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● 涡轮复杂冷却结构的设计优化
• He Q, Zhao, W, Chi Z*, Zang S. Application of Deep-Learning Method in the Conjugate Heat Transfer Optimization of Full-Coverage Film Cooling on Turbine Vanes[J]. International Journal of Heat and Mass Transfer, 2022, 195:123148.
• 章锁诚,夏硕成,迟重然*,臧述升. 双层壁叶片的模型化方法与冷却设计流程研究[J].热能动力工程 2021, 36(10):8.
• Chi Z*, Liu H, Zang S. Multi-objective optimization of the impingement-film cooling structure of a gas turbine endwall using conjugate heat transfer simulations[J]. Journal of Thermal Science and Engineering Applications, 2018, 10(2).
• Chi Z*, Liu H, Zang S. Geometrical optimization of nonuniform impingement cooling structure with variable-diameter jet holes[J]. International Journal of Heat and Mass Transfer, 2017, 108: 549-560.
• Chi Z*, Liu H, Zang S. Semi-Inverse Design Optimization Method for Film-Cooling Arrangement of High-Pressure Turbine Vanes[J]. Journal of Propulsion and Power, 2016, 32(3): 659-673.
• 迟重然*,任 静,蒋洪德,臧述升. 涡轮导叶气膜冷却结构半反设计优化方法[J].工程热物理学报, 2016,37(1):62-66.
• Chi Z, Ren J*, Jiang H. Coupled aerothermodynamics optimization for the cooling system of a turbine vane[J]. Journal of Turbomachinery, 2014, 136(5).
• Chi Z, Li X, Han C, et al. Optimization of the hole exit shaping of film holes without and with compound angles for maximal film cooling effectiveness[C]. ASME Turbo Expo 2014, GT2014-25212.
• Chi Z, Ren J*, Jiang H. Cooling Structure Optimization for a Rib-Roughed Channel in a Turbine Rotor Blade[C]. ASME Turbo Expo 2013, GT2013-94527.
• Chi Z, Wang S, Ren J*, Jiang H. Multi-dimensional platform for cooling design of air-cooled turbine blades[C]. ASME Turbo Expo 2012, GT2012-68675.
• 迟重然,温风波,王松涛*,冯国泰. 涡轮动叶冷却结构设计方法 Ⅲ:气热耦合计算[J].工程热物理学报, 2011,32(9):1485-1488.
• 迟重然,温风波,王松涛*,冯国泰. 涡轮动叶冷却结构设计方法 Ⅱ:管网计算[J].工程热物理学报, 2011,32(6):933-936.
• 王松涛*,迟重然,温风波,冯国泰. 涡轮动叶冷却结构设计方法 Ⅰ:参数化设计[J].工程热物理学报, 2011,32(4):581-584.
● 先进冷却技术与模化相似理论
• 刘亚非, 陶皓杰,迟重然*,. 蜂窝内冷通道布局对叶片冷效的影响研究[J].热能动力工程,2022. (accepted)
• Zhao W, Chi Z*, Zang S. Numerical and Experimental Study of Scaling Criteria Accuracy for Film Cooling Using CO2 Coolant[J]. International Journal of Heat and Mass Transfer, 2021, 181: 121984.
• Zhao W, Chi Z*, Zang S. Scaling criteria accuracy for turbine blade film cooling effectiveness at unmatched temperature ratio conditions[J]. Applied Thermal Engineering, 2021, 197: 117363.
• 陶皓杰,迟重然*,臧述升.涡轮动叶吸力侧单排气膜孔冷却性能研究[J].工程热物理学报,2021,42(03):595-600.
• Zhao W, Chi Z*, Zang S. Investigation of Similarity Criteria for an Internally-Cooled Turbine Vane Based on Artificial Neural Networks – PARTⅠ: Comparison of Scaling Criteria[C]. ASME Turbo Expo 2020, GT2020-14617.
• Zhao W, Wei J, Chi Z*, et al. Investigation of Similarity Criteria for an Internally-Cooled Turbine Vane Based on Artificial Neural Networks – PARTⅡ: Experimental Validation[C]. ASME Turbo Expo 2020, GT2020-16167.
• 韦景颖,迟重然*,臧述升.涡轮静叶叶型对绝热气膜冷却效率的影响[J].动力工程学报,2020,40(10):793-800.
• Chi Z*, Liu H, Zang S. Parametric Cooling Study of Single-Row Cylindrical Film Holes on Pressure Side of a Rotor Blade[C]. ASME Turbo Expo 2017, GT2017-65208.
• Chi Z*, Ren J, Jiang H, et al. Geometrical optimization and experimental validation of a tripod film cooling hole with asymmetric side holes[J]. Journal of Heat Transfer, 2016, 138(6).
• 迟重然,任 静*,蒋洪德. 燃机叶片平行肋扰流内冷通道传热特性研究Ⅱ:耦合传热特性[J].工程热物理学报, 2014,35(1):42-45.
• 迟重然,任 静*,蒋洪德. 燃机叶片平行肋扰流内冷通道传热特性研究Ⅰ:流动传热机理[J].工程热物理学报, 2013,34(4):624-627.
• Chi Z, Kan R, Ren J*, et al. Experimental and numerical study of the anti-crossflows impingement cooling structure[J]. International Journal of Heat and Mass Transfer, 2013, 64: 567-580.
● 燃机气热故障精准诊断理论
• Xia S, Chi Z*, Zang S. Comparative Study of Two Data-Driven Gas Path Fault Quantification Methods for a Single-Shaft Gas Turbine. ASME Turbo Expo 2022, GT2022-82406.
• 何庆富,迟重然*,臧述升.退化涡轮叶片形变与气动参数偏离的影响研究[J].热能动力工程,2021, 36(9):7.
• He Q, Chi Z*, Zang S. An Efficient Prediction Method for the Azimuthal Migration of Combustion Inhomogeneity in Multi-Stage Cooled Turbines[C]. ASME Turbo Expo 2021, GT2021-60220.
• 程新毓,迟重然*,臧述升.时间倾斜算法模拟涡轮热斑输运的精确性验证[J].热能动力工程,2021,36(01):38-48.
• Xia S, Chi Z*, Zang S. Improving Gas Turbine Performance through Reassembling Degraded Components: An Experimental and Computational Study[C]. ASME Turbo Expo 2020, GT2020-14627.
• 夏硕成,王辉,迟重然*,臧述升.部件性能衰减影响燃机性能的试验与仿真研究[J].工程热物理学报,2020,41(08):1877-1882.
• Chi Z*, Liu H, Zang S, et al. Full-Annulus URANS Study on the Transportation of Combustion Inhomogeneity in a Four-Stage Cooled Turbine[J]. Journal of Turbomachinery, 2019, 141(11): 111003.
• Chi Z*, Liu H, Zang S, et al. Full-Annulus URANS Study of Inlet Hot-Streak Transportation in a Four-Stage Gas Turbine[C]. ASME Turbo Expo 2018, GT2018-75596.
• 陈小岭,迟重然*,马超,臧述升.高载荷低压涡轮叶片尾缘劈缝的叶栅损失影响[J].工程热物理学报,2016,37(08):1635-1640.
● 新型动力循环与特种叶轮机
• Liu H, Chi Z*, Zang S. Transient behaviour and optimal start-up procedure of closed Brayton cycle with high thermal inertia[J]. Applied Thermal Engineering, 2021, 199: 117587.
• Liu H, Chi Z*, Zang S. Optimization of a closed Brayton cycle for space power systems[J]. Applied Thermal Engineering, 2020, 179: 115611.
• Liu H, Chi Z*, Zang S. Influence of Relative Velocity Ratio on Centrifugal Impellers Operating With Supercritical CO2[C]. ASME Turbo Expo 2018, GT2018-75590.
• Liu H, Chi Z*, Zang S. Influence of Root Fillet on the Structural and Aerodynamic Performance of a Centrifugal Impeller[C]. IGTC2015, No. 51.
学术兼职
国际期刊审稿人：ASME Journal of Heat Transfer, International Journal of Heat and Mass Transfer, Applied Thermal Engineering, Chinese Journal of Aeronautics, International Journal of Turbo&Jet Engines, International Journal of Energy Research 等
国际会议审稿人：ASME IGTI Turbo Expo, Global Power and Propulsion Forum 等
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