ZHANG Meng1,SUN Bing1. Analysis of Influence Factors for Methane Transcritical Heat Transfer Deterioration[J]. Journal of Propulsion Technology, 2020, 41(2): 382-389.
[1] 蔡国飙, 李家文, 田爱梅, 等 . 液体火箭发动机设计[M]. 北京: 北京航空航天大学出版社, 2011.
[2] 章思龙, 秦 江, 周伟星, 等 . 高超声速推进再生冷却研究综述[J]. 推进技术, 2018, 39( 10): 2177- 2190.
[3] Tomita T , Ueda S , Kawashima H , et al . Status of Experimental Research on High Performance Methane-Fueled Rocket Thrust Chamber[R]. AIAA 2011- 5935.
[4] Locke J , Pal S , Woodward R . Chamber Wall Heat Flux Measurements for a LOX/CH 4 Uni-element Rocket [R]. AIAA 2007- 5547.
[5] Wang T S , Luong V . Hot-Gas-Side and Coolant-Side Heat Transfer in Liquid Rocket Engine Combustors[J]. Journal of Thermophysics and Heat Transfer, 1994, 8( 3): 524- 530.
[6] Liu Q , Luke E A , Cinnella P . Coupling Heat Transfer and Fluid Flow Solvers for Multidisciplinary Simulations[J]. Journal of Thermophysics and Heat Transfer, 2005, 19( 4): 417- 427.
[7] Song J W , Sun B . Coupled Numerical Simulation of Combustion and Regenerative Cooling in LOX/Methane Rocket Engines[J]. Applied Thermal Engineering, 2016, 106( 8): 762- 773.
[8] Song J W , Sun B . Coupled Heat Transfer Analysis of Thrust Chambers with Recessed Shear Coaxial Injectors[J]. Acta Astronautica, 2017, 132( 3): 150- 160.
[9] 康玉东, 孙 冰 . 再生冷却通道跨临界甲烷流动传热研究[J]. 航空动力学报, 2010, 25( 11): 2494- 2497.
[10] Urbano A , Nasuti F . Onset of Heat Transfer Deterioration in Supercritical Methane Flow Channels[J]. Journal of Thermophysics and Heat Transfer, 2013, 27( 2): 298- 308.
[11] Urbano A , Nasuti F . Parametric Analysis of Heat Transfer to Supercritical-Pressure Methane[J]. Journal of Thermophysics and Heat Transfer, 2012, 26( 3): 451- 463.
[12] Wang L L , Chen Z J , Meng H . Numerical Study of Conjugate Heat Transfer of Cryogenic Methane in Rectangular Engine Cooling Channels at Supercritical Pressures[J]. Applied Thermal Engineering, 2013, 54( 1): 237- 246.
[13] Wang Y Z , Hua Y X , Meng H . Numerical Studies of Supercritical Turbulent Convective Heat Transfer of Cryogenic-Propellant Methane[J]. Journal of Thermophysics and Heat Transfer, 2010, 24 ( 3): 490- 500.
[14] Pizzarelli M , Nasuti F , Onofri M , et al . Heat Transfer Modeling for Supercritical Methane Flowing in Rocket Engine Cooling Channels[J]. Applied Thermal Engineering, 2015, 75( 1): 600- 607.
[15] 康玉东, 孙 冰 . 燃气非平衡流再生冷却流动传热数值模拟[J]. 推进技术, 2011, 32( 1): 119- 124.
[16] Votta R , Battista F , Salvatore V , et al . Experimental Investigation of Transcritical Methane Flow in Rocket Engine Cooling Channel[J]. Applied Thermal Engineering, 2016, 101( 5): 61- 70.
[17] Shokri M , Ebrahimi A . Improvement of Heat-Transfer Correlations for Supercritical Methane Coolant in Rectangular Channel[J]. Applied Thermal Engineering, 2019, 147: 216- 230.