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Annexes

• Duffa, G., Ablative thermal protection systems modeling, American Institute of Aeronautics and Astronautics, Inc., Reston, Virginia, 2013.
• Lachaud, J., Magin, T. E., Cozmuta, I., and Mansour, N. N., “A Short Review of Ablative-Material Response Models and Simulation Tools,” 7th European Symposium on Aerothermodynamics, edited by L. Ouwehand, SP-692, ESTEC-ESA, Brugge, Belgium, May 2011.
• Helber, B., Material Response Characterization of Low-Density Ablators in Atmospheric Entry Plasmas, Ph.D. thesis, Vrije Universiteit Brussel & von Karman Institute for Fluid Dynamics, Belgium, 2016.
• Schrooyen, P., Numerical Simulation of Aerothermal Flows Through Ablative Thermal Protection Systems, Ph.D. thesis, Université Catholique de Louvain & von Karman Institute for Fluid Dynamics, Belgium, Belgium, 2015.
• Schrooyen, P., Hillewaert, K., Magin, T., and Chatelain, P., “Fully Implicit Discontinuous Galerkin Solver to Study Surface and Volume Ablation Competition in Atmospheric Entry Flows,” International Journal of Heat and Mass Transfer, Vol. 103, 2016, pp. 108-124.
• Stackpoole, M., Sepka, S., Cozmuta, I., and Kontinos, D., “Post-Flight Evaluation of Stardus Sample Return Capsule Forebody Heatshield Material,” Journal of Thermophysics and Heat Transfer, Vol. 24, No. 4, 2010, pp. 694-707.
• Bottin, B., Carbonaro, M., Paris, S., Vanderhaegen, V., Novelli, A., and Vennemann, D., “VKI 1.2 MW Plasmatron Facility for the Thermal Testing of TPS Materials,” 3 rd European Workshop on Thermal Protection Systems, The Netherlands, March 1998.
• Bottin, B., Chazot, O., Carbonaro, M., Van Der Haegen, V., and Paris, S., “The VKI Plasmatron Characteristics and Performance,” Tech. rep., von Karman Inst. for Fluid Dynamics, Rhode-Saint-Genèse (Belgium), 2000.
• Mersen, “Calcarb rigid carbon thermal insulation,” Technical guide HT 29 GB 0121, Mersen, 2011.
• Whitaker, S., The Method of Volume Averaging, Vol. 13 of Theory and Applications of Transport in Porous Media, Springer Netherlands, 1st ed., 1999.
• Scoggins, J. and Magin, T. E., “Development of Mutation++: Multicomponent thermodynamic and transport property library for ionized plasmas written in C++,” 11th AIAA/ASME Joint Thermophysics and Heat Transfer Conference, AIAA Paper 2014-1966, Atlanta, GA, 16-20 June 2014.
• Turchi, A., Helber, B., Munafò, M. T and E., M. T., “Development and Testing of an Ablation Model Based on Plasma Wind Tunnel Experiments,” 11th AIAA/ASME Joint Thermophysics and Heat Transfer Conference, AIAA Paper 2014-1966, Atlanta, GA, 16-20 June 2014.
• Magin, T., A Model for Inductive Plasma Wind Tunnels, Ph.D. thesis, Université Libre de Bruxelles & Von Karman Institute for Fluid Dynamics, Belgium, 2004.
• Dullien, F., Porous media: fluid transport and pore structure, Academic Press, San Diego, 1991.
• Lachaud, J., Cozmuta, I., and Mansour, N. N., “Multiscale approach to ablation modeling of phenolic impregnated carbon ablators,” Journal of Spacecraft and Rockets, Vol. 47, No. 6, 2010, pp. 910-921.
• Park, C., Jaffe, R. L., and Partridge, H., “Chemical-kinetic parameters of hyperbolic earth entry,” Journal of Thermophysics and Heat Transfer, Vol. 15, No. 1, 2001, pp. 76-90.
• Lachaud, J., Mansour, N., Ceballos, A., Pejakovic, D., Zhang, L., and Marschall, J., “Validation of a volume-averaged fiber-scale model for the oxidation of a carbon-fiber preform,” 42nd AIAA Thermophysics Conference, No. AIAA 2011-3640, American Institute of Aeronautics and Astronautics, Honolulu, HA, 27-30 June 2011.
• Homann, F., “The effect of high viscosity on the flow around a cylinder and around a sphere,” Technical memorandum 1334, NACA, 1952, Translation of “Der Einfluss grosser Zähigkeit bei der Strömung um den Zylinder und um die Kugel”, ZAMM, vol. 16, no. 3, June 1936.
• Magin, T. E., “Cooled Pitot probe in air plasma jet,” I3. MS Seminar Series, Aachen, Germany, 13 July 2015
• Kendall, R. M., Barlett, E. P., Rindal, R. A., and Moyer, C. B., “An Analysis of the Coupled Chemically Reacting Boundary Layer and Charring Ablator: Part I.” CR-1060, NASA, 1968.
• Chen, Y.-K., Milos, F., and Gökcen, T., “Validation of a three-dimensional ablation and thermal response code,” 10th AIAA/ASME Joint Thermophysics and Heat Transfer Conference, No. AIAA 2010-4645, American Institute of Aeronautics and Astronautics, 28-30 June 2010.
• Dec, J., Braun, R., and Laub, B., “Ablative Thermal Response Analysis Using the Finite Element Method,” Journal of thermophysics and heat transfer, Vol. 26, No. 2, 2012, pp. 201-212.
• Panerai, F., Martin, A., Mansour, N. N., Sepka, S. A., and Lachaud, J., “Flow-tube oxidation experiments of the carbon preform of a phenolic-impregnated carbon ablator,” Journal of Thermophysics and Heat Transfer, Vol. 28, No. 2, 2014, pp. 181-190.