بهینه‌سازی سیستم خنک‌کننده موتور موشک با سوخت هیدروژن مایع/اکسیژن مایع با استفاده از الگوریتم زنبورعسل

[1] Yang V, Habiballah M, Popp M, Hulka J. Liquid Rocket Thrust Chambers: Aspects of Modeling, Analysis and Design. American Institute of Aeronautics and Astronautics, In C. 2005.##

[2] Yang Z, Ma Y, Zhang N, Smith R. Design optimization of shell and tube heat exchangers sizing with heat transfer enhancement. Computers & Chemical Engineering. 2020; 137:106821.##

[3] Xu G, Zhuang L, Dong B, Liu Q, Wen J. Optimization design with an advanced genetic algorithm for a compact air-air heat exchanger applied in aero engine. International Journal of Heat and Mass Transfer. 2020; 158:119952.##

[4] Bozorgan N, Ghafouri A, Assareh E., Safieddin Ardebili SM. Design and Optimization of Gasketed-Plate Heat Exchanger using Bees Algorithm. International Journal of Advanced Design and Manufacturing Technology. 2021; 14(3):55-64.##

[5] Du Y, Hu C, Yang C, Wang H, Dong W. Size optimization of heat exchanger and thermoeconomic assessment for supercritical CO2 recompression Brayton cycle applied in marine. Energy. 2022; 239:122306.##

[6] Alimohammadi HR, Naseh H, Ommi F. A Novel Framework for Liquid Propellant Engine’s Cooling System Design By Sensitivity Analysis Based on RSM and Multi-objective Optimization Using PSO. Advances in Space Research. 2021; 67(5):1682-1700.##

[7] Song J, Cui P, Li Q, Cheng P, Chen L, Liang T. System scheme and thermal performance of a third fluid cooled rocket engine. Acta Astronautica. 2022; 191:204-215.##

[8] Lee SB, Lim TK, Roh TS. Design optimization of liquid rocket engine using a genetic algorithm, Journal of the Korean of Propulsion Engineers. 2021; 16:25-33.##

[9] Saqlain A, He LS. Optimization and sizing for propulsion system of liquid rocket using genetic algorithm. Chinese Journal of Aeronautics. 2007; 20:40-60.##

[10] Shafaee M, Mohammad Zadeh P, Elkaie A, Fallah H. Design optimization of a thrust chamber using a mass-based model to improve the geometrical and performance parameters of low-thrust space propulsion systems. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 2018; 233: 095441001876728.##

[11] Ramesh D, Farrokhi R. Proposing a new strategy to determine optimal parameters for open cycle liquid propellant engines. conference of Iran aerospace association. 2006; Tehran, Iran.##

[12] Bozorgan N, Ghafouri A, Assareh E, Safieddin Ardebili SM. Design and optimization of a gas turbine regenerator with fixed pressure drop using GA and firefly algorithms. Journal of Theoretical and Applied Mechanics. 2020; 58(4): 943-952.##

[13] Garcia JCS, Tanaka H, Giannetti N, Sei Y, Saito K, Houfuku M, Takafuji R. Multiobjective geometry optimization of microchannel heat exchanger using real-coded genetic algorithm. Applied Thermal Engineering. 2022; 202:117821.

[14] Han U, Kang H, Lim H, Han J, Lee H. Development and design optimization of novel polymer heat exchanger using the multi-objective genetic algorithm. International Journal of Heat and Mass Transfer. 2022; 144:117821.##

[15] Wang C, Cui Z, Yu H, Chen K, Wang J. Intelligent optimization design of shell and helically coiled tube heat exchanger based on genetic algorithm. International Journal of Heat and Mass Transfer. 2020; 159:120140.##

[16] Zarea H, Kashkooli FM, Mehryan AM, Saffarian MR, Beherghani EN. Optimal design of plate-fin heat exchangers by a Bees Algorithm. Applied Thermal Engineering. 2014; 69:267-277.##

[17] Pham DT, Ghanbarzadeh A, Koc E, Otri S, Rahim S, Zaidi M. The Bees Algorithm Technical Note. Manufacturing Engineering Centre. 2005; Cardiff University. UK.##

[18] Daneshgar S, Zahedi R. Optimization of power and heat dual generation cycle of gas microturbines through economic, exergy and environmental analysis by bee algorithm. Energy Reports. 2022; 8:1388-1396.##

[19] Veris ADL. Fundamental concepts of liquid-propellant rocket engines, Springer Aerospace Technology, 2019.##

[20] Wang ZG. Internal Combustion Processes of Liquid Rocket Engines: Modeling and Numerical Simulations. Wiley Aeronautic & Aerospace Engineering, 2016.##

[21] Bartz DR. Turbulent boundary-layer heat transfer from rapidly accelerating flow of rocket combustion gases and of heated air. NASA CR-62615. Jet Propulsion Laboratory. 1963; California Institute of Technology, Pasadena, California, USA.##

[22] Wang Q, Wu F, Zeng M, Luo L, Sun J. Numerical simulation and optimization on heat transfer and fluid flow in cooling channel of liquid rocket engine thrust chamber. Engineering Computations. 2006; 23(8):907-921.##

[23] Mishra DP. Fundamentals of rocket propulsion, Taylor & Francis, 2017.##

[24] Huzel DK, Huang DH. Modern engineering for design of liquid-propellant rocket engines, American Institute of Aeronautics and Astronautics, 1992.##

[25] Locke JM, Landrum DB. Study of heat transfer correlations for supercritical hydrogen in regenerative cooling channels. Journal of Propulsion and power. 2008; 24(1):94-103.##