Thermoelastic formulation of a hypersonic vehicle control surface for control-oriented simulation

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2009, Pages

  Falkiewicz, Nathan J ^a   Cesnik, Carlos E S ^a   Bolenderz, Michael A ^b   Domanx, David B ^b  

^a UNIVERSITY OF MICHIGAN   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC CONFIGURATIONS; CONTROL SURFACES; CONTROL SYSTEM SYNTHESIS; DEFORMATION; FLIGHT CONTROL SYSTEMS; FLIGHT DYNAMICS; HEAT FLUX; HEAT TRANSFER; HYPERSONIC AERODYNAMICS; HYPERSONIC VEHICLES; LIFT; PROPULSION; THERMAL EXPANSION; VEHICLE PERFORMANCE;

AERO-DYNAMIC PERFORMANCE; CONTROL SURFACE DEFLECTION; DIFFERENTIAL THERMAL EXPANSION; FINITE-ELEMENT REPRESENTATION; FLUX BOUNDARY CONDITIONS; REFERENCE TEMPERATURE; STRUCTURAL DEFORMATION; STRUCTURAL DISPLACEMENT;

AERODYNAMIC DRAG;

EID: 78049291887     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2009-6284     Document Type: Conference Paper

References (18)

1. Oppenheimer, M., Skujins, T., Doman, D., and Cesnik, C., "Canard-Elevon Interactions on a Hypersonic Vehicle," Proceedings of the 2008 AIAA Atmospheric Flight Mechanics Conference, Honolulu, Hawaii, AIAA 2008-6383.
2. Skujins, T., Cesnik, C., Oppenheimer, M., and Doman, D., "Applicability of an Analytical Shock/Expansion Solution to the Elevon Control Effectiveness for a 2-D Hypersonic Vehicle Configuration," Proceedings of the 2008 AIAA Atmospheric Flight Mechanics Conference, Honolulu, Hawaii, AIAA 2008-6384.
3. Oppenheimer, M. and Doman, D., "A Hypersonic Vehicle Model Developed with Piston Theory," Proceedings of the 2006 AIAA Atmospheric Flight Mechanics Conference, Hilton Head, South Carolina, AIAA 2006-6637.
4. Oppenheimer, M., Skujins, T., Bolender, M., and Doman, D., "A Flexible Hypersonic Vehicle Model Developed with Piston Theory," Proceedings of the 2007 AIAA Atmospheric Flight Mechanics Conference, Hilton Head, South Carolina, AIAA 2007-6396.
5. Bolender, M., Oppenheimer, M., and Doman, D., "Effects of Unsteady and Viscous Aerodynamics on the Dynamics of a Flexible Air-Breathing Hypersonic Vehicle," Proceedings of the 2007 AIAA Atmospheric Flight Mechanics Conference, Hilton Head, South Carolina, AIAA 2007-6397.
6. Culler, A., Williams, T., and Bolender, M., "Aerothermal Modeling and Dynamic Analysis of a Hypersonic Vehicle," Proceedings of the 2007 AIAA Atmospheric Flight Mechanics Conference, Hilton Head, South Carolina, AIAA 2007-6395.
7. Culler, A., Crowell, A., and McNamara, J., "Studies on Fluid-Structural Coupling for Aerothermoelasticity in Hypersonic Flow," Proceedings of the 50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Palm Springs, California, AIAA 2009-2364.
8. Falkiewicz, N. and Cesnik, C., "A Reduced-Order Modeling Framework for Integrated Thermo-Elastic Analysis of Hypersonic Vehicles," Proceedings of the 50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Palm Springs, California, AIAA 2009-2308.
9. "Titanium Ti-6Al-2Sn-4Zr-2Mo (Ti-6-2-4-2), Duplex Annealed," http://www.matweb.com/search/DataSheet.aspx?matGUID= 3a01802b122647028633c9fa10e6bae8, Last Accessed 6/30/2009.
10. Myers, D., Martin, C., and Blosser, M., "Parametric Weight Comparison of Advanced Metallic, Ceramic Tile, and Ceramic Blanket Thermal Protection Systems," Tech. Rep. TM 2000-210289, NASA, June 2000.
11. Holman, J., Heat Transfer, McGraw-Hill, Inc., 8th ed., 1997.
12. Eckert, E., "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 American Society of Mechanical Engineers, Vol. 78, No. 6, August 1956.
13. Eckert, E., "Survey on Heat Transfer at High Speeds," Technical Report ARL 189, Aeronautical Research Laboratory, University of Minnesota, Minneapolis, MN, December 1961.
14. Huebner, K., Dewhirst, D., Smith, D., and Byrom, T., The Finite Element Method for Engineers, John Wiley and Sons, Inc., 4th ed., 2001.
15. Gould, P., Introduction to Linear Elasticity, Springer-Verlag, 2nd ed., 1994.
16. Chandrupatla, T. and Belegundu, A., Introduction to Finite Elements in Engineering, Prentice-Hall, Inc., 3rd ed., 2002.
17. "Equations, Tables, and Charts for Compressible Flow," Tech. Rep. NACA-1135, National Advisory Committee for Aeronautics, Ames Aeronautical Laboratory, Moffett Field, CA, 1953.
18. Anderson, J., Fundamentals of Aerodynamics, McGraw-Hill, Inc., 3rd ed., 2001.