THERMAL SCIENCE

International Scientific Journal

Authors of this Paper

External Links

INSIGHT INTO CHEMICAL REACTION KINETICS EFFECTS ON THERMAL ABLATION OF CHARRING MATERIAL

ABSTRACT
Thermal ablation plays an important role in the aerospace field. In this paper, to study the chemical kinetics effects on heat transfer and surface ablation of the charring ablative material during aerodynamic heating, a charring ablation model was established using the finite element method. The AVCOAT 5026-39H/CG material, one typical thermal protection material used in thermal protection system, was employed as the ablative material and heated by aerodynamic heating condition experienced by Apollo 4. The finite element model considers the decomposition of the resin within the charring material and the removal of the surface material, and uses Darcy’s law to simulate the fluid-flow in the porous char. Results showed that the model can be used for the ablation analysis of charring materials. Then effects of chemical kinetics on ablation were discussed in terms of four aspects, including temperature, surface recession, density distribution, and mass flux of pyrolysis gas. The pre-exponential factor and activation energy have different effects on ablation, while the effect of the reaction order is little. This paper is helpful to understand the heating and ablation process of charring ablative materials and to provide technical references for the selection and design of thermal protection materials.
KEYWORDS
PAPER SUBMITTED: 2020-10-10
PAPER REVISED: 2020-12-08
PAPER ACCEPTED: 2020-12-14
PUBLISHED ONLINE: 2021-03-27
DOI REFERENCE: https://doi.org/10.2298/TSCI201010085X
CITATION EXPORT: view in browser or download as text file
THERMAL SCIENCE YEAR 2022, VOLUME 26, ISSUE Issue 1, PAGES [529 - 543]
REFERENCES
  1. Anderson, J.D., Hypersonic and high temperature gas dynamics, AIAA, 2000.
  2. Suzuki, T., et al., Calculation of thermal response of ablator under arcjet flow condition, Journal of Thermophysics and Heat Transfer, 21 (2007), pp. 257-266.
  3. Huang, H., et al., The inverse problem in zero linear ablation of aluminizing carbon composites under high heat flux, Thermal Science, 17 (2013), pp. 1323-1327.
  4. Huang, H.M., et al., Thermal analysis of charring materials based on pyrolysis interface model, Thermal Science, 18 (2014), pp. 1591-1596.
  5. Kendall, R.M., et al., A multicomponent boundary layer chemically coupled to an ablating surface, AIAA Journal, 5 (1967), pp. 1063-1071.
  6. Chen, Y.K., Milos, F.S., Ablation and thermal response program for spacecraft heatshield analysis, Journal of Spacecraft and Rockets, 36 (1999), pp. 475-483.
  7. Chen, Y.K., Milos, F.S., Two-dimensional implicit thermal response and ablation program for charring materials, Journal of Spacecraft and Rockets, 38 (2001), pp. 473-481.
  8. Chen, Y.K., Milos, F.S., Multidimensional finite volume fully implicit ablation and thermal response code, Journal of Spacecraft and Rockets, 55 (2018), pp. 914-927.
  9. Li, W., et al., Nonlinear analysis on thermal behavior of charring materials with surface ablation, International Journal of Heat and Mass Transfer, 84 (2015), pp. 245-252.
  10. Li, W., et al., A nonlinear pyrolysis layer model for analyzing thermal behavior of charring ablator, International Journal of Thermal Sciences, 98 (2015), pp. 104-112.
  11. Li, W., et al., A new mechanism of surface ablation of charring materials for a vehicle during reentry, Applied Thermal Engineering, 106 (2016), pp. 838-849.
  12. Li, W., et al., Influence factors on the multi-field coupling performances of charring ablators on the basis of a mesoscopic ablation model, Applied Thermal Engineering, 161 (2019), pp. 114-126.
  13. Li, W., et al., Novel designs of charring composites based on pore structure control and evaluation of their thermal protection performance, International Journal of Heat and Mass Transfer, 129 (2019), pp. 59-73.
  14. Scoggins, J., et al., Development of reduced kinetic mechanism for PICA pyrolysis products, in: 42nd AIAA Thermophysics Conference, American Institute of Aeronautics and Astronautics, 2011.
  15. Lachaud, J. T., et al., Detailed chemical equilibrium model for porous ablative materials, International Journal of Heat and Mass Transfer, 90 (2015), pp. 1034-1045.
  16. Dec, J.A., Braun, R.D., Three-dimensional finite element ablative thermal response and design of thermal protection systems, Journal of Spacecraft and Rockets, 50 (2013), pp. 725-734.
  17. Dec, J.A., et al., Ablative thermal response analysis using the finite element method, Journal of Thermophysics and Heat Transfer, 26 (2012), pp. 201-212.
  18. Risch, T.K., Verification of a finite element model for pyrolyzing ablative materials, AIAA Thermophysics Conference, 2017, p. 3354.
  19. Lattimer, B.Y., et al., Thermal response of composite materials to elevated temperatures, Fire Technology, 47 (2009), pp. 823-850.
  20. Li, W., et al., Effects of gradient density on thermal protection performance of AVCOAT composites under varied heat flux, Polymer Composites, 37 (2016), pp. 1034-1041.
  21. Li, W., et al., Nonlinear pyrolysis layer model for thermal behavior of nonhomogeneous charring materials, Journal of Applied Polymer Science, 132 (2015), pp. 423-431.
  22. Li, W., et al., On the novel designs of charring composites for thermal protection application in reentry vehicles, Applied Thermal Engineering, 93 (2016), pp. 849-855.
  23. Curry, D.M., Stephens, E.W., Apollo ablator thermal performance at superorbital entry velocities, National Aeronautics and Space Administration, (1970).
  24. Mouritz, A.P., et al., Review of fire structural modelling of polymer composites, Composites Part A-Applied Science and Manufacturing, 40 (2009), pp. 1800-1814.
  25. Park, J.M., et al., Effects of carbon nanotubes and carbon fiber reinforcements on thermal conductivity and ablation properties of carbon/phenolic composites, Composites Part B-Engineering, 67 (2014), pp. 22-29.
  26. Milos, F., et al., Arcjet testing and thermal model development for multilayer felt reusable surface insulation, Journal of Spacecraft and Rockets, 51 (2014), 2, pp. 397-411.
  27. Johansson, B.T., et al., A meshless method for an inverse two-phase one-dimensional nonlinear Stefan problem, Mathematics and Computers in Simulation, 101 (2014), pp. 61-77.
  28. Cui, M., et al., A new approach for the estimation of temperature-dependent thermal properties by solving transient inverse heat conduction problems, International Journal of Thermal Sciences, 58 (2012), pp. 113-119.
  29. Hosseini, S.A., et al., Extension of the operational Tau method for solving 1-D nonlinear transient heat conduction equations, Journal of King Saud University Science, 25 (2013), pp. 283-288.
  30. Yang, X.H., et al., Influence of non-conducting pore inclusions on phase change behavior of porous media with constant heat flux boundary, International Journal of Thermal Sciences, 64 (2013), pp. 137-144.
  31. Khajehpour, S., et al., A domain decomposition method for the stable analysis of inverse nonlinear transient heat conduction problems, International Journal of Heat and Mass Transfer, 58 (2013), pp. 125-134.
  32. Belghazi, H., et al., Analytical solution of unsteady heat conduction in a two-layered material in imperfect contact subjected to a moving heat source, International Journal of Thermal Sciences, 49 (2010), pp. 311-318.
  33. Huang, H. X., et al., Thermal response of heat-resistant layer with pyrolysis, Thermal Science, 16 (2012), pp. 69-78.
  34. Shen, Y. N., et al., Modeling pulsed laser ablation of aluminum with finite element analysis considering material moving front, International Journal of Heat and Mass Transfer, 113 (2017), pp. 1246-1253.
  35. Wang, Y., Multiphysics analysis of lightning strike damage in laminated carbon/glass fiber reinforced polymer matrix composite materials: a review of problem formulation and computational modeling, Composites Part A-Applied Science and Manufacturing, 101 (2017), pp. 543-553.
  36. Wang, Y., Modeling ablation of laminated composites: a novel manual mesh moving finite element analysis procedure with ABAQUS, International Journal Heat and Mass Transfer, 116 (2018), pp. 306-313.
  37. Wang, Y., et al., Modeling of pyrolyzing ablation problem with ABAQUS: a one-dimensional test case, Journal of Thermophysics and Heat Transfer, 32 (2018), pp. 544-548.
  38. Wang, Y., et al., Assessment of a one-dimensional finite element charring ablation material response model for phenolic-impregnated carbon ablator, Aerospace Science and Technology, 91 (2019), pp. 301-309.

© 2024 Society of Thermal Engineers of Serbia. Published by the Vinča Institute of Nuclear Sciences, National Institute of the Republic of Serbia, Belgrade, Serbia. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution-NonCommercial-NoDerivs 4.0 International licence