[1] Darabi, H., Roshanian, J., and Zare, H., "Design of Liquid Propellant Engine, Using Collaborative Optimization and Evolutionary Algorithms", The Institution of Mech. Engineers, Part G: J. Aerospace Eng., Spain, 2014.
[2] Thakre, P., Chemical Erosion of Graphite and Refractory Metal Nozzles and Its Mitigation in Solid-Propellant Rocket Motors, Proquest, Umi Dissertation Publishing, Ann Arbor, Michigan, USA, 2008.
[3] Bartz, D.R., "Turbulent Boundary-Layer Heat Transfer from Rapidly Accelerating Wow of Rocket Combustion Gases and of Heated Air", Jet Propulsion Lab., California, Tech. Rep. NASA-CR-62615, 1963.
[4] Back, L.H., Massier, P.F., and Gier, H.L. "Convective Heat Transfer in a Convergent-Divergent Nozzle", Int. J. Heat and Mass Transfer, Vol. 7, No. 5, pp. 549-568, 1964.
[5] Swann, R.T. and Pittman, C.M., "Numerical Analysis of the Transient Response of Advanced Thermal Protection Systems for Atmospheric Entry", NASA-TN-D-1370, L-1359, 1964.
[6] Chung, B.T.F., Chang, T.Y., Hsiao, J.S., and Chang, C.I., "Heat Transfer with Ablation in a Half Space Subjected to Time-Variant Heat Fluxes", J. Heat Transfer, Vol. 105, No. 1, pp. 200-203, 1983.
[7] Torres, Y., Stefanini, L., and Suslov, D., "Influence of Curvature in Regenerative Cooling System of Rocket Engine", Propulsion Physics, Vol. 1, pp. 171-184, 2009.
[8] Pizzarelli, M., Nasuti, F., and Onofri, M., "Trade-off Analysis of High-Aspect-Ratio-Cooling Channels for Rocket Engines", Int. J. Heat and Fluid Flow, Vol. 44, pp. 458-467, 2013.
[9] Coetzee, N., "Heat Transfer Coefficients of Smooth Tubes in the Turbulent Flow Regime", Dissertation, University of Pretoria, South Africa, 2015.
[10] Żyluk, A. and Pietraszek, M., "Investigation of an Additional Oxidizer Chage Effect on Elected Characteristics of a Solid-Fuel Rocket Engine", J. Theoretical and Appled Mech., Vol. 52, No. 1, pp. 139-149, 2014.
[11] Adami, A., Mortazavi, M., and Nosratollahi, M., "Heat Transfer Modeling of Bipropellant Thrusters for using in Multidisciplinary Design Optimization Algorithm", J. Fluid Flow, Heat and Mass Transfer, Vol. 2, pp. 40-46, 2015.
[12] Moore, S.S., "Ballistics Modeling of Combustion Heat Loss Through Chambers and Nozzles of Solid Rocket Motors", Dissertation, California State University, USA, 2010.
[13] Kays, W., Crawford, M. E., and Weigand, B., Convective Heat and Mass Transfer, 4th Ed., McGraw-Hill, New York, USA, 2005.
[14] Ahmad, R.A., "Convective Heat Transfer in the Reusable Solid Rocket Motor of the Space Transportation System", Heat Transfer Engineering, Vol. 26, No. 10, pp.30-45, 2005.
[15] Huzel, D.K. and Huang, D.H., "Modern Engineering for Design of Liquid-Propellant Rocket Engines", Volume 147 of Progress in Astronautics and Aeronautics, AIAA, 1992.
[16] Cross, P.G. and Boyd, I.D., "Two-dimensional Modeling of Ablation and Pyrolysis with Application to Rocket Nozzles.", The 46th AIAA Thermophysics Conf., p. 3383, 2016.
[17] Faridani, M. M., "Mathematical Modeling of Transpiration Cooling in Cylindrical Domain", Dissertation, Eastern Mediterranean University (EMU)-Doğu Akdeniz Üniversitesi (DAÜ), Turkey, 2015.
[18] Anderson, J. D., Computational Fluid Dynamics the Basic with Applications, McGraw-Hill, New York, USA, 1995.
[19] Ruffin, A., "Numerical Investigation of Nozzle Thermochemical Behaviour in Hybrid Rocket Motors (M.Sc. Thesis)", University of Padova, Italy, 2015.
[20] Razmjooei, M., Shahbazi, M., and Ommi, F.", Quasi-one-dimensional Modeling of Internal Ballistic in Solid Propellant Rocket, Considering Saderholm Erosive Burning Model", Iranian Scientific Association of Energetic Material, Vol. 13, No. 3, pp. 197-208, 2019.