Three-dimensional aeroelastic and aerothermoelastic behavior in hypersonic flow

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

Volumn 7, Issue , 2005, Pages 4655-4701

  McNamara, Jack J ^a,c   Friedmann, Peretz P ^a,c   Powell, Kenneth G ^a,c,d   Thuruthimattam, Biju J ^a   Bartels, Robert E ^b  

^a UNIVERSITY OF MICHIGAN   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

^c AIAA   (United States)

^d Department of Aerospace Engineering ^*

Author keywords

[No Author keywords available]

Indexed keywords

ASPECT RATIO; COMPUTATIONAL FLUID DYNAMICS; CURVE FITTING; FLUTTER (AERODYNAMICS); HYPERSONIC FLOW; JETS; LEAST SQUARES APPROXIMATIONS; MATHEMATICAL MODELS; PISTONS; THERMOELASTICITY; WINGS;

AEROTHERMOELASTIC BEHAVIOR; FLUTTER IDENTIFICATION; GENERIC HYPERSONIC VEHICLES; LEAST SQUARE CURVE FITTING METHOD;

HYPERSONIC AERODYNAMICS;

EID: 28844485739     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-2175     Document Type: Conference Paper

References (68)

1. Bisplinghoff, R.L. and Dugundji, J., Influence of Aerodynamic Heating on Aeroelastic Phenomena, Pergamon Press, 1958, pp. 288-312.
2. Garrick, I.E., "A Survey of Aerothermoelasticity," Aerospace Engineering, January, 1963, pp. 140-147.
3. Hedgepeth, J. and Widmayer, E., "Dynamic and Aeroelastic Problems of Lifting Re-Entry Bodies," Aerospace Engineering, January, 1963, pp. 148-153.
4. Laidlaw, W.R. and Wyker, J.H., "Potential Aerothermoelastic Problems Associated with Advanced Vehicle Design," Aerospace Engineering, January, 1963, pp. 154-164.
5. Xue, D.Y. and Mei, C., "Finite Element Two-Dimensional Panel Flutter at High Supersonic Speeds and Elevated Temperature," Proc. 31st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, No. AIAA Paper No. 90-0982, 1990, pp. 1464-1475.
6. Gray, E.G. and Mei, C., "Large-Amplitude Finite Element Flutter Analysis of Composite Panels in Hypersonic Flow," Proc. 33rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, No. AIAA Paper No. 92-2130, Dallas, TX, April 16-17 1992, pp. 492-512.
7. Abbas, J.F. and Ibrahim,R.A., "Nonlinear Flutter of Orthotropic Composite Panel Under Aerodynamic Heating," AIAA J., Vol. 31, No. 8, 1993, pp. 1478-1488.
8. Bein, T., Friedmann, P., Zhong, X., and Nydick, I., "Hypersonic Flutter of a Curved Shallow Panel with Aerodynamic Heating," Proc. 34th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, No. AIAA Paper No. 93-1318, La Jolla, CA, April 19-22 1993.
9. Nydick, I., Friedmann, P.P., and Zhong, X., "Hypersonic Panel Flutter Studies on Curved Panels," Proc. 36th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, No. AIAA Paper no. 95-1485, New Orleans, LA, April 1995, pp. 2995-3011.
10. Mei, C., Abdel-Motagly, K., and Chen, R., "Review of Nonlinear Panel Flutter at Supersonic and Hypersonic Speeds," Applied Mechanics Reviews, 1998.
11. Ricketts, R., Noll, T., Whitlow, W., and Huttsell,L., "An Overview of Aeroelasticity Studies for the National Aerospace Plane," Proc. 34th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, No. AIAA Paper No. 93-1313, La Jolla, CA, April 19-22 1993, pp. 152 - 162.
12. Spain, C., Zeiler, T.A., Bullock, E., and Hodge, J.S., "A Flutter Investigation of All-Moveable NASP-Like Wings at Hypersonic Speeds," Proc. 34th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, No. AIAA Paper No. 93-1315, La Jolla, CA, April 19-22 1993.
13. Scott, R.C. and Pototzky, A.S., "A Method of Predicting Quasi-Steady Aerodynamics for Flutter Analysis of High Speed Vehicles Using Steady CFD Calculations," Proc. 34th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, No. AIAA Paper No. 93-1364, La Jolla, CA, April 19-22 1993, pp. 595-603.
14. Spain, C., Zeiler, T.A., Gibbons, M.D., Soistmann, D.L., Pozefsky, P., DeJesus, R.O., and Brannon.C.P., "Aeroelastic Character of a National Aerospace Plane Demonstrator Concept," Proc. 34th AIAA/ASME/ASCE/AHS/ ASC Structures, Structural Dynamics and Materials Conference, La Jolla, CA, April 19-22 1993, pp. 163-170.
15. Rodgers, J.P., "Aerothermoelastic Analysis of a NASP-Like Vertical Fin," Proc. 33rd AIAA/ASME/ASCE/AHS Structures, Structural Dynamics and Materials Conference, No. AIAA-92-2400-CP, Dallas, TX, April 1992.
16. Heeg, J., Zeiler, T., Pototzky, A., Spain, C., and Engelund, W., "Aerothermoelastic Analysis of a NASP Demonstrator Model," Proc. 34th AIAA/ASME/ASCE/AHS/ ASC Structures, Structural Dynamics and Materials Conference, No. AIAA Paper No. 93-1366, La Jolla, CA, April 19-22 1993, pp. 617-627.
17. Heeg, J. and Gilbert, M.G., "Active Control of Aerothermoelastic Effects for a Conceptual Hypersonic Aircraft," Journal of Aircraft, Vol. 30, 1993, pp. 453-458.
18. Blades, E., Ruth, M., and Fuhrman, D., "Aeroelastic Analysis of the X-34 Launch Vehicle," Proc. 40th AIAA/ASME/ASCE/AHS/ ASC Structures, Structural Dynamics and Materials Conference, No. AIAA Paper No. 99-1352, St. Louis, MO, 1999, pp. 1321-1331.
19. Gupta, K.K., Voelker, L.S., Bach, C., Doyle, T., and Hahn, E., "CFD-Based Aeroelastic Analysis of the X-43 Hypersonic Flight Vehicle," 39th Aerospace Sciences Meeting & Exhibit, No. AIAA Paper No. 2001-0712, 2001.
20. Nydick, I. and Friedmann, P.P., "Aeroelastic Analysis of a Generic Hypersonic Vehicle," Proc. CEAS/AIAA/ICASE/NASA Langley International Forum on Aeroelasticity and Structural Dynamics, No. NASA/CP-1999-209136/PT2, Williamsburg, VA, June 22-25 1999, pp. 777-810.
21. Friedmann, P.P., McNamara, J.J., Thuruthimattam, B.J., and Nydick, I., "Aeroelastic Analysis of Hypersonic Vehicles," J. of Fluids and Structures, Vol. 19, 2004, pp. 681-712.
22. Berry, S.A., Horvath, T.J., Hollis, B.R., Thompson, R.A., and Hamilton, H.H., "X-33 Hypersonic Boundary Layer Transition," 33rd AIAA Thermophysics Conference, No. AIAA Paper No. 99-3560, Norfolk, VA, June 28 - July 1 1999.
23. Riley, C.J., Kleb, W.L., and Alter, S.J., "Aeroheating Predictions for X-34 Using An Inviscid-Boundary Layer Method," 36th Aerospace Sciences Meeting & Exhibit, No. AIAA 98-0880, Reno, NV, January 1998.
24. Thuruthimattam, B.J., Friedmann, P.P., McNamara, J.J., and Powell, K.G., "Aeroelasticity of a Generic Hypersonic Vehicle," Proc. 43rd AIAA/ASME/ASCE/AHS Structures, Structural Dynamics and Materials Conference, No. AIAA Paper No. 2002-1209, Denver, CO, April 2002.
25. Thuruthimattam, B.J., Friedmann, P.P., McNamara, J.J., and Powell, K.G., "Modeling Approaches to Hypersonic Aerothermoelasticity with Application to Resuable Launch Vehicles," Proc. 44th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics and Materials Conference, No. AIAA Paper No. 2003-1967, Norfolk, VA, April 2003.
26. McNamara, J.J., Thuruthimattam, B.J., Friedmann, P.P., Powell, K.G., and Bartels, R.E., "Hypersonic Aerothermoelastic Studies for Reusable Launch Vehicles," Proc. 45th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics and Materials Conference, No. AIAA Paper No. 2004-1590, Palm Springs, CA, April 2004.
27. Krist, S.L., Biedron, R.T., and Rumsey, C.L., CFL3D User's Manual (Version 5.0), NASA, TM 1998-208444, 1997, CFL3D v.6 update: http://cfl3d.larc.nasa.gov/Cfl3dv6/cfl3dv6.html.
28. Robinson, B.A., Batina, J.T., and Yang, H.T., "Aeroelastic Analysis of Wings Using the Euler Equations with a Deforming Mesh," Journal of Aircraft, Vol. 28, November 1991, pp. 778-788.
29. Cunningham, H.J., Batina, J.T., and Bennett, R.M., "Modern Wing Flutter Analysis by Computational Fluid Dynamic Methods," Journal of Aircraft, Vol. 25, No. 10, 1989, pp. 962-968.
30. Lee-Rausch, E.M. and Batina, J.T., "Wing Flutter Boundary Prediction Using Unsteady Euler Aerodynamic Method," Proc. 34th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics and Materials Conference, No. AIAA Paper No. 93-1422, 1993, pp. 1019-1029.
31. Lee-Rausch, E.M. and Batina, J.T., "Calculation of AGARD Wing 445.6 Flutter Using Navier-Stokes Aerodynamics," Proc. AIAA 11th Applied Aerodynamics Conference, No. AIAA Paper No. 93-3476, Hampton, VA, August 9-11 1993.
32. Batina, J.T., "Unsteady Euler Airfoil Solutions Using Unstructured Dynamic Meshes," AIAA Journal, Vol. 28, 1990, pp. 1381-1388.
33. Tezduyar, T.E., Behr, M., and Liou, J., "A New Strategy for Finite Element Computations involving Moving Boundaries and Interfaces - The Deforming-spatial-domain/Space-time Procedure: I. The concept and the Preliminary Numerical Tests," Computer Methods in Applied Mechanics and Engineering, Vol. 94, 1992, pp. 339-351.
34. Hughes, T.J.R. and Hulbert, G.M., "Space-Time Finite Element Methods For Elastodynamics: Formulations and Error Estimates," Computer Methods in Applied Mechanics and Engineering, Vol. 66, 1988, pp. 339-363.
35. Patil, M.J., Hodges, D.H., and Cesnik, C.E.S., "Nonlinear Aeroelastic Analysis of Complete Aircraft in Subsonic Flow," Journal of Aircraft, Vol. 37, No. 5, September 2000, pp. 753-760.
36. Donea, J., Guiliani, S., and Halleux, J.P., "An Arbitrary Lagrangian-Eulerian Finite Element Method for Transient Dynamic Fluid-Structure Interactions," Computer Methods in Applied Mechanics and Engineering, Vol. 33, 1982, pp. 689-723.
37. Bendiksen, O.O., "A New Approach to Computational Aeroelasticity," Proc. AIAA/ASME/ASCE/AHS/ASC 32nd Structure, Structural Dynamics and Materials Conf., Baltimore, MD, April 8-9 1991, pp. 1712-1727, AIAA Paper 91-0939.
38. Farhat, C., Lesoinne, M., and Maman, N., "Mixed Explicit/Implicit Time Integration of Coupled Aeroelastic Problems: Three-field Formulation, Geometric Conservation and Distributed Solution," International Journal for Numerical Methods in Fluids, Vol. 21, 1995, pp. 807-835.
39. Tran H. and Farhat, C., "An Integrated Platform for the Simulation of Fluid-Structure-Thermal Interaction Problems," Proc. 43rd AIAA/ASME/ASCE/AHS Structures, Structural Dynamics and Materials Conference, No. AIAA Paper No. 2002-1307, Denver, CO, April 2002.
40. Stephens, C.H., Arena Jr., A.S., and Gupta, K.K., "Application of the transpiration method for aeroservoelastic prediction using CFD," Proceedings of the 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit, No. AIAA Paper 98-2071, Long Beach, CA, April 20-23 1998.
41. Hartwich, P. and Agrawal, S., "Perturbing Multiblock Patched Grids in Aeroelastic Design Optimization Applications," No. AIAA 97-2038, June 1997.
42. Bartels, R.E., "Mesh Strategies for Accurate Computation of Unsteady Spoiler and Aeroelastic Problems," Journal of Aircraft, Vol. 37, No. 3, 2000, pp. 521-525.
43. Thuruthimattam, B.J., Fundamental Studies in Hypersonic Aeroelasticity Using Computational Methods, Ph.D. thesis, The University of Michigan, 2005.
44. Bartels, R.E., "New Mesh Movement and Aeroelasticity in CFL3D: Implementation and Use," NASA TM to be published, 2005.
45. Bousman, W.G. and Winkler, D.J., "Application of the Moving-Block Analysis," Proceedings of the AIAA Dynamics Specialist Conference, No. AIAA 81-0653, Atlanta, GA, April 1981, pp. 755-763.
46. Hammond, C.E. and Dogget, Jr. R.V., "Determination of Subcritical Damping by Moving-Block/Randomdec Applications," Proceedings of the Conference on Flutter Testing Techniques, NASA Dryden RC, Edwards, CA, October 1975, pp. 59-76.
47. Bennett, R.G. and Desmarais, R., "Curve Fitting of Aeroelastic Transient Response Data with Exponential Functions," No. NASA-SP-415, Oct. 1975, pp. 43-58.
48. Matsuzaki, Y. and Ando, Y., "Estimation of Flutter Boundary from Random Responses due to Turbulence at Subcritical Speeds," J. of Aircraft, Vol. 18, No. 10, 1981, pp. 862-868.
49. Pak, C.G. and Friedmann, P.P., "New Time Domain Technique for Flutter Boundary Identification," Proceedings of the AIAA Dynamics Specialist Conference, No. AIAA Paper 92-2102, Dallas, Tx, April 1992, pp. 201-214.
50. Batill, S.M., Carey, D.M., and Kehoe, M.W., "Digital Time Series Analysis for Flutter Test Data," Proceedings of the AIAA Dynamics Specialist Conference, No. AIAA Paper 92-2103, Dallas, Tx, April 1992, pp. 215-223.
51. Chen, P.C. and Liu, D.D., "Unified Hypersonic/Supersonic Panel Method for Aeroelastic Applications to Arbitrary Bodies," Journal of Aircraft, Vol. 39, No. 3, 2002, pp. 499-506.
52. Liu, D.D., Chen, P.C., Tang, L., Chang, K.T., and Gao, X.W., "Expedient Hypersonic Aerothermodynamics Methodology for RLV/TPS Design," Proc. 11th AIAA/AAAF International Conference on Space Planes and Hypersonic Systems and Technologies, Orleans, France, September 2002.
53. Ashley, H. and Zartarian, G., "Piston Theory - A New Aerodynamic Tool for the Aeroelastician," Journal of the Aeronautical Sciences, Vol. 23, No. 12, 1956, pp. 1109-1118.
54. Lighthill, M.J., "Oscillating Airfoils at High Mach Numbers," Journal of the Aeronautical Sciences, Vol. 20, No. 6, June 1953.
55. Anderson, J.D., Aerothermodynamics: A Tutorial Discussion, chap. 1, AIAA, 1992, pp. 3-57.
56. Bisplinghoff, R.L., "Some Structural and Aeroelastic Considerations of High-Speed Flight," Journal of the Aerospace Sciences, Vol. 23, No. 4, April 1956, pp. 289-329.
57. Rogers, M., "Aerothermoelasticity," AeroSpace Engineering, October 1958, pp. 3443.
58. Garrick, I.E., "Aeroelasticity Effects of High Temperatures," Aerospace Engineering, January 1963, pp. 140-147.
59. Budiansky, B. and Mayers, J., "Influence of Aerodynamic Heating on the Effective Torsional Stiffness of Thin Wings," Journal of the Aeronautical Sciences, December 1956, pp. 1081-1093.
60. Bertin, J.J., Hypersonic Aerothermodynamics, AIAA, Washington, DC, 1994.
61. Thornton, E.A., Thermal Structures for Aerospace Applications, AIAA, Reston, VA, 1996.
62. "MSC.NASTRAN Reference Manual," 2001.
63. Bisplinghoff, R.L., Ashley, H., and Halfman, R.L., Aeroelasticity, Addison-Wesley, 1955.
64. Reissner, E. and Stein M., "Torsion and Transverse Bending of Cantilever Plates," NACA TN 2369, 1951.
65. Crawley, E.F. and Dugundji, J., "Frequency Determination and Non-Dimensionalization for Composite Cantilever Plates," Journal of Sound and Vibration, Vol. 72, No. 1, 1980, pp. 1-10.
66. Gern, F. and Librescu, L., "Aeroelastic Tailoring of Composite Wings Exhibiting Nonclassical Effects and Carrying External Stores," Journal of Aircraft, Vol. 37, No. 6, 2000, pp. 1097-1104.
67. Ellis, D.A., Pagel, L.L., and Schaeffer, D.M., "Design and Fabrication of a Radiative Actively Cooled Honeycomb Sandwich Structural Panel for a Hypersonic Aircraft," NASA CR 2957, 1978.
68. Nydick, I., Studies in Hypersonic Aeroelasticity, Ph.D. thesis, University of California, Los Angeles, 2000.