Progress of Coupled Heat Transfer Mechanisms of Regenerative Cooling System in a Scramjet by Ni He, Chaoyang Liu, Yu Pan, Jian Liu

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The Influence of Thrust Chamber Structure Parameters on Regenerative Cooling Effect with Hydrogen Peroxide as Coolant in Liquid Rocket Engines by Chuang Zhou, Nanjia Yu, Shuwen Wang, Shutao Han, Haojie Gong, Guobiao Cai, Jue Wang

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Experiments on Heat Transfer of Supercritical Pressure Kerosene in Mini Tube under Ultra-High Heat Fluxes by Jianguo Yan, Shouchun Liu, Pengcheng Guo, Qincheng Bi

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Numerical Study on the Effect of Buoyancy on Heat Transfer and Flow of Aviation Kerosene by YAO Changxin

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Numerical Study on Flow and Heat Transfer of Supercritical Hydrocarbon Fuel in Curved Cooling Channel by Ying Zhang, Yong Cao, Keyu Gong, Shuyuan Liu, Limin Wang, Zhengchun Chen

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A Coupled Heat Transfer Calculation Strategy for Composite Cooling Liquid Rocket Engine by Bo Xu, Bing Chen, Jian Peng, Wenyuan Zhou, Xu Xu

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A Parametrical Study on Convective Heat Transfer between High-Temperature Gas and Regenerative Cooling Panel by Jiangyu Hu, Ning Wang, Jin Zhou, Yu Pan

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Comparison and Evaluation of Transport Property Prediction Performance of Supercritical Hydrocarbon Aviation Fuels and Their Pyrolyzed Products via Endothermic Reactions by Sung-rok Hwang, Hyung Ju Lee

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Heat transfer and flow structures of supercritical n-decane in a regenerative cooling channel loaded with non-uniform heat flux by Jian Liu, Mengyao Xu, Kai Ma, Chaoyang Liu, Wenxiong Xi

Subjects: “…regenerative cooling…”
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Thermodynamic performance and flow structures analysis of supercritical CO2 applied in a regenerative cooling channel mounted with mini-ribs by Mengyao Xu, Jian Liu, Wenxiong Xi, Chaoyang Liu, Bengt Sunden

Subjects: “…Regenerative cooling…”
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Development and research testing of a low thrust on gaseous-propellant rocket engine chamber by A. I. Musteikis, A. A. Levikhin, S. V. Kolosenok

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Model validation and parametric study of fluid flows and heat transfer of aviation kerosene with endothermic pyrolysis at supercritical pressure by Keke Xu, Hua Meng

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Working state map of hydrocarbon fuels for regenerative cooling by Chen Zhang, Hui Gao, Jiajun Zhao, Guice Yao, Dongsheng Wen

Subjects: “…Regenerative cooling…”
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Study on the heat transfer characteristics of regenerative cooling for LOX/LCH4 variable thrust rocket engine by Jie Song, Tao Liang, Qinglian Li, Peng Cheng, Dongdong Zhang, Peng Cui, Jun Sun

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Heat Transfer and Flow Structure Characteristics of Regenerative Cooling in a Rectangular Channel Using Supercritical CO₂ by Jian Liu, Mengyao Xu, Pengchao Liu, Wenxiong Xi

Subjects: “…regenerative cooling…”
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Numerical Analysis of a Supercritical Heat Transfer of Cryogenic Methane in Regeneratively Cooled Rocket Engine by Mohammed Amine DJEFFAL, Nabil BENAMARA, Abdelkader LAHCENE, Ali BENOUAR, Abdelkader BOULENOUAR, Mohammed MERZOUG

Subjects: “…regenerative cooling…”
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Numerical Investigation on the Heat Transfer of <i>n</i>-Decane in a Horizontal Channel with Axially Nonuniform Heat Flux under Supercritical Pressure by Jin Zhang, Qilin Zhou, Xudong Zhao, Yuguang Jiang, Wei Fan

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Influence of helix angle on heat transfer characteristics of regenerative cooling in spiral channel by Xinlin Liu, Zhuohang Jiang, Qinglian Li, Jie Song, Peng Cheng

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Thermal Behaviour of the Cooling Jacket Belonging to a Liquid Oxygen/Liquid Methane Rocket Engine Demonstrator in the Operation Box by Daniele Ricci, Francesco Battista, Manrico Fragiacomo, Ainslie Duncan French

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Numerical Investigation on the Thermal Behaviour of a LOx/LCH₄ Demonstrator Cooling System by Daniele Ricci, Francesco Battista, Manrico Fragiacomo

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