International Scientific Journal


Attention in this work is focused on aerodynamic heating and aero-thermo-mechanical analysis of fin type structures on the missile at supersonic flight. At high Mach number the heat due to friction between body and flow, i.e. viscous heating must be taken into account because the velocity field is coupled with the temperature field. The flow field around the fins of the missile and especially the temperature distribution on its surface, as well as aerodynamic-thermal-structural analyses are numerically modeled in ANSYS Workbench environment. The investigation was carried out for two Mach numbers (M = 2.3 and M = 3.7). Own available structural experimental results have been used for computational structural mechanics (CSM) validation and verification, in order to assure credibility of numerical fluid-thermal-structure interaction (FTSI). Conducted simulations were carried out to better understand the FTSIs of the missile fin during supersonic flight.
PAPER REVISED: 2016-11-11
PAPER ACCEPTED: 2016-11-29
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THERMAL SCIENCE YEAR 2017, VOLUME 21, ISSUE Issue 6, PAGES [3037 - 3049]
  1. Van Driest, E. R., The Problem of Aerodynamic Heating, Aeronautical Engineering Review, 15 (1956), 10, pp. 26-41
  2. Hopkins, E. J., Inouye, M., An Evaluation of Theories for Predicting Turbulent Skin Friction and Hypersonic Mach Numbers, AIAA Journal, 9 (1971), 6, pp. 993-1003
  3. Poll, D. I. A., An Introduction to the Problem of Aerodynamic Heating, Aeronautical Engineering Internal Report 8901, 1989
  4. Quinn, R. D., Gong, L., Real-Time Aerodynamic Heating and Surface Temperature Calculations for Hypersonic Flight Simulation, NASA Technical Memorandum, NASA-TM-4222, 1990
  5. Wurster, K. E., Stone, H. W., Aerodynamic Heating Environment Definition/Thermal Protection System Selection for the HL-20, Journal of Spacecraft Rockets, 30 (1993), 5, pp. 549-557
  6. Nishikawa, H., Aerodynamic Heating with Turbulent Flows, AE525 Research Project, 1994
  7. Mazzoni, J. A., Filho, J. B. P., Machado, H. A., Aerodynamic heating on VSB-30 sounding rocket, Proceedings, 18th International Congress of Mechanical Engineering, Ouro Preto, MG, November, 2005
  8. Mahulikar, S. P., Theoretical aerothermal concepts for configuration design of hypersonic vehicles, Aerospace Science and Technology, 9 (2005), pp. 681-685
  9. Cayzac, R., et al., Navier-Stokes computation of heat transfer and aero-heating modeling for supersonic projectiles, Aerospace Science and Technology, 10 (2006), pp. 374-384
  10. Culler, A. J., Crowell, A. R., McNamara, J. J., Studies on Fluid-Structural Coupling for Aerothermoelasticity in Hypersonic Flow, Proceedings, 50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Palm Springs, California, May, 2009, AIAA Paper 2009-2364
  11. Kostoff, R. N., Cummings, R. M., Highly cited literature of high-speed compressible flow research, Aerospace Science and Technology, 26 (2013), pp. 216-234
  12. Bao, W., et al., Effect of structural factors on maximum aerodynamic heat flux of strut leading surface, Applied Thermal Engineering, 69 (2014), pp. 188-198
  13. Ocokoljić, G. J., at al., Aerodynamic shape optimization of guided missile based on wind tunnel testing and CFD simulation, Thermal Science - Online First, doi: 10.2298/TSCI1505151840
  14. Başkut, E., Akgül, A., Development of a Coupling Procedure for Static Aeroelastic Analyses, Scientific Technical Review, 61 (2011), 3-4, pp. 39-48
  15. Vidanović, N. D., Aerodynamic-structural optimization of aircraft lifting surfaces, Ph.D. thesis, (in Serbian), Faculty of Mechanical Engineering, University of Belgrade, Serbia, 2015
  16. Kroyer, R., FSI analysis in supersonic fluid flow, Computers & Structures, 81 (2003), pp. 755-764
  17. Friedmann, P. P., et al., Aeroelastic analysis of hypersonic vehicles, Journal of Fluids and Structures, 19 (2004), pp. 681-712
  18. Seo, Y-J, et al., Effects of multiple structural nonlinearities on limit cycle oscillation of missile control fin, Journal of Fluids and Structures, 27 (2011), pp. 623-635
  19. Firouz-Abadi, R. D., et al., Analysis of non-linear aeroelastic response of a supersonic thick fin with plunging, pinching and flapping free-plays, Journal of Fluids and Structures, 40 (2013), pp. 163-184
  20. Ognjanović, O., Maksimović, K., Stamenković, D., Vasić, Z., The Effects of Thermal Gradients on Stress Distributions, Proceedings, 4th International Congress of Serbian Society of Mechanics, Vrnjačka Banja, Serbia, June, 2013, pp. 365-370
  21. Rašuo, B., Aeronautical Safeguarding (VTOb), VIZ, Military Academy, Belgrade, 2004, (in Serbian)
  22. Design Modeler User's Guide, Release 15.0, ANSYS, Inc., November 2013.
  23. ANSYS Meshing User's Guide, Release 15.0, ANSYS, Inc., November 2013.
  24. Anderson, J. D., Jr., Computational Fluid Dynamics, The Basics with Applications, McGraw-Hill, Inc., Singapore, 1995
  25. ANSYS Fluent Theory Guide, Release 15.0, ANSYS, Inc., November 2013.
  26. ANSYS Fluent User's Guide, Release 15.0, ANSYS, Inc., November 2013.
  27. Menter, F. R., Two-Equation Eddy-Viscosity Turbulence Models for Engineering Applications, AIAA Journal, 32 (1994), 8, pp. 1598-1605
  28. Menter, F. R., Kuntz, M., Langtry, R., Ten Years of Industrial Experience with the SST Turbulence Model, in: Turbulence, Heat and Mass Transfer 4 (Ed. K. Hanjalić, Y. Nagano, M. Tummers), Begell House, Inc., 2003, pp. 625-632
  29. Menter, F. R., Review of the shear-stress transport turbulence model experience from an industrial perspective, International Journal of Computational Fluid Dynamics, 23 (2009), 4, pp. 305-316
  30. Vidanović, N. D., et al., Validation of the CFD code used for determination of aerodynamic characteristics of nonstandard AGARD-B calibration model, Thermal Science, 18 (2014), 4, pp. 1223-1233
  31. Rao, S. S., The Finite Element in Engineering, Elsevier, 2004
  32. System Coupling User's Guide, Release 15.0, ANSYS, Inc., November 2013.
  33. Kamakoti, R., Shyy, W., Fluid-structure interaction for aeroelastic applications, Progress in Aerospace Sciences, 40 (2004), pp. 535-558
  34. Jansen, K., Shakib, F., Hughes, T., Fast Projection Algorithm for Unstructured Meshes, in: Computational Nonlinear Mechanics in Aerospace Engineering (Ed. S. N. Atluri), American Institute of Aeronautics and Astronautics, 1992, pp. 175-204
  35. Galpin, P. F., Broberg, R. B., Hutchinson, B. R., Three-Dimensional Navier Stokes Predictions of Steady-State Rotor/Stator Interaction with Pitch Change, Proceedings, 3rd Annual Conference of the CFD Society of Canada, Banff, Alberta, Canada, June, 1995
  36. Maksimovic, S., et al., Determination of Load Distributions on Main Helicopter Rotor Blades and Strength Analysis of the Structural Components, Journal of Aerospace Engineering, 27 (2014), 6
  37. Maksimovic, S., Stress and strength analysis of fin-test Model 1, No: 023-01-M, Internal report of Military Technical Institute, Belgrade, 2001
  38. Rašuo, B., Aircraft Production Technology, University of Belgrade, Faculty of mechanical engineering, Belgrade, 1995, (in Serbian)
  39. ANSYS Mechanical APDL Element Reference, Release 15.0, ANSYS, Inc., November 2013

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