[1] Binder, M., n RL10A-3-3A Rocket Engine Model using the Rocket Engine Transient Simulator (ROCETS) Software, NASA Contractor Report 190786, 1993.
[2] LeClair, A.C. and Majumdar, A.K., “Computational Model of the Chilldown and Propellant Lloading of the Space Shuttle External Tank,” AIAA, Vol. 6561, 2010, p. 2010.
[3] Kanmuri, A., Wakamatsu, Y., Kanda, T.,
Torii, Y., and et.al., Transient Analysisof LOX/LH2 Rocket Engine (LE-7),” Monterey, CA (US); AIAA1989.
[4] Cai, G., Fang, J., Xu, X. and Liu, M. “Performance Prediction and Optimization for Liquid Rocket Engine Nozzle,” Aerospace Science and Technology, Vol. 11, 2007, pp. 155-162.
[5] Van Overbeke T. J., and Shuen, J. S. “A Numerical Study of Chemically Reacting Flow in Nozzles,” AIAA-89-2793, California, July 10-12, 1989.
[6] Zhang, H. He, Y. and Tao, W., “Numerical Study of Film and Regenerative Cooling in a Thrust Chamber at High Pressure,” Numerical Heat Transfer, Part A: Applications, Vol. 52, 2007, pp. 991-1007.
[7] Marchi, Ch. H., Laroca, F., Silva,
A. F.C. D. and Hinckel, J. N. “Numerical Solutions of Flows in Rocket Engines with Regenerative Cooling,”
Numerical Heat Transfer, Part A: Applications, Vol. 45, Issue 7, 2004, pp. 699-717.
[8] Naraghi, M. H., “RTE-A Computer Code for Three-Dimensional Rocket Thermal Evaluation,” User Manual, Tara Technologies, LLC, Yorktown Heights, NY, Vol. 6, 2002, pp. 27-30.
[9] Dunn, S., Coats, D. and French, J., “TDK’02™ Two-Dimensional Kinetics (TDK) Nozzle Performance Computer Program,” User’s Manual, Prepared by Software & Engineering Associates, Inc, 2002.
[10] Naraghi, M., Dunn, S. and Coats, D., “A Model for Design and Analysis of Regeneratively Cooled Rocket Engines,” AIAA paper, Vol. 3852, 2004, p. 2004.
[11] Frölich, A., Popp, M., Schmidt, G. and Thelemann, D., “Heat Transfer Characteristics of H2/O2 –Combustion Chambers,” AIAA Paper 93-1826, June 1993.
[12] Poramir and A. F. Tabatabaee, “Numerical Solution of Three Dimentional Heat Transfer Through the Combustion Chamber and Study of Treatment of Coolant Flow in the Cooling Channel,” 6th Iranian Aerospace Conference, K. N. Toosi Univercity, Tehran, Iran, Feb. 1385, (in Persian).
[13] Asadallahi and Mollahajian, A. “Study and Optimization Regeneration Cooling System in the Nozzle of Liquid Rocket Engine,” 7th Iranian Aerospace Conference, Sharif University of Technology, Tehran, Iran, Feb. 1386, (in Persian).
[14] M. Eisakhani, Simulation of Phisycal and Geometric Parameters Effects in Regenerative Cooling, (M.S. ThesisP, Tarbiat Modares University, Tehran, Iran, Sep. 1381, (in Persian).
[15] Shine, S., Kumar, S. S. and Suresh, B., “A new Generalised Model for Liquid Film Cooling in Rocket Combustion Chambers,,” International Journal of Heat and Mass Transfer, Vol. 55, 2012, pp. 5065-5075.
[16] Gomet, L., Robin, V. and Mura, A. “Lagrangian Modelling of Turbulent Spray Combustion Under Liquid Rocket Engine Conditions,” Acta Astronautica, Vol. 94, 2014, pp. 184-197.
[17] Karimi, H., Nassirharand, A. and Mohseni, M. “Modeling and Simulation of a Class of Liquid Propellant Engine Pressurization Systems,” Acta Astronautica, Vol. 66, 2010, pp. 539-549.
[18] Kim, S.-K. and et al., “Multidisciplinary Simulation of a Regeneratively Cooled Thrust Chamber of Liquid Rocket Engine: Turbulent combustion and nozzle flow,” International Journal of Heat and Mass Transfer, Vol. 70, 2014. pp. 1066-1077.
[19] Urbano, A. and et al., “Exploration of Combustion Instability Triggering using Large Eddy Simulation of a Multiple Injector Liquid Rocket Engine,” Combustion and Flame, Vol. 169, 2016. pp. 129-140.
[20] Yang, W. and B. Sun, “Numerical Simulation of Liquid Film and Regenerative Cooling in a Liquid Rocket,” Applied Thermal Engineering, Vol. 54, No. 2, pp. 460-469.
[21] Guo,Y., Chan, C. C. K., . Lau, K. S. “A Pure Eulerian Model for Simulating Dilute Spray Combustion,” Elsevier Science, Fuel 81, 2002, pp. 2131-2144.
[22] De Giorgi, M. G., Sciolti, A. and Ficarella, A. “DifferentCombustion ModelsAppliedtoHighPressure LOX/CH4 jet Flames,” 4th European Conference for Aerospace Sciences, Saint Petersburg, Russia , July 2011.
[23] Yen-Sen Chen, A ., Chou, T.H., Gu, B.R., Wu, J.S., Wu, B., Lian,Y.Y., Yang, L., “Multiphysics Simulations of Rocket Engine Combustion,” Elsevier, Computers & Fluids, Vol. 45, Issue 1, 2011, pp. 29-36.
Ulas, A. and Boysan, E., “Numerical Analysis of Regenerative Cooling in Liquid Propellant Rocket Engines,” Aerospace Science and Technology, Vol. 24, No. 1, 2013, p.p. 187-197.
)
