Skip to main content
SpringerLink
Log in
Book cover

A Modern Course in Aeroelasticity pp 551–609Cite as

Nonlinear Aeroelasticity

  • Chapter

Part of the book series: Solid Mechanics and Its Applications ((SMIA,volume 116))

This is a preview of subscription content, log in via an institution.

Chapter
USD   29.95
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
eBook
USD   119.00
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book
USD   159.99
Price excludes VAT (USA)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info

Tax calculation will be finalised at checkout

Purchases are for personal use only

Learn about institutional subscriptions

Preview

Unable to display preview. Download preview PDF.

Unable to display preview. Download preview PDF.

References for Chapter 11

  1. Thompson, J. M. T. and Stewart, H. B., Nonlinear Dynamics and Chaos, John Wiley and Sons, 1988.

    Google Scholar 

  2. 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.

    Google Scholar 

  3. 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.

    Google Scholar 

  4. Denegri, C.M., Jr., “Limit Cycle Oscillation Flight Test Results of a Fighter with External Stores,” Journal of Aircraft, Vol. 37, No. 5, pp. 761–769, 2000.

    Google Scholar 

  5. 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, pp. 887–895, 2001.

    Google Scholar 

  6. AGARD Specialists Meeting on Wings-with-Stores Flutter, 39th Meeting of the Structures and Materials Panel, AGARD Conference Proceedings No. 162, Munich, Germany, October 1974.

    Google Scholar 

  7. Bunton, R.W. and Denegri, C.M. Jr., “Limit Cycle Oscillation Characteristics of Fighter Aircraft,” Journal of Aircraft, Vol. 37, No. 5, pp. 916–918, September 2000.

    Google Scholar 

  8. 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.

    Google Scholar 

  9. Cunningham, A.M., Jr., “The Role of Nonlinear Aerodynamics in Fluid-Structure Interactions,” AIAA Paper 98-2423, 1998.

    Google Scholar 

  10. 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.

    Google Scholar 

  11. Dobbs, S.K., Miller, G.D. and Stevenson, J.R., “Self Induced Oscillation Wind Tunnel Test of a Variable Sweep Wing,” 26th AIAA/ ASME/ASCE/AHS Structures, Structural Dynamics and Materials Conference, AIAA Paper 85-0739-CP, Orlando, FL, April 15–17, 1985.

    Google Scholar 

  12. 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.

    Google Scholar 

  13. 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.

    Google Scholar 

  14. Croft, J., “Airbus Elevator Flutter: Annoying or Dangerous?”, Aviation Week and Space Technology, August 2001.

    Google Scholar 

  15. Dowell, E. H., Panel Flutter, NASA Special Publication, SP-8004, 1972.

    Google Scholar 

  16. Dowell, E.H., Aeroelasticity of Plates and Shell, Kluwer Academic Publishers, 1975.

    Google Scholar 

  17. 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, January 2001.

    Google Scholar 

  18. Dowell, E.H. and Hall, K.C., “Modeling of Fluid-Structure Interaction,” Annual Review of Fluid Mechanics, Vol.33, 2001, pp. 445–490.

    Article  Google Scholar 

  19. 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.

    Google Scholar 

  20. Beran, P. and Silva, W., “Reduced-Order Modeling: New Approaches for Computational Physics,” AIAA Paper 2001–0853, 39th Aerospace Sciences Meeting and Exhibit, Reno, NV, January 2001.

    Google Scholar 

  21. Kim, T., and Bussoletti, J.E., “An Optimal Reduced Order Aeroelastic Modeling Based on a Response — Based Modal Analysis of Unsteady CFD Models,” AIAA Paper 2001-1525, 2001.

    Google Scholar 

  22. Silva, W.A., “Application of Nonlinear Systems Theory to Transonic Unsteady Aerodynamic Responses,” Journal of Aircraft, Vol. 30, No. 5, pp. 660–668, 1993.

    MathSciNet  Google Scholar 

  23. Silva, W.A., “Extension of a Nonlinear System Theory to General-Frequency Unsteady Transonic Aerodynamic Responses,” 34th AIAA Structures, Structural Dynamics, and Materials Conference, Reston, VA, pp. 2490–2503, 1993.

    Google Scholar 

  24. Silva, W.A., “Extension of a Nonlinear Systems Theory to Transonic Unsteady Aerodynamic Responses,” AIAA Paper 93–1590, April 1993.

    Google Scholar 

  25. Silva, W.A., “Discrete-Time Linear and Nonlinear Aerodynamic Impulse Responses for E cient (CFD) Analyses,” PhD Thesis, College of William Mary, Williamsburg, VA, October 1997.

    Google Scholar 

  26. Silva, W.A., “Identification of Linear and Nonlinear Aerodynamic Impulse Response Using Digital Filter Techniques,” AIAA Atmospheric Flight Mechanics Conference, Reston, VA, 1997, pp. 584–597.

    Google Scholar 

  27. Silva, W.A., “Reduced-Order Models Based on Linear and Nonlinear Aerodynamic Impulse Response,” International Forum on Aeroelasticity and Structural Dynamics, NASA Langley Research Center, Hampton, VA, June 1999 pp. 369–379.

    Google Scholar 

  28. Raveh, D., Levy, Y. and Karpel, M., “Aircraft Aeroelastic Analysis and Design Using CFD-Based Unsteady Loads,” AIAA Paper 2000–1325, 41st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit, Atlanta, GA, April 2000.

    Google Scholar 

  29. Raveh, D.E., “Reduced-Order Models for Nonlinear Unsteady Aerodynamics,” AIAA Journal, Vol. 39, No.8, 2001, pp. 1417–1429.

    Google Scholar 

  30. Farhat, C., Geuzaine, P., Brown, G. and Harris, C., “Nonlinear Flutter Analysis of an F-16 in Stabilized, Accelerated, and Increased Angle of Attack Flight Conditions,” AIAA Paper 2002–1490, April 2002.

    Google Scholar 

  31. Farhat, C., Harris, C. and Rixen, D., “Expanding a Flutter Envelope Using Accelerated Flight Data: Application to An F-16 Fighter Configuration,” AIAA Paper 2000–1702, April 2000.

    Google Scholar 

  32. Roughen, K.M., Baker, M.L. and Fogarty, T., “Computational Fluid Dynamics and Doublet-Lattice Calculation of Unsteady Control Surface Aerodynamics,” Journal of Aircraft, Vol. 24, No. 1, 2001, pp. 160–166.

    Google Scholar 

  33. Schuster, D.M., Edwards, J.W. and Bennett, R.M., “An Overview of Unsteady Pressure Measurements in the Transonic Dynamics Tunnel,” AIAA Paper No. 2000–1770, presented at the AIAA Dynamics Specialists Conference, Atlanta, GA, April 2000.

    Google Scholar 

  34. Ashley, H., “Role of Shocks in the’ sub-Transonic’ Flutter Phenomenon,” Journal of Aircraft, Vol. 17, 1980, pp. 187–197.

    Google Scholar 

  35. Bartels, R.E. and Schuster, D.M., “A Comparison of Two Navier-Stokes Aeroelastic Methods Using BACT Benchmark Experimental Data,” Journal of Guidance, Control, and Dynamics, Vol. 23, No. 5, 2000, pp. 1094–1099.

    Google Scholar 

  36. Davis, S.S. and Malcolm, G.N., “Transonic Shock-Wave/Boundary Layer Interactions on an Oscillating Airfoil,” AIAA Journal, Vol. 18, No. 11, 1980, pp. 1306–1312.

    Google Scholar 

  37. McMullen, M., Jameson, A. and Alonso, J.J., “Application of a Nonlinear Frequency Domain Solver to Euler and Navier-Stokes Equations,” AIAA Paper 2002–0120, 40th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 2002.

    Google Scholar 

  38. Kreiselmaier, E. and Laschka, B., “Small Disturbance Euler Equations: Effcient and Accurate Tool for Unsteady Load Prediction,” Journal of Aircraft, Vol. 37, No. 5, 2000.

    Google Scholar 

  39. Ruiz-Calavera, L.P. (ed.), “Verificationand Validation Data for Computational Unsteady Aerodynamics Codes,” Research and Technology Organization TW-26, 2000.

    Google Scholar 

  40. Farhat, C. and Lesoinne, M., “A Conservative Algorithm for Exchanging Aerodynamic and Elastodynamic Data in Aeroelastic Systems,” AIAA Paper 98-0515, January 1998.

    Google Scholar 

  41. Farhat, C. and Lesoinne, M., “A Higher-Order Subiteration Free Staggered Algorithm for Nonlinear Transient Aeroelastic Problems,” AIAA Journal, Vol. 36, No. 9, 1998, pp.1754–1756.

    Google Scholar 

  42. Farhat, C. and Lesoinne, M., “Enhanced Partitioned Procedures for Solving Nonlinear Transient Aeroelastic Problems,” AIAA Paper 98–1806, April 1998.

    Google Scholar 

  43. Raveh, D.E., Levy, Y. and Karpel, M., “Effcient Aeroelastic Analysis Using Computational Unsteady Aerodynamics,” Journal of Aircraft, Vo. 38, No.3, 2001, pp. 547–556.

    Google Scholar 

  44. Thomas, J.P., Dowell, E.H. and Hall, K.C., “Nonlinear Inviscid Aerodynamic Effects of Transonic Divergence, Flutter and Limit Cycle Oscillations,” AIAA Paper 2001–1209, presented at 42nd AIAA/ASME /ASCE /AHS /ASC Structures, Structural Dynamics and Materials Conference, Seattle, WA, April 2001.

    Google Scholar 

  45. 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, presented at 42nd AIAA/ASME /ASCE/AHS /ASC Structures, Structural Dynamics, and Materials Conference and Exhibit, Seattle, WA, April 16–19, 2001.

    Google Scholar 

  46. Gupta, K.K., “Development of a Finite Element Aeroelastic Analysis Capability,” Journal of Aircraft, Vol. 33, No. 5, 1996, pp. 995–1002.

    Google Scholar 

  47. 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.

    Google Scholar 

  48. Silva, W.A., Keller, D.F., Florance, J.R., Cole, S.R. and Scott, R.C., “Experimental Steady and Unsteady Aerodynamic and Flutter Results for HSCT Semi-span Models”, 41st Structures, Structural Dynamics and Materials Conference, AIAA No. 2000-1697, April 2000.

    Google Scholar 

  49. Ruiz-Calavera, L.P. and et al, “A New Compendium of Unsteady Aerodynamic Test Cases for CFD: Summary of AVT WG-003 Activities,” International Forum on Aeroelasticity and Structural Dynamics, June 1999.

    Google Scholar 

  50. 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.

    Google Scholar 

  51. 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, 2000, pp. 922–929.

    Google Scholar 

  52. Hall, K.C., Thomas, J.P, and Dowell, E.H., “Proper Orthogonal Decomposition Technique for Transonic Unsteady Aerodynamic Flows,” AIAA Paper 99-0655, AIAA Journal, Vol. 38, No. 10, 2000, pp. 1853–1862.

    Google Scholar 

  53. Hall, K.C., Thomas, J.P, and Dowell, E.H., “Proper Orthogonal Decomposition Technique for Transonic Unsteady Aerodynamic Flows,” AIAA Paper 99-0655, AIAA Journal, Vol. 38, No. 10, pp. 1853–1862, October 2000.

    Google Scholar 

  54. Hall, K.C., Thomas, J.P. and Dowell, E.H., “Reduced-Order Modeling of Unsteady Small Disturbance Flows Using a Frequency-Domain Proper Orthogonal Decomposition Technique,” AIAA Paper 99-0655, presented at 37th AIAA Aerospace Sciences Meeting and Exhibition, Reno, NV, January 1999.

    Google Scholar 

  55. Isogai, K., “On the Transonic-Dip Mechanism of Flutter of Sweptback Wing,” AIAA Journal, Vol. 17, No. 7, 1979, pp. 793–795.

    Google Scholar 

  56. Ehlers, F.E. and Weatherhill, W.H., “A Harmonic Analysis Method for Unsteady Transonic Flow and Its Application to the Flutter of Airfoils,” NASA CR-3537, May 1982.

    Google Scholar 

  57. Edwards, J.W., Bennett, R.M., Whitlow, W., Jr. and Seidel, D.A., “Time-Marching Transonic Flutter Solutions Including Angle-of-Attack Effects,” Journal of Aircraft, Vol. 20, No. 11, 1983, pp. 899–906.

    Google Scholar 

  58. Prananta, B.B., Hounjet, J.H.L. and Zwaan, R.J., “Two-Dimensional Transonic Aeroelastic Analysis Using Thin-Layer Navier-Stokes Methods,” Journal of Fluids and Structures, Vol. 12, 1998, pp. 655–676

    Article  Google Scholar 

  59. Bohbot, J. and Darracq, D., “Time Domain Analysis of Two D.O.F. Airfoil Flutter Usingan Euler/Turbulent Navier-Stokes Implicit Solver,” International Forum on Structural Dynamics, Vol.II, pp. 75–86, Madrid, Spain, June 2001.

    Google Scholar 

  60. Bendiksen, O.O., “Energy Approachto Flutter Suppression and Aeroelastic Control,” Journal of Guidance, Control and Dynamics, Vol. 24, No 1, pp.176–184, February 2001.

    Google Scholar 

  61. Bendiksen, O.O., “Transonic Flutter,” AIAA Paper 2002-1488, 43rd AIAA/ASME /ASCE/AHS /ASC Structures, Structural Dynamics and Materials Conference, Denver, CO, April 2002.

    Google Scholar 

  62. Bendiksen, O.O., “Transonic Flutter and the Nature of the Transonic Dip,” IFASD 2001, Vol. 11, Madrid, Spain, June 2001.

    Google Scholar 

  63. Dogget, R.V., Jr., Rainey, A.G. and Morgan, H.G., “An Experimental Investigation of Aerodynamic E ects of Airfoil Thickness on Transonic Flutter Characteristics,” NASA TM X-79, 1959.

    Google Scholar 

  64. Dowell, E.H., Crawley, E.F., Curtiss, H.C. Jr., Peters, D.A., Scanlan, R.H., and Sisto, F., A Modern Course in Aeroelasticity, Dor-drecht/Boston: Kluwer Academic Publishers, 699 pp, 3rd Edition, 1995.

    Google Scholar 

  65. Dowell, E.H. and Tang, D.M., “Nonlinear Aeroelasticity and Unsteady Aerodynamics,” AIAA paper 2002-0003, The Theodore von Karman Lecture, AIAA Journal, Vol. 40, No. 9, 2002, pp.1697–1707.

    Google Scholar 

  66. O’Neil, T., Gilliat, H. and Strganac, T., “Investigation of Aeroelastic Response for a System with Continuous Structural Nonlinearities,” AIAA Paper 96-1390, 1996.

    Google Scholar 

  67. Block, J.J. and Strganac, T.W., “Applied Active Control for a Nonlinear Aeroelastic Structure,” Journal of Guidance, Control, and Dynamics, Vol. 21, No. 6, 1998, pp. 838–845.

    Google Scholar 

  68. Ko, J., Kurdila, A.J. and Strganac, T.W., “Nonlinear Control of a Prototypical Wing Section with Torsional Nonlinearity,” Journal of Guidance, Control and Dynamics, Vol. 20, No. 6, 1997, pp. 1181–1189.

    Google Scholar 

  69. Ko, J., Strganac, T.W. and Kurdila, A.J., “Adaptive Feedback Linearization for the Control of a Typical Wing Section with Structural Nonlinearity,” Nonlinear Dynamics, Vol. 18, No. 3, 1999, pp. 289–301.

    Article  Google Scholar 

  70. Ko, J., Strganac, T.W. and Kurdila, A.J., “Stability and Control of a Structurally Nonlinear Aeroelastic System,” Journal of Guidance, Control and Dynamics, Vol. 21, No. 5, 1998, pp. 718–725.

    Google Scholar 

  71. Thompson, D.E. and Strganac, T.W., “Store-Induced Limit Cycle Oscillations and Internal Resonance in Aeroelastic Systems,” 41st AIAA Structures, Structural Dynamics and Materials Conference, AIAA Paper 2000-1413, 2000.

    Google Scholar 

  72. Cole, S.R., “Effects of Spoiler Surfaces on the Aeroelastic Behavior of a Low-Aspect Ratio Wing,” 31st AIAA Structures, Structural Dynamics and Materials Conference, AIAA Paper 90-0981, pp. 1455–1463, 1990.

    Google Scholar 

  73. Oh, K., Nayfeh, A.H. and Mook, D.T., “Modal Interactions in the Forced Vibration of a Cantilever Metallic Plate,” Nonlinear and Stochastic Dynamics, Vol. 192, 1994, pp. 237–247.

    Google Scholar 

  74. Pai, P.F. and Nayfeh, A.H., “Three-Dimensional Nonlinear Vibrations of Composite Beams-I: Equations of Motion,” Nonlinear Dynamics, Vol. 1, 1990, pp. 477–502.

    Article  Google Scholar 

  75. Stearman, R.O., Powers, E.J., Schwarts, J. and Yurkorvich, R., “Aeroelastic System Identification of Advanced Technology Aircraft Through Higher Order Signal Processing,” 9th International Modal Analysis Conference, pp. 1607–1616, Florence, Italy, April 1991.

    Google Scholar 

  76. Gilliatt, H.C., Strganac, T.W., and Kurdila, A.J., “Nonlinear Aeroelastic Response of an Airfoil,” 35th Aerospace Sciences Meeting and Exhibit, AIAA Paper 97-0459, pp 258–266, Reno, NV, January 1997.

    Google Scholar 

  77. Chang, J.H., Stearman, R.O., Choi, D. and Powers, E.J., “Identification of Aeroelastic Phenomenon Employing Bispectral Analysis Techniques,” International Modal Analysis Conference and Exhibit, Vo. 2, pp. 956–964, 1985.

    Google Scholar 

  78. Tang, D.M. and Dowell, E.H., “Effects of Angle of Attack on Nonlinear Flutter of a Delta Wing,” AIAA Journal, Vol.39, No. 1, 2001, pp. 15–21.

    Google Scholar 

  79. 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.

    Google Scholar 

  80. 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.

    Google Scholar 

  81. Schairer, E.T. and Hand, L.A., “Measurement of Unsteady Aeroelastic Model Deformation by Stereo Photogrammetry,” AIAA Paper 97-2217, June 1997.

    Google Scholar 

  82. Preidikman, S. and Mook, D.T., “Time Domain Simulations of Linear and Nonlinear Aeroelastic Behavior,” Journal of Vibration and Control, Vol. 6, No.8, pp. 1135–1175, 2000.

    Google Scholar 

  83. Patil, M.J., Hodges, D.H. and Cesnik, C., “Nonlinear Aeroelasticity and Flight Dynamics of High-Altitude Long-Endurance Aircraft,” AIAA Paper 99-1470, 1999.

    Google Scholar 

  84. Patil, M.J., Hodges, D.H. and Cesnik, C.E., “Nonlinear Aeroelastic Analysis of Complete Aircraft in Subsonic Flow,” Journal of Aircraft, Vol. 37, No. 5, pp. 753–760, September–October 2000.

    Google Scholar 

  85. Tang, D.M. and Dowell, E.H., “Experimental and Theoretical Study on Aeroelastic Response of High-Aspect-Ratio Wings,” AIAA Journal, Vol. 39, No. 8, pp. 1430–1441, August 2001.

    Google Scholar 

  86. Kim, K. and Strganac, T., “Aeroelastic Studies of a Cantilever Wing with Structural and Aerodynamic Nonlinearities,” AIAA Paper 2002-1412, 43rd AIAA/ASME/ASCE/AHS/ACS Structures, Structural Dynamics and Materials Conference, Denver, CO, April 2002.

    Google Scholar 

  87. Crespo da Silva, M.R.M. and Glynn, C.C., “Nonlinear Flexural—Torsional Dynamics of Inextensional Beams—I: Equations of Motions,” Journal of Structural Mechanics, Vol. 6, No. 4, 1978, pp. 437–448.

    Google Scholar 

  88. Chen, P.C., Sarhaddi, D. and Liu, D.D., “Limit Cycle Oscillation Studies of a Fighter with External Stores,” AIAA Paper 98-1727, 1998.

    Google Scholar 

  89. Kholodar, D.B., Thomas, J.P., Dowell, E.H. and Hall, K.C., “A Parametric Study of Transonic Airfoil Flutter and Limit Cycle Oscillation Behavior,” AIAA Paper 2002-1211, presented at the AIAA/ASME/ ASCE/AHS SDM Conference, Denver, CO, April 2002.

    Google Scholar 

  90. Knipfer, A. and Schewe, G., “Investigations of and Oscillation Supercritical 2-D Wing Section in a Transonic Flow,” 36th Aerospace Sciences Meeting and Exhibit, AIAA Paper No. 99-0653, January 1999.

    Google Scholar 

  91. Schewe, G. and Deyhle, H., “Experiments on Transonic Flutter of a Two-Dimensional Supercritical Wing with Emphasis on the Nonlinear E ects,” proceeding of the Royal Aeronautical Society Conference on Unsteady Aerodynamics, London, U.K., July 17–18, 1996.

    Google Scholar 

  92. Schewe, G., Knipfer, A. and Henke, H., “Experimentelle und numerisch Untersuchung zum transonischen Flgelflattern im Hinblick auf nichtlineare E ecte,” unpublished manuscript, February 1999.

    Google Scholar 

  93. Schewe, G., Knipfer, A., Mai, H. and Dietz, G., “Experimental and Numerical Investigation of Nonlinear E ects in Transonic Flutter ” English Version (Translated by Dr.W.F. King III), German Aerospace Center DLR Final Report Number DLR IB 232-2002 J 01, Corresponds to Final Report for BMBF: Nichtlineare E ekte beim transsonischen Flattern (FKZ 13 N 7172), and Internal Report DLR IB 2001 J03, January 25, 2002.

    Google Scholar 

  94. Thomas, J.P., Dowell, E.H. and Hall, K.C., “Modeling Viscous Transonic Limit Cycle Oscillation Behavior Usinga Harmonic Balance Approach,” AIAA Paper 2002-1414, presented at 43rd AIAA/ ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit, Denver, CO, April 22–25, 2002.

    Google Scholar 

  95. Weber, S., Jones, K.D., Ekaterinaris, J.A. and Platzer, M.F., “Transonic Flutter Computations for a 2-D Supercritical Wing,” AIAA Paper 99-0798, 36th Aerospace Sciences Meeting and Exhibit, Reno, NV, January 1999.

    Google Scholar 

  96. Tang, L., Bartels, R.E., Chen, P.C. and Liu, D.D., “Simulation of Transonic Limit Cycle Oscillations Using a CFD Time-Marching Method,” AIAA Paper 2001-1290, 42nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Seattle. WA, April 2001.

    Google Scholar 

  97. Castro, B.M., Ekaterinaris, J. A., and Platzer, M. F., “Navier-Stokes Analysis of Wind-Tunnel Interference on Transonic Airfoil Flutter,” AIAA Journal, Vol. 40, No. 7, 2002, pp. 1269–1276.

    Google Scholar 

  98. Thomas, J.P., Dowell, E.H., and Hall, K.C., “A Harmonic Balance Approach for Modeling Three-Dimensional Nonlinear Unsteady Aerodynamics and Aeroelasticity,” IMECE paper 2003-32532, 2001.

    Google Scholar 

  99. Edwards, J.W., “Calculated Viscous and Scale E ects on Transonic Aeroelasticity,” AGARD-R-822, Numerical Unsteady Aerodynamic and Aeroelastic Simulation, pp.1-1–1-1, March 1998.

    Google Scholar 

  100. 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.

    Google Scholar 

  101. Edwards, J.W., “Transonic Shock Oscillations and Wing Flutter Calculated with an Interactive Boundary Layer Coupling Method,” NASA TM-110284, August 1996.

    Google Scholar 

  102. Parker, E.C., Spain, C.V. and Soistmann, D.L., “Aileron Buzz Investigatedon Several Generic NASP Wing Configurations,” AIAA Paper 91-0936, April 1991.

    Google Scholar 

  103. Pak, C. and Baker, M.L., “Control Surface Buzz Analysis of a Generic Nasp Wing,” AIAA Paper 2001-1581, 2001.

    Google Scholar 

  104. Beran, P.S., Khot, N.S., Eastep, F.E., Snyder, R.D., Zweber, J.V., Huttsell, L.J. and Scott, J.N., “The Dependence of Store-Induced Limit-Cycle Oscillation Predictions on Modeling Fidelity,” RTO Applied Vehicle Technology Panel Symposium on Reduction of Military Vehicle Acquisition Time and Cost Through Advanced Modeling and Virtual Product Simulation, Paper 44, Paris, France, April 2002.

    Google Scholar 

  105. Hutsell, L., Schuster, D., Volk, J., Giesing, J. and Love, M., “Evaluation of Computational Aeroelasticity Codes for Loads and Flutter,” AIAA Paper 2001-569, 2001.

    Google Scholar 

  106. Woodson, S.H., “Wing Drop,” article in the McGraw-Hill 2002 Yearbook of Science and Technology, McGraw-Hill, New York, 2001.

    Google Scholar 

  107. Chambers, J.R., “Historical Review: Perspective on Experiences with Uncommanded Lateral Motions at High-Subsonic and Transonic Speeds,” Ball Aerospace & Technologies Report, Aerospace Systems Division, February 1999.

    Google Scholar 

  108. Nayfeh, A.H., Elzebda, J.M. and Mook, D.T., “Analytical Study of the Subsonic Wing-Rock Phenomenon for Slender Delta Wings,” Journal of Aircraft, Vol. 26, No. 9, 1989, pp. 805–809.

    Google Scholar 

  109. Ericsson, L.E., “Flow Physics Generating Highly Nonlinear Lateral Stability Characteristics of 65-Degree Delta-Wing-Body,” Journal of Aircraft, Vol. 38, No. 5, 2001, pp. 932–934.

    Google Scholar 

  110. Kokolios, A. and Cook, S.P., “Modeling Abrupt Wing Stall From Flight Test Data,” 32nd Annual Symposium of the Society of Flight Test Engineers, Seattle, WA, September 2001.

    Google Scholar 

  111. Lamar, J.E., Hall, R.M., Sanders, E.N., Cook, S.P. and Grove, D.V., “Status and Plans of Abrupt Wing Stall Figures-of-Merit (FOM) Studies From Experimental and Computational Fluid Dynamics,” NASA Technical Report in Preparation, 2003.

    Google Scholar 

  112. Heeg, J., “Analytical and Experimental Investigation of Flutter Suppression by Piezoelectric Actuation,” NASA Technical Paper 3241, 1993.

    Google Scholar 

  113. Lazarus, K.B., Crawley, E.F. and Lin, C.Y., “Fundamental Mechanism of Aeroelastic Control with Control Surface and Strain Actuation,” 32nd AIAA/ASME/ASCE/AHS SDM Conference, pp. 1817–1831, Baltimore, MD, April 1991.

    Google Scholar 

  114. Lazarus, K.B., Crawley, E.F. and Lin, C.Y., “Multi-variable Active Lifting Surface Control Using Strain Actuation: Analytical and Experimental Results,” Journal of Aircraft, Vol. 34, No. 3, 1997, pp. 313–321.

    Google Scholar 

  115. Vipperman, J.S., Barker, J.M., Clark, R.L. and Balas, G.S., “Comparison of μ-and H2-Synthesis Controllers on an Experimental Typical Section,” Journal of Guidance, Control and Dynamics, Vol. 22, No. 2, 1999, pp. 278–285.

    Google Scholar 

  116. Clark, R.L., Frampton, K.D. and Dowell, E.H., “Control of a Three Degree of Freedom Airfoil with Limit Cycle Behavior,” AIAA Journal of Aircraft, Vol. 37, No. 3, 2000, pp. 533–536.

    Google Scholar 

  117. Frampton, K.D. and Clark, R.L., “Experiments on Control of Limit Cycle Oscillations in a Typical Section,” AIAA Journal of Guidance, Control and Dynamics, Vol. 23, No. 5, 2000, pp. 956–960.

    Google Scholar 

  118. Rule, J.A., Richard, R.E. and Clark, R.L., “Design of an Aeroelastic Delta Wing Model for Active Flutter Control,” AIAA Journal of Guidance, Control and Dynamics, Vol. 24, No. 5, 2001, pp. 918–924.

    Google Scholar 

  119. Richard, R.W., Rule, J.A. and Clark, R.L., “Genetic Spatial Optimization of Active Elements on an Aeroelastic Delta Wing,” ASME Journal of Vibration and Acoustics, Vol. 123, 2001, pp. 466–471.

    Google Scholar 

  120. Platanitis, G. and Strganac, T., “Control of a Wing Section with Nonlinearities Using Leading and Trailing Edge Control Surfaces,” AIAA Paper No. 2002-1718, 43rd AIAA/ASME/ASCE/ AHS/ACS Structures, Structural Dynamics and Materials Conference, Denver, CO, April 2002.

    Google Scholar 

Download references

Editor information

Editors and Affiliations

  1. Duke University, Durham, NC, USA

    Earl H. Dowell

Rights and permissions

Reprints and permissions

Copyright information

© 2005 Springer Science + Business Media, Inc.

About this chapter

Cite this chapter

(2005). Nonlinear Aeroelasticity. In: Dowell, E.H. (eds) A Modern Course in Aeroelasticity. Solid Mechanics and Its Applications, vol 116. Springer, Dordrecht. https://doi.org/10.1007/1-4020-2106-2_11

Download citation

  • DOI: https://doi.org/10.1007/1-4020-2106-2_11

  • Publisher Name: Springer, Dordrecht

  • Print ISBN: 978-1-4020-2039-1

  • Online ISBN: 978-1-4020-2106-0

  • eBook Packages: Springer Book Archive

Publish with us

Policies and ethics

Search

Navigation