A reduced order aerothermodynamic modeling framework for hypersonic aerothermoelasticity

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

Volumn , Issue , 2010, Pages

  Crowell, Andrew R ^a   McNamara, Jack J ^a   Kecskemety, Krista M ^a   Goerig, Trevor W ^a  

^a The Ohio State University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE SAMPLING METHODS; AEROTHERMOELASTICITY; AIR BREATHING; COMPUTATIONALLY EFFICIENT; EFFICIENT COMPUTATION; FREESTREAM MACH NUMBER; HIGHLY NONLINEAR; INPUT PARAMETER; KRIGING APPROACH; LATIN HYPERCUBE; MEAN SQUARED ERROR; MODELING FRAMEWORKS; MULTI-DISCIPLINARY; ONE-PASS; PARAMETER SPACES; PROPER ORTHOGONAL DECOMPOSITIONS; PROPULSION SYSTEM; REDUCED ORDER; REDUCED ORDER MODELING TECHNIQUE; REDUCED ORDER MODELS; REDUCED-ORDER MODELING; RMS ERRORS; SAMPLING STRATEGIES; SIDESLIP ANGLES; STRUCTURAL DEFORMATION; SURFACE HEAT FLUX DISTRIBUTION; SURFACE HEAT FLUXES; SURFACE TEMPERATURES; TURBULENT TRANSITION;

COMPUTATIONAL FLUID DYNAMICS; CONTROL SURFACES; HEAT FLUX; HYPERSONIC AERODYNAMICS; HYPERSONIC VEHICLES; MACH NUMBER; PROPULSION; STRUCTURAL DYNAMICS; SURFACES; THREE TERM CONTROL SYSTEMS;

THREE DIMENSIONAL;

EID: 84855621533     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (51)

1. Mansour, N., Pittman, J., and Olson, L., "Fundamental Aeronautics Hypersonics Project: Overview," AIAA Paper 2007-4263, June 2007.
2. Bolender, M. A. and Doman, D. B., "Nonlinear Longitudinal Dynamic Model of an Air-Breathing Hypersonic Vehicle," Journal of Spacecraft and Rockets, Vol. 44, No. 2, March-April 2007, pp. 374-387.
3. Cazier, Jr., F.W. and Ricketts, R. H., "Structural Dynamic and Aeroelastic Considerations for Hypersonic Vehicles," AIAA Paper 1991-1255, April 1991.
4. Anderson, Jr., J. D., Hypersonic and High-Temperature Gas Dynamics, American Institute of Aeronautics and Astronautics, Reston, Virginia, 2nd ed., 2006.
5. Blankson, I. M., "Air-Breathing Hypersonic Waveriders: A Survey of Research Needs," Proceedings of the First International Waverider Symposium, University of Maryland, College Park, Maryland, October 1990.
6. Bertin, J. J. and Cummings, R. M., "Fifty Years of Hypersonics: WhereWe've Been and WhereWe're Going," Progress in Aerospace Sciences, Vol. 39, April 2003, pp. 511-536.
7. Fidan, B., Mirmirani, M., and Ionnou, P., "Flight Dynamics and Control of Air-Breathing Hypersonic Vehicles: Review and New Directions," AIAA Paper 2003-7081, December 2003.
8. McNamara, J. J. and Friedmann, P. P., "Aeroelastic and Aerothermoelastic Analysis of Hypersonic Vehicles: Current Status and Future Trends," AIAA Paper 2007-2013, April 2007.
9. Weiting, A., Dechaumphai, P., Bey, K., Thornton, E., and Morgan, K., "Application of Integrated Fluid-Thermal-Structure Analysis Methods," Thin-walled Structures, 1991, 11 pp. 1-23.
10. Culler, A. J. and McNamara, J. J., "Coupled Flow-Thermal-Structural Analysis for Response Prediction of Hypersonic Vehicle Skin Panels," AIAA Paper 2010-2965, April 2010.
11. Culler, A. J., Crowell, A. R., and McNamara, J. J., "Studies on Fluid-Structural Coupling for Aerothermoelasticity in Hypersonic Flow," AIAA Paper 2009-2364, May 2009.
12. Miller, B. A., McNamara, J. J., Culler, A. J., and Spottswood, S. M., "The Impact of Flow Induced Loads on Snap-Through Behavior of Acoustically Excited, Thermally Buckled Panels," AIAA Paper 2010-2540, April 2010.
13. Torrez, S., Driscoll, J., Bolender, M., Oppenheimer, M., and Doman, D., "Effects of Improved Propulsion Modelling on the Flight Dynamics of Hypersonic Vehicles," AIAA Paper 2008-6386, 2008, AIAA Atmospheric Flight Mechanics Conference and Exhibit, Honolulu HI.
14. McNamara, J. J., Friedmann, P. P., Powell, K. G., Thuruthimattam, B. J., and Bartels, R. E., "Three-Dimensional Aeroelastic and Aerothermoelastic Behavior in Hypersonic Flow," AIAA Paper 2005-2175, April 2005.
15. Dugundji, J. and Calligeros, J. M., "Similarity Laws for Aerothermoelastic Testing," Journal of the Aero/Space Sciences, Vol. 29, No. 8, August 1962, pp. 935-950.
16. Gnoffo, P., "Updates to Multi-Dimensional Flux Reconstruction for Hypersonic Simulations on Tetrahedral Grids," AIAA Paper 2010-1271, January 2010, 48th AIAA Aerospace Sciences Meeting.
17. Candler, G. V., "Comparison of CFD and Theoretical Post-Shock Gradients in Hypersonic Flow," AIAA Paper 2009-3719, June 2009, 39th AIAA Fluid Dynamics Conference.
18. Candler, G. V., Mavriplis, D. J., and Trevino, L., "Current Status and future Prospects for the Numerical Simulation of Hypersonic Flows," AIAA Paper 2009-153, January 2009, 47th AIAA Aerospace Sciences Meeting.
19. Eckert, E. R. G., "Engineering Relations for Heat Transfer and Friction in High-Velocity Laminar and Turbulent Boundary-Layer Flow Over Surfaces With Constant Pressure and Temperature," Transactions of the ASME, Vol. 78, No. 6, August 1956, pp. 1273-1283.
20. Dechaumphai, P., Thornton, E. A., and Wieting, A. R., "Flow-Thermal-Structural Study of Aerodynamically Heated Leading Edges," Journal of Spacecraft and Rockets, Vol. 26, No. 4, July-August 1989, pp. 201-209.
21. Kontinos, D., "Coupled Thermal Analysis Method with Application to Metallic Thermal Protection Panels," Journal of Thermophysics and Heat Transfer, Vol. 11, No. 2, April-June 1997, pp. 173-181.
22. McNamara, J. J., Culler, A. J., and Crowell, A. R., " Aerothermoelastic Modeling Considerations for Hypersonic Vehicles," 16thAIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, No. AIAA-2009-7397, Bremen, Germany, Oct. 2009.
23. Lucia, D. J., Beran, P. S., and Silva, W. A., "Reduced Order Modeling: New Approaches for Computational Physics," Progress in Aerospace Sciences, Vol. 40, February 2004, pp. 51-117.
24. Dowell, E. H. and Hall, K. C., "Modeling of Fluid-Structure Interaction," Annual Review of Fluid Mechanics, Vol. 33, 2001, pp. 445- 490.
25. Lucia, D. J., Reduced Order Modeling for High Speed Flows with Moving Shocks, Ph.D. Thesis, Air Force Institute of Technology, Wright-Patterson AFB, Ohio, 2001.
26. Tang, L., Chen, P., Liu, D., Gao, X., Shyy, W., Utturkar, Y., and Zhang, B., "Proper Orthogonal Decomposition and Response Surface Method for TPS/RLV Structural Design and Optimization: X-43 Case Study," AIAA Paper 2005-839, January 2005.
27. McNamara, J. J., Gogulapati, A., Friedmann, P. P., and Banavara, N. K., "Approximate Modeling of Unsteady Aerodynamic Loads in Hypersonic Aeroelasticity," Proceedings of the International Forum on Aeroelasticity and Structural Dynamics, No. IFASD-2007- 099, Stockholm, Sweden, June 2007.
28. Crowell, A. R., Culler, A. J., and McNamara, J. J., "Reduced Order Aerothermodynamics for Two-way Coupled Aerothermoelasticity in Hypersonic Flow," Proceedings of the International Forum on Aeroelasticity and Structural Dynamics, No. IFASD-2009-094, Seattle, Washington, June 2009.
29. McNamara, J. J., Friedmann, P. P., Crowell, A. R., and Gogulapati, A., "Reduced Order Modeling of Unsteady Hypersonic Aerodynamics," Proceedings of the International Forum on Aeroelasticity and Structural Dynamics, No. IFASD-2009-031, Seattle, Washington, June 2009.
30. Simpson, T. W., Mauery, T. M., Korte, J. J., and Mistree, F., "Kriging Models for Global Approximation in Simulation-Based Multidisciplinary Design Optimization," AIAA Journal, Vol. 39, No. 12, December 2001, pp. 2233-2241.
31. Kumano, T., Jeong, S., Obayashi, S., Ito, Y., Hatanaka, K., and Morino, H., "Multidisciplinary Design Optimization of Wing Shape for a Small Jet Aircraft Using Kriging Model," AIAA Paper 2006-932, January 2006.
32. Lam, X. B., Kim, Y. S., Hoang, A. D., and Park, C. W., "Coupled Aerostructural Design Optimization Using the Kriging Model and Integrated Multiobjective Optimization Algorithm," Journal of Optimization Theory and Applications, DOI 10.1007/s10957-009- 9520-9, March 2009.
33. Lophaven, S. N., Nielsen, H. B., and Sondergaard, J., "DACE A Matlab Kriging Toolbox Version 2.0," Technical Report IMMTR- 2002-12, August 2002.
34. Jin, R., Chen, W., and Sudjianto, A., "On Sequential Sampling for Global Metamodeling i Engineering Design," Proceedings of Design Engineering Technical Conferences and Computers and Information in Engineering Conference, September-October 2002, Montreal, Canada.
35. Glaz, B., Active/Passive Optimization of Helicopter Rotor Blades for Improved Vibration, Noise, and Performance Characteristics, Ph.D. Thesis, University of Michigan, Ann Arbor, Michigan, 2008.
36. Chung, H. S. and Alonso, J. J., "Comparison of Approximation Models with Merit Functions for Design Optimization," AIAA Paper 2000-4754, September 2000.
37. Falkiewicz, N. J. and Cesnik, C. E., "A Reduced-Order Modeling Framework for integrated Thermo-Elastic Analysis of Hypersonic Vehicles," Proceedings 50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Palm Springs, CA, 2009, AIAA Paper 2009-2308.
38. Sacks, J., Welch, W. J., Mitchell, T. J., andWynn, H. P., "Design and Analysis of Computer Experiments," Statistical Science, Vol. 4, No. 4, 1989, pp. 409-435.
39. Lumley, J. L., "The Structure of Inhomogeneous Turbulence," Proceedings of the International Colloquium on the Fine Scale Structure of the Atmosphere and its Influence on Radio Wave Propagation, Moscow, Dokl, Akad, Nauk SSSR, 1967, pp. 166-178.
40. Romanowski, M. C., "Reduced Order Unsteady Aerodynamic and Aeroelastic Models Using Karhunen-Loeve Eigenmodes," AIAA Paper 1996-3981, September 1996.
41. Queipo, N. V., Haftka, R. T., Shyy, W., Goel, T., Vaidyanathan, R., and Tucker, P. K., "Surrogate-Based Analysis and Optimization," Progress in Aerospace Sciences, Vol. 41, January 2005, pp. 1-28.
42. Hartwich, P. and Agrawal, S., "Perturbing Multiblock Patched Grids in Aeroelastic Design Optimization Applications," AIAA Paper 97-2038, June 1997.
43. Bartels, R. E., Rumsey, C. L., and Biedron, R. T., "CFL3D User's Manual - General Usage and Aeroelastic Analysis (Version 6.4)," NASA TM 2006-214301, 2006.
44. Dubac, L., Cantariti, F., Woodgate, M., Gribben, B., Badcock, K. J., and Richards, B. E., "A grid deformation technique for unsteady flow computations," International Journal for Numerical Methods in Fluids, Vol. 32, 2000, pp. 285-311.
45. Thompson, J., Bharat, S., and Weatherill, N., Handbook of Grid Generation, CRC Press, Boca Raton, FL, 1st ed., 1998.
46. Krist, S. L., Biedron, R. T., and Rumsey, C. L., "CFL3D User's Manual (Version 5.0)," NASA TM 1998-208444, 1997, CFL3D Version 6.0 update: http://cfl3d.larc.nasa.gov/Cfl3dv6/cfl3dv6.html.
47. Menter, F. R. and Rumsey, C. L., "Assessment of Two-Equation Turbulence Models for Transonic Flows," AIAA Paper 1994-2343, June 1994.
48. Roy, C. J. and Blottner, F. G., "Methodology for Turbulence Model Validation: Application to Hypersonic Flows," Journal of Spacecraft and Rockets, Vol. 40, No. 3, May-June 2003, pp. 313-325.
49. Rumsey, C. L., "Compressibility Considerations for k-w Turbulence Models in Hypersonic Boundary Layer Applications," NASA/TM2009-215705, April 2009.
50. McNamara, J. J., Friedmann, P. P., Powell, K. G., Thuruthimattam, B. J., and Bartels, R. E., "Aeroelastic and Aerothermoelastic Behavior in Hypersonic Flow," AIAA Journal, Vol. 46, No. 10, October 2008, pp. 2591-2610.
51. Rumsey, C. L., "Apparent Transition Behavior of Widely Used Turbulence Models," International Journal of Heat and Fluid Flow, Dec. 2007, Vol. 28, No. 6, pp. 1460 - 1471.