

1. Dowell, E. H., Edwards . J.W. and Strganac, T.W, "Nonlinear Aeroelasticity," Journal of Aircraft, Vol. 40, No. 5, Sept.-Oct. 2003, pp. 857-874.
2. Dowell, E. H. and Tang, D. M., "Nonlinear Aeroelasticity and Unsteady Aerodynamics," AIAA Journal, Vol. 40, No. 9, 2002, pp. 1697-1707.
3. Dowell, E. H. and Hall, K. C., "Modeling of Fluid-Structure Interaction," Annual Reviews of Fluid Mechanics, Vol. 33, 2001, pp. 445-490.
4. Lucia, D. J., Beran, P. S. and Silva, W. A., "Reduced-Order Modeling: New Approaches for Computational Physics," Progress in Aerospace Sciences, Vol. 40, No. 1-2: 2004, pp. 51-117.
5. th Edition, Kluwer Academic Publishers, 2004.
6. Dowell, E. H. and Tang, D. M., "Dynamics of Very High Dimensional Systems," World Scientific, 2003. See especially Chapters 4, 13 and 14.
7. Hashimoto, A., Aoyama, T. and Nakamura, Y., "Effects of Turbulent Boundary Layer on Panel Flutter," AIAA Journal, Vol. 47, No. 12, 2009, pp. 2785-2791.
8. Dowell, E. H., "Aerodynamic Boundary Layer Effects on Flutter and Damping of Plates," Journal of Aircraft, Vol. 10, No. 12, 1973, pp. 734-738.
9. Muhlstein, L. and Gaspers, P., and Riddle, D., "An Experimental Study of the Influence of the Turbulent Boundary Layer on Panel Flutter," NASA TN D4486, 1968.
10. Dugundji, J., Dowell, E. and Perkin, B., "Subsonic Flutter of Panels on a Continuous Elastic Foundation, "AIAA Journal, Vol. 1, No. 5, 1963, pp. 1146-1154.
11. Dowell, E. H., "Aeroelasticity of Plates and Shells, "Kluwer Academic Publishers, 1975. See Appendix II.
12. Tang, D. M., Yamamoto, H. and Dowell, E. H., "Flutter and Limit Cycle Oscillations of Two-Dimensional Panels in a Three-Dimensional Axial Flow, "Journal of Fluids and Structures, Vol. 17, 2003, pp. 225-242.
13. Tang, L., Paidoussis, and Jiang, J. "Cantilevered Flexible Plates in Axial Flow: Energy Transfer and the Concept of a Flutter-Mill," Journal of Sound and Vibration, Vol. 326, 2009, pp. 263-276.
14. Hoffman, N. R., "Subsonic Flutter Model Tests of an All-Movable Stabilizer with 35 Degree Sweepback," WADC Technical Note 55-623. November 1955.
15. Tang, D., Dowell, E. H. and Virgin, L. N., "Limit Cycle Behavior of an Airfoil with a Control Surface," Journal of Fluids and Structures, Vol. 12, No. 7, 1998, pp. 839-858.
16. Tang, D. and Dowell, "Aeroelastic Airfoil with Freeplay at Angle of Attack with Gust Excitation," AIAA Journal, Vol. 48, No. 2, pp. 427-442.
17. Lee, D., Chen, P., Tang, D. and Dowell, E., "Nonlinear Gust Response of a Control Surface with Freeplay," AIAA 2010-3116, presented at the 51st AIAA SDM Conference, April 12-15, Orlando, Fl., 2010.
18. Schlomach, C., "All-Moveable Control Surface Freeplay," presentation to the Aerospace Flutter and Dynamics Council, NASA Langley Research Center, April 2-3, 2009.
19. Lieu, T., Farhat, C. and Lesoinne, A., "Reduced-Order Fluid/Structure Modeling of a Complete Aircraft Configuration," Computer Methods in Applied Mechanics and Engineering, Vol. 195, No. 41-43, 2006, pp. 5730- 5742.
20. Lieu, T. and Farhat, C., "Adaptation of Aeroelastic Reduced-Order Models and Application to an F-16 Configuration," AIAA Journal, Vol. 45, No. 6, 2007, pp. 1244-1257.
21. Amsallem, D. and Farhat, C., "Interpolation Method for Adapting Reduced-Order Models and Application to Aeroelasticity," AIAA Journal, Vol. 46, No. 7, 2008, pp. 1803-1813.
22. Romanowski, M. C., "Reduced Order Unsteady Aerodynamic and Aeroelastic Models Using Kahunen- Loeve Eigenmodes [POD Modes], AIAA Paper96-3981, presented at the AIAA/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Bellevue, Washington, 1996.
23. Hall, K.C., Thomas, J. P. and Dowell, E. H., "Proper Orthogonal Decomposition Technique for Transonic Unsteady Aerodynamic Flows," AIAA Journal, Vol.38, No. 10, 2000, pp. 1853-1862.
24. Thomas, J. P., Dowell, E. H. and Hall, K. C., "Three-Dimensional Aeroelasticity Using Proper Orthogonal Decomposition Based Reduced Order Models," Journal of Aircraft, Vol. 40, No. 3, 2003, pp. 544-551.
25. Dowell, E. H., Thomas, J. P. and Hall, K. C., "Transonic Limit Cycle Oscillation Analysis Using Reduced Order Models," Journal of Fluids and Structures, Vol. 19, No. 1, 2004, pp. 17-27.
26. Beran, P. S., Lucia, D. J. and Pettit, Cl. L., "Reduced-Order Modeling of Limit-Cycle Oscillation for Aeroelastic Systems," Journal of Fluids and Structures, Vol.19, No. 5, 2004, PP. 575-590.
27. Lucia, D. J. and Beran, P. S., "Reduced-Order Model Development Using Proper Orthogonal Decomposition and Volerra Theory," AIAA Journal, Vol. 42, No. 6, 2004, pp. 1181 -1190.
28. Mortara, S. A., Slater, J. and Beran, P., "Analysis of Nonlinear Aeroelastic Panel Response Using Proper Orthogonal Decomposition," Journal of Vibration and Acoustics, Vol. 126, No. 3, 2004, pp. 416-421.
29. Anttonen, J. S. R., King, P. I. and Beran, P. S., "Applications of Multi-POD to a Pitching and Plunging Airfoil," Mathematical and Computer Modeling," Vol.42, No. 3-4, 2005, pp. 245-259.
30. McMullen, M. and Jameson, A., "The Computational Efficiency of Non-linear Frequency Domain Methods," Journal Computational Physics, Vol. 212, No. 2, 2006, pp. 637-661.
31. McMullen, M., Jameson, A. and Alonzo, J., "Demonstration of Nonlinear Frequency Domain Methods," AIAA Journal, Vol. 44, No. 7, 2006, pp. 1428-1435.
32. Timme, S. and Badcock, K., "Implicit Harmonic Balance Solver for Transonic Flow with Forced Motions," AIAA Journal, Vol. 47, No. 4, 2009, pp. 893-901.
33. Hall, K. C., Thomas, J. P. and Clark, W. S., "Computation of Unsteady Nonlinear Flows in Cascades Using a Harmonic Balance Technique," AIAA Journal, Vol. 40, No. 5, 2002, pp. 879-886.
34. Thomas, J. P., Dowell, E. H. and Hall, K. C., "Modeling Viscous Transonic Limit Cycle Oscillations Behavior Using a Harmonic Balance Approach," Journal of Aircraft, Vol. 41, No. 6, 2004, pp. 1266-1274.
35. Beran, P. S. and Lucia, D. J., "A Reduced Order Cyclic Method for Computation of Limit Cycles," Nonlinear Dynamics, Vol. 39, No. 1-2, 2005, pp. 143-158.
36. Liu, L., Thomas, J. P., Dowell, E. H., Attar, P. J. and Hall, K.C., "A Comparison of Classical and High Dimensional Harmonic Balance Approaches for a Duffing Oscillator," Journal of Computational Physics, Vol. 215, No. 1, 2006, pp. 298-320.
37. Dowell, E. H., Hall, K. C., Thomas, J. P., Kielb, R. E., Spiker, M. A. and Denegri, Jr., C. M., "A New Solution Method for Unsteady Flows Around Oscillating Bluff Bodies," Proceedings of the IUTAM Symposium on Fluid-Structure Interaction in Ocean Engineering, 2007, Springer.
38. Custer, C. H., Thomas, J. P., Dowell, E. H. and Hall, K. C., "A Nonlinear Harmonic Balance Method for the CFD Code OVERFLOW 2," International Forum on Aeroelasticity and Structural Dynamics, Paper 2009-050, Seattle, Washington, June 2009.
39. Thomas, J. P., Custer, C. H., Dowell, E. H. and Hall, K. C., "Unsteady Flow Computations Using a Harmonic Balance Approach Implemented about the OVERFLOW 2 Flow Solver," 19th AIAA Computational Fluid Dynamics Conference, Paper 2009-4270, San Antonio, Texas, June 2009.
40. Thomas, J. P., Dowell, E. H. and Hall, K. C., "Using Automatic Differentiation to Create Nonlinear Reduced Order Model Aerodynamic Solver," AIAA Journal, Vol. 48, No. 1, 2010, pp. 19-24.
41. Thompson, J. M. T. and Stewart, H. B., Nonlinear Dynamics and Chaos, John Wiley and Sons, 1988.
42. Denegri, C.M., Jr., "Correlation of Classical Flutter Analyses and Nonlinear Flutter Responses Characteristics," International Forum on Aeroelasticity and Structural Dynamics, pp. 141-148, Rome, Italy, June 1997.
43. Denegri, C.M., Jr. and Cutchins, M.A., "Evaluation of Classical Flutter Analysis for the Prediction of Limit Cycle Oscillations," AIAA Paper 97-1021, April 1997.
44. Denegri, C.M., Jr., "Limit Cycle Oscillation Flight Test Results of a Fighter with External Stores," Journal of Aircraft, Vol. 37, No. 5, 2000, pp. 761-769.
45. Denegri, C.M., Jr. and Johnson, M.R., "Limit Cycle Oscillation Prediction Using Artificial Neural Networks," Journal of Guidance, Control, and Dynamics, Vol. 24, No. 5, 2001, pp. 887-895.
46. th Meeting of the Structures and Materials Panel, AGARD Conference Proceedings No. 162, Munich, Germany, October 1974.
47. Bunton, R.W. and Denegri, C.M. Jr., "Limit Cycle Oscillation Characteristics of Fighter Aircraft," Journal of Aircraft, Vol. 37, No. 5, 2000, pp. 916-918.
48. Cunningham, A.M. Jr., "A Generic Nonlinear Aeroelastic Method with Semi-Empirical Nonlinear Unsteady Aerodynamics," Vol. 1 and 2, AFRL-VA-WP-R-1999-3014, 1999.
49. Cunningham, A.M., Jr., "The Role of Nonlinear Aerodynamics in Fluid-Structure Interactions," AIAA Paper 98-2423, 1998.
50. Cunningham, A.M., Jr. and Geurts, E.G.M., "Analysis of Limit Cycle Oscillation/Transonic High Alpha Flow Visualization," AFRL-VA-WP-TR-1998- 3003, Part I, January 1998.
51. th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics and Materials Conference, AIAA Paper 85-0739-CP, Orlando, FL, April 15-17, 1985.
52. Hartwich, P.M., Dobbs, S.K., Arslan, A.E. and Kim, S.C., "Navier-Stokes Computations of Limit Cycle Oscillations for a B-1-Like Configuration," AIAA Paper 2000-2338, AIAA Fluids 2000, Denver, CO, June 2000.
53. Dreim, D.R., Jacobson, S.B. and Britt, R.T., "Simulation of Non-Linear Transonic Aeroelastic Behavior on the B-2," NASA CP-1999-209136, CEAS/AIAA/ICASE/NASA Langley International Forum on Aeroelasticity and Structural Dynamics, pp. 511-521, June 1999.
54. Croft, J., "Airbus Elevator Flutter: Annoying or Dangerous?", Aviation Week and Space Technology, August 2001.
55. Dowell, E.H., "Aeroelasticity of Plates and Shell," Kluwer Academic Publishers, 1975.
56. Dowell, E. H., "Panel Flutter," NASA Special Publication, SP-8004, 1972.
57. Yurkovich, R.N., Liu, D.D. and Chen, P.C., "The State-of-the-Art of Unsteady Aerodynamics for High Performance Aircraft," AIAA Paper 2001-0428, Aerospace Sciences Conference, January 2001.
58. Bennett, R.M. and Edwards, J.W., "An Overview of Recent Developments in Computational Aeroelasticity," AIAA Paper No. 98-2421, presented at the AIAA Fluid Dynamics Conference, Albuquerque, NM, June 1998.
59. Farhat, C. and Lesoinne, M., "Enhanced Partitioned Procedures for Solving Nonlinear Transient Aeroelastic Problems," AIAA Paper 98-1806, April 1998.
60. Raveh, D.E., Levy, Y. and Karpel, M., "Efficient Aeroelastic Analysis Using Computational Unsteady Aerodynamics," Journal of Aircraft, Vo. 38, No. 3, 2001, pp. 547-556.
61. nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit, Seattle, WA, April 16-19, 2001.
62. Gupta, K.K., "Development of a Finite Element Aeroelastic Analysis Capability," Journal of Aircraft, Vol. 33, No. 5, 1996, pp. 995-1002.
63. Scott, R.C., Silva, W.A., Florance, J.R. and Keller, D.F., "Measurement of Unsteady Pressure Data on a Large HSCT Semi-span Wing and Comparison with Analysis," AIAA Paper 2002-1648.
64. st Structures, Structural Dynamics and Materials Conference, AIAA No. 2000-1697, April 2000.
65. Bennett, R.M., Eckstrom, C.V., Rivera, J.A., Jr., Danberry, B.E., Farmer, M.G. and Durham, M.H., "The Benchmark Aeroelastic Models Program: Description and Highlights of Initial Results," NASA TM 104180, April 1991.
66. Bennett, R.M., Scott, R.C., and Wieseman, C.D., "Computational Test Cases for the Benchmark Active Controls Model," Journal of Guidance, Control, and Dynamics, Vol. 23, No. 5, September 2000, pp. 922-929.
67. Kholodar, D.E., Dowell, E.H., Thomas, J.P., and Hall, K.C., "Limit-Cycle Oscillations of a Typical Airfoil in Transonic Flow," Journal of Aircraft, Vol. 41, No. 5, AIAA, 2004.
68. Rivera, Jr., J., "Dansberry, B., Bennett, R., Durham, M., and Silva, W., "NACA0012 Benchmark Model Experimental Flutter Results with Unsteady Pressure Distributions," Technical Memorandum 107581, NASA, 1992.
69. Schwarz, J.B., Dowell, E.H., Thomas, J.P., Hall, K.C., Rausch, R.D. and Bartels, R.E., "Improved Flutter Boundary Prediction for an Isolated Two Degree of Freedom Airfoil", Journal of Aircraft, Vol. 46, No. 6, 2009, pp. 2069-2076.
70. Thomas, J.P., Dowell, E.H., and Hall, K.C., "Theoretical Predictions of Limit Cycle Oscillations for Flight Flutter Testing of the F-16 Fighter," Journal of Aircraft, Vol. 46, No. 5, 2009, pp. 1667-1672.
71. Dowell, E.H. and Tang, D., "Nonlinear Aeroelasticity and Unsteady Aerodynamics," AIAA Journal, Vol. 40, No. 9, 2002, pp. 1697-1707.
72. Gordnier, R.E. and Melville, R.B., "Physical Mechanisms for Limit-Cycle Oscillations of a Cropped Delta Wing," AIAA Paper 99-3796, Norfolk, VA, June 1999.
73. Gordnier, R.E. and Melville, R.B., "Numerical Simulation of Limit-Cycle Oscillations of a Cropped Delta Wing Using the Full Navier-Stokes Equations," International Journal of Computational Fluid Dynamics, Vol. 14 No. 3, 2001, pp. 211-224.
74. Schairer, E.T. and Hand, L.A., "Measurement of Unsteady Aeroelastic Model Deformation by Stereo Photogrammetry," AIAA Paper 97-2217, June 1997.
75. Thomas, J. P., Dowell, E. H. and Hall, K. C., "A Harmonic Balance Approach for Modeling Three- Dimensional Nonlinear Unsteady Aerodynamics and Aeroelasticity," IMECE-2002-32532, Presented at the ASME International Mechanical Engineering Conference and Exposition, November 17-22, 2002, New Orleans, Louisiana.
76. Edwards, J.W., "Calculated Viscous and Scale Effects on Transonic Aeroelasticity," Paper No. 1 in "Numerical Unsteady Aerodynamic and Aeroelastic Simulation". AGARD Report 822, March 1998.
77. Edwards, J.W., Schuster, D.M., Spain, C.V., Keller, D.F. and Moses, R.W., "MAVRIC Flutter Model Transonic Limit Cycle Oscillation Test," AIAA Paper No. 2001-1291, April 2001.
78. Edwards, J.W., "Transonic Shock Oscillations and Wing Flutter Calculated with an Interactive Boundary Layer Coupling Method," NASA TM-110284, August 1996.
79. Parker, E.C., Spain, C.V. and Soistmann, D.L., "Aileron Buzz Investigated on Several Generic NASP Wing Configurations," AIAA Paper 91-0936, April 1991.
80. Pak, C. and Baker, M.L., "Control Surface Buzz Analysis of a Generic Nasp Wing," AIAA Paper 2001- 1581, 2001.
81. Huttsell, L., Schuster, D., Volk, J., Giesing, J. and Love, M., "Evaluation of Computational Aeroelasticity Codes for Loads and Flutter," AIAA Paper 2001-569, 2001.
82. Edwards, J. W., "Calculated Viscous and Scale Effects on Transonic Aeroelasticity," Journal of Aircraft, Vol. 45, No. 6, 2008, pp. 1863-1871.
83. Barakos, G. and Drikakis, D., "Numerical Simulation of Transonic Buffet Flows Using Various Turbulence Closures, "International Journal of Heat and Fluid Flow, Vol. 21, 2000, pp. 620-626.
84. Raveh, D., "A Numerical Study of an Oscillating Airfoil in Transonic Buffeting Flows," AIAA Journal, Vol. 47, No. 3, 2009, pp. 505-515.
85. Raveh, D. and Dowell, E. H., "Aeroelastic Response of Airfoil in Buffeting Transonic Flows," In International Forum on Aeroelasticity and Structural Dynamics, Seattle, WA, 2009, IFASD-2009-161.
86. Raveh, D. and Dowell, E. H., "Frequency Lock-In Phenomenon for Oscillating Airfoils in Buffeting Flows," Accepted for publication in the Journal of Fluids and Structures.
87. McDevitt, J. B. and Okuno, A. F., "Static and Dynamic Pressure Measurements on a NACA 0012 Airfoil in the Ames High Reynolds Number Facility," NASA TP 2485, 1985.
88. Kielb, R., Barter, J. T. and Hall, K. C., "Blade Excitation by Aerodynamic Instabilities-A Compressor Blade Study," ASME GT-2003-38634, ASME Turbo Expo Conference, 2003.
89. Williams, M. H., "Linearization of Unsteady Transonic Flows Containing Shocks," AIAA Journal, Vol. 17, No. 4, 1979, pp.394-397.
90. Woodgate, M. A. and Badcock, K. J., "Implicit Harmonic Balance Solver for Transonic Flow with Forced Motions," AIAA Journal, Vol. 47, No. 4, 2009, pp. 893-901.
91. Friedmann, P.O., "Rotary-Wing Aeroelasticity: Current Status and Future Trends," AIAA Journal, Vol. 42, No. 10, 2004, pp. 1953-1972.
92. th International Symposium held at Duke University, 8-11 September, 2003, Springer, 2006.
93. Attar, P., Tang, D. and Dowell, E. H., "Nonlinear Aeroelastic Study for Folding Wing Structures," Presented at the NATO AVT-168 Symposium on Morphing Structures, 2009.
94. Batina, J., Introduction of the ASP3D Computer Program for Unsteady Aerodynamics and Aeroelastic Analyses, NASA TM-2005-213909, 2005.