Yakimov, A.S. "Calculation of Heat Exchange Characteristics Transpiration Cooling Systems." Applied Mechanics & Materials. 2015, 756, 365-371.
 Turner, M. J. “Rocket and Spacecraft Propulsion: Principles, Practice and New Developments”; Springer Science & Business Media. 2008, 3, 153-228.
 Swann, R.T. and C.M. Pittman, Numerical analysis of the transient response of advanced thermal protection systems for atmospheric entry1962: National Aeronautics and Space Administration.
 Chung, B., et al., Heat transfer with ablation in a half space subjected to time-variant heat fluxes. Journal of heat transfer, 1983. 105(1): p. 200-203.
 Blackwell, B., Numerical prediction of one-dimensional ablation using a finite control volume procedure with exponential differencing. Numerical Heat Transfer, Part A: Applications, 1988. 14(1): p. 17-34.
 Ren, F., H. Sun, and G. Deng, A theoretical calculation method of local ablation in region of shock-boundary layer interaction, in 6th Joint Thermophysics and Heat Transfer Conference1994, American Institute of Aeronautics and Astronautics.
 Zien, T.-F. and C.-Y. Wei, Heat transfer in the melt layer of a simple ablation model. Journal of thermophysics and heat transfer, 1999. 13(4): p. 450-459.
 Braga, W.F., M.B. Mantelli, and J.L.F. Azevedo. Approximate analytical solution for onedimensional ablation problem with time-variable heat flux. in AIAA Thermophys. Conference. 2003.
 Kuo, K. K. and Keswani, S. T., "A Comprehensive Theoretical Model for Carbon-Carbon Composite Nozzle Recession," Combustion Science and Technology, Vol. 42, No. 3-4, 1985, pp. 145-164.
 Thakre, P. and Yang, V., "Chemical Erosion of CarbonCarbon/Graphite Nozzles in Solid-Propellant Rocket Motors," Journal of Propulsion and Power, Vol. 24, No. 4, 2008, pp. 822-833.
 Bianchi, D., Nasuti, F., and Martelli, E., "Coupled Analysis of Flow and Surface Ablation in Carbon-Carbon Rocket Nozzles," Journal of Spacecraft and Rockets, Vol. 46, No. 3, 2009, pp. 492-500.
 Bianchi, D. and Nasuti, F., "Analysis of Carbon-Carbon Nozzle Erosion with Shape-Change Effects in Full-Scale Solid-Rocket Motors," Journal of Propulsion and Power, Vol. 28, No. 4, 2012, pp. 820-830.
 Riise, J.A.K., Computer Code for Thermal Analysis of Rocket Motors. 2008.
 Mohammadiun, H. and M. Mohammadiun, Numerical Modeling of Charring Material Ablation with Considering Chemical-Reaction Effects, Mass Transfer and Surface Heat Transfer. Arabian Journal for Science and Engineering, 2013. 38(9): p. 2533-2543.
 Ghaderi Dehkordi, Y., "Investigation of the Effect of Reinforcement on Thermo-Physical Properties of Ablative Heat Shields,” Vol. 3, No. 2, Journal of Aerospace Research Technology, summer 2010, pp. 55-65.
 Turchi, Alessandro. A gas-surface interaction model for the numerical study of rocket nozzle flows over pyrolyzing ablative materials. Diss. PhD thesis, Von Karman Institute for Fluid Dynamics, 2013.
 Cross PG, Boyd ID. Two-Dimensional Modeling of Ablation and Pyrolysis with Application to Rocket Nozzles. Journal of Spacecraft and Rockets. 2016 Oct 21;54(1):212-24.
 Kato, Sumio, Keiichi Okuyama, Kenta Gibo, Takuma Miyagi, Toshiyuki Suzuki, Kazuhisa Fujita, Takeharu Sakai, Seiji Nishio, and Akihiro Watanabe. "Thermal Response Simulation of Ultra Light Weight Phenolic Carbon Ablator by the Use of the Ablation Analysis Code." TRANSACTIONS of the Japan N Society for Aeronautical and Space Sciences, Aerospace Technology Japan 10, No. ists 28, 2012, pp. 31-39.
 Bae, J. "Development of Equilibrium Flow CFD Code Using CEA Database and Prediction on Ablation of SiC Coating Nozzle." PhD diss., Master Dissertation, Seoul National University, 2017.
 Bucchi, Andrea, Claudio Bruno, and Alessandro Congiunti. "Investigation of transpiration cooling performance in LOX/Methane liquid rocket engines." Journal of Spacecraft and Rockets, vol. 42, no. 3, 2005, pp. 476-486,.
 Kuzenov, V. V., and S. V. Ryzhkov. "Approximate method for calculating convective heat flux on the surface of bodies of simple geometric shapes." In Journal of Physics: Conference Series, vol. 815, no. 1, p. 012024. IOP Publishing, 2017.
 Amirhossein Adami, Mahdi Mortazavi and Mehran Nosratollahi,” Heat Transfer Modeling of Bipropellant Thrusters for using in Multidisciplinary Design Optimization Algorithm”, Journal of Fluid Flow, Heat and Mass Transfer, Volume: 2, 2015.
 Kanevce, Ljubica P., Gligor H. Kanevce, and Zore Z. Angelevski. "Comparison of two kinds of experiments for estimation of thermal properties of ablative composite." In Proceedings of the 3º International Conference on Inverse Problems in Engineering, Port Ludlow, USA. 1999.
 Ahmadi, A., "One-dimensional Investigation of Ablatin in The Nozzle Throat", 9th Conference on Fluid Dynamics, 1383.
Bianchi, Daniele. "Modeling of ablation phenomena in space applications." 2008.