课题组研究目标
Our Researches, Your Innovations


R-R透平

一. 主要研究领域和方向
1. 透平机械气热性能不确定性量化和敏感性分析与鲁棒性优化
（1）透平机械气热性能的不确定性量化和敏感性分析。

（2）透平机械气热性能和寿命评估以及鲁棒性优化设计。

（3）透平机械高保真定常与非定常气热性能研究。

 

2. 燃气轮机和航空发动机热端部件气热性能和冷却结构布局

（1）涡轮级轮缘密封燃气入侵和封严效率与轮缘密封结构设计研究。

（2）涡轮叶顶流动传热和高效冷却布局设计研究。

（3）涡轮端壁气热性能和流热耦合机理与非轴对称端壁设计研究。

3. 热力透平密封技术
（1）透平旋转动密封泄漏流动和高效封严结构设计研究。

（2）透平机械旋转密封鼓风热效应和流热耦合研究。

（3）透平机械旋转动密封非定常气流激振和转子动力特性及增稳抑振结构设计研究。

（4）透平机械旋转动密封磨损状态下流热固耦合和运行性能与寿命评估。

（5）透平机械接触式刷式密封泄漏/摩擦热效应/力学行为研究。

 

4. 超临界二氧化碳透平热功转换和设计理论

（1）超临界二氧化碳透平设计方法和优化。

（2）超临界二氧化碳透平密封系统设计和干气封严性能研究。
 

二. 学术专著

[1] 李军，晏鑫，李志刚. 热力透平密封技术[M]. 西安交通大学出版社，“十二五”国家重点出版规划，2015.

[2] 李军，邵卫东. 格子Boltzmann方法与计算气动声学[M]. 科学出版社，2021.

三. 国家发明专利：
[1] 邓清华，丰镇平，李军，带有隔热与冷却作用的高温燃气密封结构，专利号：ZL 2004 1 007377.3

[2] 李志刚，李军，一种具有止旋抑振作用的防旋板结构，专利号：ZL 2015 1 0292681.8

[3] 李军，高庆，李志刚，一种具有阻尼孔和导流叶片的径向轮缘密封结构，专利号：ZL 2015 1 0600896.1

[4] 李志刚，李军，一种具有自止旋收敛型旋转密封结构，专利号：ZL 2017 1 0132590.7

[5] 晏鑫，代欣波，张康，李军，一种可调间隙的密封泄漏特性实验台，专利号： ZL 2017 1 0375614.1

[6] 李军，张元桥，李志刚，一种前挡板带喷嘴的耐高压低迟滞刷式密封结构，专利号 ZL2018 1 0509513.3

[7] 李军，陈尧兴，李志刚, 一种具有内凹型迷宫齿的迷宫密封结构, 专利号 ZL 2018 1 0481310.8

[8] 李军，杜昆，李志刚，一种具有提高端壁冷却效率的异形槽缝冷却结构，专利号：ZL201810373908.5

[9] 李军，杜昆，李志刚，一种具有提高静叶通道端壁冷却效率的槽缝冷却结构，专利号：ZL201810321060.1

[10] 李军，程舒娴，李志刚，燃气透平动叶前缘下端壁的局部球凹非轴对称端壁造型结构，专利号：ZL201810321049.5

[11] 李军，程舒娴，李志刚，宋立明，一种具有内齿槽的径向轮缘密封结构，专利号：ZL201811456646.5

[12] 李军，张元桥，李志刚，一种带刷式密封条的迷宫密封结构，专利号：ZL201810508427.0

 

四. 软件著作权：

[1] 李军，宋立明，丰镇平，汽轮机通流部分准三维气动优化设计软件，2011SR075704,2011年10月21日

[2] 宋立明，李军，丰镇平，汽轮机通流部分准三维热力分析及设计软件，2011SR057444,20111年8月15日

[3] 宋立明，李军，丰镇平，能量回收透平一维热力分析及设计软件，2013SR077362,2013年7月30日

[4] 李军，王天昊，李志刚，宋立明，透平机械迷宫密封泄漏特性分析软件，2019SR0580750, 2019年6月6日

[5] 李军，王天昊，李志刚，宋立明，透平机械迷宫密封转子动力特性分析软件，2019SR0772312,2019年7月25日

[6] 李军，王天昊，李志刚，宋立明，S-CO2迷宫密封性能预测分析软件，2020SR1662469， 2020年9月6日

[7] 李军，黄明，李志刚，宋立明，涡轮动叶叶顶气热性能不确定分析软件，2021SR034882,2021年3月5日

五. 学术论文

 

2024年

英文期刊论文

[1] Tao Yuan, Rui Yang, Zhigang Li, Jun Li*. et al. Thermal characteristics and cooling effect for SCO2 dry gas seal with multiple dynamic groove types[J]. Applied Thermal Engineering, 2024, 236: 121896.

[2] Ming Huang, Kaiyuan Zhang, Zhigang Li, Jun Li*. Effect of multi-cavity on the aerothermal performance robustness of the squealer tip under geometric and operational uncertainties[J]. Energy, 2024, 287: 129691.

[3] Ming Huang, Kaiyuan Zhang, Zhigang Li, Jun Li*. Innovative Framework for Robustness Analysis of Blade Multicavity Squealer Tip Aerothermal Performance[J]. AIAA Journal of Thermophysics and Heat Transfewr, 2024, 38(1): 5-19.

[4] Qineng Wang, Liming Song, Zhendong Guo, Jun Li, Zhenping Feng, A Novel Multi-Fidelity Surrogate for Efficient Turbine Design Optimization[J]. ASME Journal of Turbomachinery, 2024, 146(4): 041011.

[5] Xuebin Liu, Fei Zeng, Zhi Tao, Liming Song, Jun Li. Effect of film hole diameter and attack angle on the film cooling performance of leading edge with double swirl chamber under crossflow condition[J]. Applied Thermal Engineering, 2024, 242: 122539.

[6] Kaiyuan Zhang, Zhiyu Li, Weidong Shao, Zhigang Li, Jun Li*. Film cooling effect of upstream jump coolant on turbine endwall with combustor-turbine interface misalignment[J]. International Journal of Thermal Sciences, 2024, 201: 109055.

[7] Zuohong Zhou, Kaiyuan Zhang, Ming Huang, Zhigang Li, Jun Li*. Numerical investigations on film cooling effectiveness and heat transfer performance of inclined film hole on the turbine blade squealer tip with plasma actuation[J]. Aerospace Science and Technology, 2024, 151: 109283.

[8] Tianui Sun, Bo Bai, Zhigang LI， Jun Li*.Sensitivity analysis of turine stage aerothermal characteristics and blade cooling performance considering combustor swirl and hot spot[J]. Applied Thermal Engineering, 2024, 254: 123892.

[9] Wensong Xue, Zhi Fang, Tianhao Wang, Zhigang Li, Jun Li*. Rotordynamic characteristics of a novel labyrinth seal with partition and helical groove teeth[J]. Proc. IMechE Part A: Journal of Power and Energy, 2024, 238(3): 515-529.

[10] Kaiyuan Zhang, Zhiyu Li, Ming Huang, Zhigang Li, Jun Li*. Uncertainty quantification of turbine ewndwall aeorthermal performance under combustor-turbine interface louver coolant and cavity[J]. Applied Thermal Engineering, 2024, 253: 123800

 

中文期刊论文

[1] 薛文松，王天昊，李志刚，李军*. 基于试验设计方法的液相孔型-迷宫密封几何参数敏感性分析[J]. 西安交通大学学报, 2024, 58(3): 58-68.

[2] 赵欣悦，雷隆，李志刚，李军*. 燃气透平轮缘密封流动特性和气动性能[J]. 西安交通大学学报，2024, 58(5): 111-123.

[3] 张垲垣，栗智宇，李志刚，李军*. 燃烧室百叶与双排孔冷气对透平端壁冷却性能影响研究[J]. 西安交通大学学报， 2024, 58(6): 65-76.

[4] 周祚弘，黄明，晏鑫，李志刚，李军*. 环形电极等离子激励控制透平叶顶间隙泄漏流动研究[J]. 西安交通大学学报，2024, 58(6): 128-138.

 

国际会议论文

[1] Tianyi Sun, Zhiyu Li, Zhigang Li, Jun Li*. et al. Effects of Combustor Residual Swirl and Hot Spot on Aerothermal Characteristics and Cooling Performance of Gas Turbien Blade[C]. GT2024-124545.

[2] Zhiyu Li, Kaiyaun Zhang, Zhigang Li, Jun Li*. Aerothermal Performance of Slashface Leakage with Double Surface Angle Under Realistic Swirling Inflow[C]. GT2024-124933.

[3] Run Cao, Rui Yang, Qinghua Deng, Jun Li* et al., Numerical Investigations on the Aerodynamic Performance of Supercritical Carbon Dioxide Centrifugal Compressor[C], GT2024-125624.

[4] Tianhao Wang, Zhigang Li, Jun Li*. A Wide-Bandwidth and High-Resolution Identification Method for the Dynamic Characteristics of Annular Gas Seals Uing Hilbert Transform[C]. GT2024-126191.

[5] Xinnan Chen, Bo Bai, Zhigang Li, Jun Li*. Effect of Film Hole Configuration on the Impingement Film Composite Cooling Performance of a Simulated Turbine Blade Leading Edge[C]. GT2024-126204.

[6] Yuxuan Dong, Rui Yang, Xidong Wang, Zhigang Li, Jun Li*. Liming Song. Multi-Objective Aerodynamic Optimization of Gas Turbine Exhaust Diffuser: Experimental and Numerical Validations[C]. GT2024-127354.

 

 

2023年

英文期刊论文

[1] Ming Huang, Zhigang Li, Jun Li*. Robustness Analysis on Aerothermal Performance of the Winglet Squealer Tip - Part 1: Aerodynamic Performance[J]. ASME Journal of Turbomachinery, 2023, 145(1): 011013.

[2] Ming Huang, Zhigang Li, Jun Li*. Robustness Analysis on Aerothermal Performance of the Winglet Squealer Tip - Part 2: Heat Transfer Performance[J]. ASME Journal of Turbomachinery, 2023, 145(1): 011014.

[3] Jiajie Guo, Xinjun Wang, Zhi Tao, Liming Song, Jun Li. Effects of the inclined angle of novel film holes on the aero-thermal performance of a squealer tip[J]. Applied Thermal Engineering, 2023, 219: 119623.

[4] Kaiyuan Zhang, Zhiyu Li, Jun Wu, Zhigang Li, Jun Li*. Turbine nozzle endwall aero-thermal characteristics under combustor louver coolant with interface cavity[J]. Applied Thermal Engineering, 2023, 219: 119683.

[5] Shijie Jiang, Zhigang Li, Jun Li*, Liming Song, Numerical investigations on the unsteady leakage flow and heat transfer characteristics of the turbine blade squealer tip[J]. Journal of the Global Power and Propulsion Society, 2023, 7:1-12.

[6] Kaiyuan Zhang, Zhiyu Li, Zhigang Li, Jun Li*. Gas turbine ednwall film cooling and heat transfer characteristics with a multi-cavity slashface gap design[J]. Aerospace Science and Technology, 2023, 132: 108076.

[7] Tao Yuan, Zhigang Li, Jun Li, Qi Yuan. Static and Rotordynamic Characteristics for Supercritical Carbon Dioxide Spiral Groove Dry Gas Seal with the Titled Seal Ring[J]. ASME Journal of Engineering for Gas Turbines and Power, 2023, 145(1): 011011.

[8] Zhihong Jin, Kai Mao, Zhigang Li, Jun Li. A Comparison of Static and Rotordynamic Characteristics for Three Types of Impeller Front Seals in a Liquid Oxygen Turbopump[J]. ASME Journal of Engineering for Gas Turbines and Power, 2023, 145(3): 031025.

[9] QIngfeng Cong, Kaiyuan Zhang, Zhigang Li, Jun Li. Numerical Investigations on Gas Ingestions Mechanism Based on Flow Instabilities in Rim Seal and Cooling Characteristics of Endwall in a 1.5-Stage Axial Turbine[J]. ASME Journal of Engineering for Gas Turbines and Power, 2023, 145(5): 051001.

[10] Bo Bai, Zhigang Li, Kaiyuan Zhang, Jun Li, Shuo Mao, Wing F. Ng. Effects of Hole Blockage on Endwall Film Cooling and Vane Phantom Cooling Performance of a Transonic Turbine Vane[J]. ASME Journal of Engineering for Gas Turbines and Power, 2023, 145(4): 041001.

[11] Shijie Jiang, Zhigang Li, Jun Li*. Effect of unsteady passing wake on the aerodynamic and heat transfer performance of the turbine blade squealer tip[J]. Proc. IMechE Part A: J. Power and Energy, 2023, 237(1): 19-32.

[12] Run Cao, Qinghua Deng, Zhigang Li, Jun Li, Tieyu Gao. Design strategy for inlet conditions of supercritical CO2 centrifugal Compressor[J]. The Journal of Supercritical Fluids, 2023, 196: 105879.

[13] Zhi Fang, Zhigang Li, Jun Li. Numerical Investigation on the Leakage and Rotordyanmic Characteristics for a Hole-Pattern Seal in Wet-Gas Conditions[J]. ASME Journal of Engineering for Gas Turbines and Power, 2023, 145(6): 061003.

[14] Yuxuan Dong, Zhigang Li, Jun Li*. Investigations on the Splitter structure to Improve the Aerodynamic Performance of Gas Turbine Exhaust Diffuser at Different Swirl Angles[J]. ASME Journal of Engineering for Gas Turbines and Power, 2023, 145(6): 061015.

[15] Shuo Mao, Daniel Van Hout, Kaiyuan Zhang, Jin Woo Lee, Wig F. Ng, Hongzhou Xu, Michael Fox, Jun Li. Upstream Jet Coolng and Dual Cavity Slashface Leakage Cooling on a Transonic Nozzle Guide Vane Endwall[J]. ASME Journal of Turbomachinery, 2023, 145(8): 081006.

[16] Xinnan Chen, Zhigang Li, Jun Li*. Effect of Microchannel on the Composite Cooling Performance of a Simulated Turbine Blade Leading Edge[J]. ASME Journal of Heat and Mass Transfer, 2023, 145(10): 101001.

[17] Ming Huang, Kaiyuan Zhang, Zhigang Li, Jun Li*. Comprehensive Aerothermal Investigation of Turbine Blade Multicavity Squealer Tip Using a Novel Methodology With Uncertainty Quantification[J]. ASME Journal of Thermal Science and Engineering Applications, 2023, 15(10): 101010.

[18] Zhiyu Li, Kaiyuan Zhang, Zhigang Li, Jun Li*. Effects of proactive phantom cooling on turbine endwall aerodynamic and film cooling performance considering aggresive swirling inflow[J]. Applied Thermal Engineering, 2023, 235: 121333.

 

中文期刊论文

[1] 孙添一，张垲垣，李志刚，李军*. 燃烧室出流条件对涡轮静叶端壁流动结构和传热冷却特性的影响[J]. 西安交通大学学报，2023, 57(1): 152-163.

[2] 胡乐豪，邓清华，刘洲洋，李军，丰镇平. 超临界二氧化碳密封内摩擦损失数值研究及流动特性分析[J]. 西安交通大学学报, 2023, 57(3): 68-78.

[3] 白波，董雨轩，李志刚，李军. 一种燃气涡轮叶片气热性能实验台[J]. 工程热物理学报，2023, 44(4): 987-993.

[4] 陈欣楠，李志刚，李军*，徐庆宗，杜强. 二次冲击对静叶前缘冷却性能影响的对比研究[J]. 西安交通大学学报, 2023, 57(5): 34-45.

[5] 许承天，白波，李志刚，李军*. 涡轮动叶倾斜肩壁凹槽状叶顶气动性能研究[J]. 西安交通大学学报，2023, 57(5): 46-57.

 

国际会议论文

[1] Guoying Yang, Rui Yang, Qinghua Deng, Bozhou Xu, Jun Li, Zhenping Feng. Numerical Investigations of Flow Characteristics in a Supercritical Carbon Dioxide Turbine for 20 Megawatt Brayton Cycle[C]. GT2023-101767.

[2] Zhoubin Zhao, Qinghua Deng, Lehao Hu, Jun Li. Zhenping Feng. Windage Loss and Flow Characteristics in Back Gap of Radial Inflow Impellers with Steam Medium[C].GT2023-102360.

[3] Pengfei Song, Dengqian Ma, Zhigang Li, Jun Li*. Numerical and Experimental Investigations on the Leakage Flow Characteristics and Temperature Distributions of Brush Seal[C]. GT2023-102763.

[4] Qing Cong, Long Lei, Kaiyuan Zhang, Zhigang Li, Jun Li*.  Effects of Inflow Swirl on the Sealing Effectiveness of Turbine Rim Seal[C]. GT2023-102768.

[5] Zhuocong Li, Zhignag Li, Jun Li. A Full Three-Dimensional Transient Flyid-Structure Interaction Model for the Dynamic Characteristics Predictions of Bump-type Gas Foil Journal Bearings[C]. GT2023-102802.

[6] Yulin Wang, Can Guo, XInnan Chen, Tiayi Sun, DaweiChen, Zhigang LI, Jun Li. A Novel Prediction Model for the Aerodynamic Losses Increase Due to Film Cooling Injections from Gas Turbine Vane Surface[C]. GT2023-102906.

[7] Qineng Wang, LimingSong, Zhendong Guo, Jun Li. Zhenping Feng. A Novel Multi-Fidelity Surrogate for Turbomachinery Design Optimization[C]. GT2023-104237.

 

 

 

 

 

2022年

英文期刊论文

[1] Zhigang Li, Bo Bai, Jun Li*, Shuo Mao, Wing F. Ng, Hongzhou Xu, Michael Fox. Endwall Heat Transfer and Cooling Performance of a Transonic Turbine Vane with Upstream Injection Flow[J]. ASME Journal of Turbomachinery, 2022, 144(4): 041004.

[2] Bo Bai, ZHigang LI, Jun Li, Shuo Mao, Wing F. Ng. The Effects of Axisymmetric Convergence Contouring and Blowing Ratio on Endwall Film Cooling and vane Pressure Side Surface Phantom Cooling Performance[J]. ASME Jouranl of Engineering for Gas Turbines and Power, 2022, 144(2): 021020.

[3] Tianhao Wang, Zhigang LI, Jun LI*. Rotordynamic Characteristics of the Straight-Through Labyrinth Seal Based on the Applicability Analysis of Leakage Models Using Bulk-Flow Method[J]. ASME Journal of Engineering for Gas Turbines and Power. 2022, 144(1): 011028.

[4] Yuxuan Dong, Zhigang Li, Jun Li*. AN INvestigation of the Tapered Strut on the Aerodynamic Performance of the Exhaust Diffuser Under DIfferent Swirls[J]. ASME Journal of Engineering for Gas Turbines and Power, 2022, 144(1): 011006.

[5] Hongyan Bu, Yufeng Yang, Liming Song, Jun Li. Improving the Film Cooling Performance of a Turbine Endwall With Multi-Fidelity Modeling Considering Conjugate Heat Transfer[J]. ASME Journal of Turbomachinery, 2022, 144(1): 011011.

[6] Kaiyuan Zhang, Zhigang LI, Jun Li*. Non-Axisymmetric endwall contouring optimization and performance assessment as affected by simulated purge flow and backward hole injection[J]. International Journal of Thermal Sciences, 2022, 172-107297.

[7] Shijie Jiang, Zhigang Li, Jun Li*. Effects of the casing step size on the tip leakage flow pattern and heat transfer characteristics of turbine blade squealer tip[J]. International Journal of Thermal Sciences, 2022, 174: 107442.

[8] Ming Huang, Zhigang Li, Jun Li*, Liming Song. Uncertainty quantification and sensitivity analysis of aerothermal performance for the turbine blade squealer tip[J]. International Journal of Thermal Sciences, 2022, 175: 107460.

[9] Shijie Jiang, Zhigang Li, Jun Li*. Effect of casing purge flow on heat transfer and cooling performance of blade squealer tip for a gas turbine stage[J]. Proc. IMechE Part A: Journal of Power and Energy, 2022, 236(2): 224-240.

[10] Wensong Xue, ZHi Fang, Zhigang Li, Jun Li. Rotordynamic Characteristics of a Noval Labyrinth Seal with Swirl Brakes at Seal Entrance and Cavity[J]. ASME Journal of Engineering for Gas Turbines and Power, 2022, 144(5): 051017-1-12.

[11] Ming Huang, Zhigang Li, Jun Li*. Investigations on the aerothermal performance of the turbine blade winglet squealer tip within uncertainty framework[J]. Aerospace Science and Technology, 2022, 123:107506-1-19.

[12] Ming Huang, Zhigang Li, Jun Li*, Liming SOng. Efficient Uncertainty Quantification and Sensitivity Analysis on the Aerothermal Performace of Turbine Blade Squealer Tip[J]. ASME Journal of Turbomachinery, 2022, 144(5): 051014-1-16.

[13] Boyang Xia, Jun Li*. An Efficient impelemntation of nodal discontinuous Galerkin lattice Boltzmann method and validation for direct numerical simulation of turbulent flows[J]. Computers and Mathematics with Applications, 2022, 117:284-298.

[14] Zhigang Li, Zhuocong Li, Jun Li*, Zhenping Feng. Static and Rotordynamic Characteristucs for Two Types of Novel Hole-Pattern Seals Operating in Supercritical CO2 Turbomachinery[J]. ASME Journal of Engineering for Gas Turbines and Power, 2022, 144(7): 071006-1-14.

[15] Ming Huang, Zhigang Li, Jun Li*. Robustness Analysis on the Aerothermal Performance of Turbine Blade Squealer Tip[J]. ASME Journal of Engineering for Gas Turbines and Power, 2022, 144(7): 071011-1-16.

[16] Shijie Jiang, Zhigang Li, Jun Li*. Effects of Rib Design on the Unsteady Tip Heat Transfer Amplitude for a Turbine Rotor Blade[J]. ASME Journal of Thermal Science and Engineering Applications, 2022, 14(10): 101011-1-15.

[17] Jie Wang, Chao Zhang, Xuebin Liu, Liming Song, Jun Li. Experimental and numerical investigation on the film cooling performance of cylindrical hole and fan-shaped hole with vortex generator fed by corssflow[J]. International Journal of Heat and Mass Transfer, 2022, 187:122560.

 

 

 

中文论文

[1] 孙添一，李志刚，李军*. 发散冷却和前缘槽缝射流作用下涡轮静叶端壁流动结构的研究[J]. 西安交通大学学报, 2022, 56(1): 120-128.

[2] 黄明，李志刚，李军*，宋立明. 涡轮动叶凹槽状叶顶传热特性和气动性能的不确定性量化研究[J].推进技术，2022, 43(3): 224-236.

[3] 薛文松，方志，王天昊，李志刚，李军. 防旋板结构的迷宫密封转子动力特性研究[J]. 西安交通大学学报，2022, 56(3): 105-116.

[4] 陈欣楠，李志刚，李军*. 冲击孔偏置对静叶前缘和吸力面冷却性能的影响[J]. 西安交通大学学报, 2022, 56(4): 50-60.

[5] 曹润，李志刚，李军*，邓清华，高铁瑜. 具有密封结构的超临界二氧化碳离心压缩机特性研究[J]. 西安交通大学学报，2022, 56(4): 127-137.

[6] 栗智宇，张垲垣，李志刚，李军*. 燃烧室出口旋流对静叶栅端壁流动型态和传热冷却特性的影响[J]. 西安交通大学学报，2022, 56(4): 72-82.

[7] 邓清华，胡乐豪，赵奕萌，杨国英，李军，丰镇平. 轴类间隙内摩擦损失模型验证及流动特性分析[J]. 西安交通大学学报, 2022, 56(5): 54-63.

[8] 许承天，李志刚，李军*. 考虑气膜冷却脉动特性的涡轮动叶凹槽状叶顶气动和冷却性能研究[J]. 西安交通大学学报, 2022, 56(5): 127-140.

[9] 董雨轩，李志刚，李军*. 支撑板构型提升燃气轮机排气扩压器气动性能研究[J]. 西安交通大学学报, 2022, 56(5): 209-222.

[10] 丛庆丰，李志刚，程舒娴，李军*. 涡轮径向轮缘密封非定常燃气入侵和封严效率的数值研究[J]. 推进技术，2022, 43(6): 83-93. 

 

 

 

2021年

[1] Yaoxing CHEN, Zhigang LI, Jun LI*, Xin YAN. Effects of swirl brake axial arrangement on the leakage performance and rotor stability of labyrinth seals[J]. Chinese Journal of Aeronautics, 2021, 34(1): 22-31.

[2] Zhi tao, Boyang Yu, Yixing Li, Liming Song, Jun Li. Effects of non-axisymmetric endwall countouring on aerothermal performance of a gas turbine blade endwall with a purge flow[J]. International Journal of Thermal Science, 2021, 164: 106921.

[3] Zhi Tao, Fengchao Li, Boyang Yu, Penyuan Zhu, Liming Song, Jun Li. Effects of the positive pre-swirl purge flow on endwall aero-thermal performance of a gas turbine blade[J]. International Journal of Thermal Science, 2021, 165: 106565.

[4] Zhigang Li, Zhi Fang, Jun Li*, Zhenping Feng. Static and Rotordynamic Characteristics for Two Types of Novel Mixed Liquid Damper Seals With Hole-Pattern/Pocket-Textured Stator and Helically Grooved Rotor[J]. ASME Journal of Engineering for Gas Turbines and Power, 2021, 143(4): 041019-1-16.

[5] Yuanqiao Zhang, Jun Li*, Dengqian Ma, Yuan He, Jingjin Ji, Bo Sun, Zhigang Li, Xin Yan. Experimental and Numerical Investigations on the Leakage Flow Characteristics of Helical-Labyrinth-Brush Seals[J]. ASME Journal of Engineering for Gas Turbines and Power, 2021, 143(4): 041023-1-13.

[6] Xinbo Dai, Xin Yan, Kun He, Jun Li, Zhenping Feng. Numerical Investigations of Leakage Performance Degradations in Labyrinth and Flexible Seals Due to Wear[J]. ASME Journal of Engineering for Gas Turbines and Power, 2021, 143(5): 051003-1-15.

[7] Dengqian Ma, Zhigang Li, Jun Li*. A Three-Dimensional Tube Bundle Model Analysis for Leakage Flow Characteristics of Variables Bristle Diameter Brush Seals With Bristle Pack Stratification[J]. ASME Journal of Engineering for Gas Turbines and Power, 2021, 143(5): 051014-1-16.

[8] Dengqian Ma, Yuanqiao Zhang, Zhigang Li, Jun Li*, Xin Yan. Numerical Investigations on the Leakage Flow Characteristics of Brush Seal based on the Three-Dimensional Staggered Tube Bundle Model[J]. ASME Journal of Engineering for Gas Turbines and Power, 2021, 143: 051023-1-11.

[9] Hongyan Bu, Zhendong Guo, Liming Song, Jun Li. Effects of Cooling Configurations on the Aerothermal Performance of a Turbine Endwall With Jet Impingment and Film Cooling[J]. ASME Journal of Turbomachinery, 2021, 143(6): 061013-1-12.

[10] Kaiyuan Zhang, Zhigang Li, Jun Li*, Influence of slashface leakage coupled with quasi-labyrinth seal technique on gas turbine endwall aerothermal performance and blade suction side surface phantom cooling[J]. Proc. ImechE Part A: J Power and Energy, 2021, 235(3): 351-367.

[11] Zhi Tao, Zhendong Guo, Liming Song, Jun Li. Uncertainty Quantification of Aero-Thermal Performance of a Blade Endwall Considering Slot Geometry Deviation and Mainstream Fluctuation[J]. ASME Journal of Turbomachinery, 2021, 143(11): 111013.

[12] Zhigang Li, Zhuocong Li, Jun Li*, Zhenping Feng. Leakage and Rotordynamic Characteristics for Three Types of Annular Gas Seals Operating in Supercritical CO₂ Turbomachinery[J]. ASME Journal of Engineering for Gas Turbines and Power, 2021, 143(10): 101002

 

 

中文期刊论文

[1] 程舒娴，李军*，李志刚，宋立明. 轮缘密封整周模型流动与封严特性数值研究[J]. 工程热物理学报, 2021, 42(2): 370-376.

[2] 张垲垣，李志刚，李军*. 透平端壁冷却及泛冷却最优的端壁造型设计研究[J]. 西安交通大学学报, 2021, 55(5): 1-9.

[3] 王天昊，李志刚，李军*. 采用Bulk-Flow模型的直通式迷宫密封转子电流特性研究[J]. 西安交通大学学报. 2021, 55(5): 25-33.

[4] 董雨轩，李志刚，李军*. 支撑板型线和径向倾斜设计对燃气轮机排气扩压器气动性能的影响[J]. 推进技术. 2021, 42(6): 1245-1255.

[5] 李军*，栗智宇，李志刚，张垲垣，宋立明. 燃烧室和涡轮相互作用下高压涡轮级气热性能研究进展[J]. 航空学报, 2021, 42(3): 024111-1-26.

[6] 黄明，李军*，李志刚，宋立明. 动叶凹槽状叶顶气膜冷却有效度和气动性能不确定性量化研究[J]. 西安交通大学学报, 2021, 55(5): 181-192.

 

国际会议论文

[1] Qingfeng CONG, Zhigang LI, Jun Li*. Numerical Investigations on the Aerodynamic Performance and Endwall Cooling Characteristics of Turbine During Acceleration Process With Lagging Effects[C]. Proceedings of ASME Rurbo Expo 2021: Turbomachinery Technical Conference and Exposition, GT2021, June 7-11, 2021, Virtual, Online, GT2021-59142.

[2] Ming HUANG, Zhigang LI, Jun Li*, Liming Song. Investigations on the Aerothermal Performance Uncertainty Quantification of the Turbine Blade Squealer Tip[C]. Proceedings of ASME Rurbo Expo 2021: Turbomachinery Technical Conference and Exposition, GT2021, June 7-11, 2021, Virtual, Online, GT2021-59033.

[3] Zhiyu LI, Kaiyuan ZHANG, Zhigang LI, Jun LI*. Numerical Investigations on the Aerothermal Performance and Film Cooling Effectiveness of Turbine Vane Endwall at Inlet Swirl Conditions[C]. Proceedings of ASME Rurbo Expo 2021: Turbomachinery Technical Conference and Exposition, GT2021, June 7-11, 2021, Virtual, Online, GT2021-59062.

[4] Tianhao WANG, Zhigang LI Jun LI*. Rotordynamic Characteristics of the Straight-Through Labyrinth Seal Based on the Applicability Analysis of Leakage Models using Bulk-Flow Method[C]. Proceedings of ASME Rurbo Expo 2021: Turbomachinery Technical Conference and Exposition, GT2021, June 7-11, 2021, Virtual, Online, GT2021-59568.

[5] Wensong XUE, Yang CHEN, Zhigang LI, Jun LI*, Experimental Measurements and Numerical Investigations on the Aerodynamic Performance and Internal Flow Fields of Tangential Addmission Volutes for Steam Turbines[C]. Proceedings of ASME Rurbo Expo 2021: Turbomachinery Technical Conference and Exposition, GT2021, June 7-11, 2021, Virtual, Online, GT2021-59140.

[6] Tao YUAN, Zhigang LI, Jun LI*, Qi YUAN. Design and Analysis of Cooling Structure for Dry Gas Seal Chamber of Supercritical Carbon Dioxide Turbine Shaft End[C]. Proceedings of ASME Rurbo Expo 2021: Turbomachinery Technical Conference and Exposition, GT2021, June 7-11, 2021, Virtual, Online, GT2021-59177.

[7] Zhi Fang, Zhigang Li, Jun Li, Zhenping Feng. Static and Rotordynamic Characteristics for Two Novel Hole-Pattern Annular Liquid Seals With Circumferential-/Axially-Oblique Hole Cavities[C]. Proceedings of ASME Rurbo Expo 2021: Turbomachinery Technical Conference and Exposition, GT2021, June 7-11, 2021, Virtual, Online, GT2021-58996.

[8] Hongyan Bu, Yufeng Yang, Liming Song, Jun Li. Improving the Film Cooling Performance of a Turbine Endwall With Multi-Fidelity Modeling Considering Conjugation Heat Transfer[C]. Proceedings of ASME Rurbo Expo 2021: Turbomachinery Technical Conference and Exposition, GT2021, June 7-11, 2021, Virtual, Online, GT2021-59015.

[9] Jie Wang, Chao Zhang, Xuebin Liu, Liming Song, Jun Li, Zhenping Feng. Experimental Investigation and Optimal Design on the Film Cooling Performance of Fan-Shaped Hole With Vortex Generator Fed by Crossflow[C]. Proceedings of ASME Rurbo Expo 2021: Turbomachinery Technical Conference and Exposition, GT2021, June 7-11, 2021, Virtual, Online, GT2021-59144.

 

 

2020年

英文期刊论文

[1] Chao Zhang, Jie Wang, Xuebin Liu, Limig Song, Jun Li, Zhenping Feng, Experimental and Numerical Study on the Flat-Plate Film Cooling Enhancement Using the Vortex Generator Downstream for the Fan-Shaped Hole Configuration[J]. ASME Journal of Turbomachinery, 2020, 142(3): 031006.

[2] Zhou JF, Wang XJ, Li J, et al. Effects of Diameter Ratio and Inclination Angle on Flow and Heat Transfer Characteristics of Sister Holes Film Cooling[J]. International Communications in Heat and Mass Transfer. 2020, 110: 104426.

[3] Zhigang Li, Zhi Fang, Jun Li*, Zhenping Feng, Numerical Modeling of Static and Rotordynamic Characteristics for Three Types of Helically Grooved Liquid Annular Seals[J]. ASME Journal of Vibration and Acoustics, 2020, 142(4): 041001.

[4] Chuang Wu, Xiaoxiao Xu, Qibin Li, Jun Li, Shunsen Wang, Chao Liu, Proposal and assessment of a combined cooling and power system based on the regenerative supercritical carbon dioxide Brayton cycle integrated with an absorption refrigeration cycle for engine waste heat recovery[J]. Energy Conversion and Management, 2020, 207, 112527.

[5] Shijie Jiang, Zhigang Li, Jun Li*, Liming Song. Effects of the novel rib layouts on the tip leakage flow pattern and heat transfer performance of turbine blade[J]. Proc. IMechE Part G: Journal of Aerospace Engineering, 2020, 234(8): 1446-1459.

[6] Yaoxing CHEN, Zhigang LI, Jun LI*, Xin YAN. Effects of tooth bending damage on the leakage performance and rotordynamic coefficients of labyrinth seals[J]. Chinese Journal of Aeronautics. 2020, 33(4): 1206-1217.

[7] Yuanqiao ZHANG, Jun LI*, Zhigang LI, Xin YAN. Effect of bristle pack position on the rotordynamic characteristics of brush-labyrinth seals at various operating conditions[J]. Chinese Journal of Aeronautics., 2020, 33(4): 1192-1205.

[8] Zhigang Li, Zhi Fang, Jun Li*, Influence of Annular/Pocket Groove on the Static and Rotordynamic Characteristics of Hole-Pattern Seals[J]. ASME Journal of Engineering for Gas Turbines and Power, 2020, 142(6): 061013.

[9] Zhi Tao, Yunjia Yao, Penyuan Zhu, Liming SONG, Jun Li. Experimental and numerical study on film cooling effectiveness of an annular cascade endwall with different slot configuration[J]. International Journal of Thermal Sciences, 2020, 158: 106517.

[10] Dengqian Ma, Jun Li*, Yuanqiao Zhang, Zigang Li, Xin Yan, Liming Song. Application of blade tip shroud brush seal to improve the aerodynamic performance of turbine stage[J]. Proc. ImechE Part A: I Power and Energy, 2020, 234(6): 777-794.

[11] Chenxi Li, Jiacheng Xia, Liming SONG, Jun Li, An aerothermal analysis of the effects of tip gap height and cavity depth of a gas turbine blade[J]. International Journal of Thermal Science, 2020, 158: 106521.

[12] Yuanqiao Zhang, Jun Li*, Zhigang Li, Xin Yan. Numerical Comparison of Leakage Flow and Rotordynamics Characteristics for Two Types of Labyrinth Seals With Baffles[J]. ASME Journal of Engineering for Gas Turbines and Power, 2020, 142(9): 091008-1-17.

[13] Zhigang Li, Zi Fang, Jun Li*, A Comparison of Static and Rotordynaic Characteristics for Two Types of Liquid Annular Seals With Parallelly Grooved Stator/Rotor[J]. ASME Journal of Engineering for Gas Turbines and Power, 2020, 142(9): 091012-1-17.

 

中文期刊论文

[1] 薛文松，陈阳，李军*，白昆仑，田朝阳，汽轮机切向进气蜗壳气动性能研究[J].西安交通大学学报，2020, 54(1): 125-134.

[2] 方志，李志刚，李军，异形孔腔结构对液体孔型密封泄漏特性及转子耗功的影响[J],西安交通大学学报，2020, 54(1): 143-149.

[3] 董雨轩，李志刚，李军*，预旋对燃气涡轮排气蜗壳气动性能影响的数值研究[J].西安交通大学学报，2020, 54(1): 116-124.

[4] 刘璐园，张元桥，李军*，张家培，刘晓澜，杨锐，杨建道，刷式密封对透平级气动性能影响的研究[J]. 工程热物理学报，2020, 41(1): 122-127.

[5] 曹润，李志刚，邓清华，李军*，高铁瑜. 超临界二氧化碳离心压气机设计和气动性能研究[J]. 西安交通大学学报, 2020, 54(4): 44-52

[6] 姜世杰，李志刚，李军*. 肋条布局对涡轮动叶凹槽状叶顶传热和气动性能的影响研究[J]. 推进技术, 2020, 41(5): 1103-1111

[7] 白波，李志刚，李军. 上游台阶结构对跨声速透平叶栅端壁气膜冷却性能的影响[J]. 西安交通大学学报, 2020, 54(5): 1-8.

[8] 薛文松，李军*，陈阳等. 横向间距和截面形状对汽轮机切向进气蜗壳气动性能的影响[J]. 西安交通大学学报，2020, 54(7): 94-103.

[9] 夏博阳，邵卫东，李军*. 三维间断噶辽金玻尔兹曼方法的完全匹配吸收边界条件研究[J]. 西安交通大学学报, 2020, 54(7): 113-120

[10] 李志刚，方志，李军*. 液相和多相环境下环形动密封泄漏流动和转子动力特性的研究进展[J].西安交通大学学报，2020, 54(9): 1-22

[11] 马登骞，张元桥，李志刚，李军*，晏鑫. 采用三维叉排管束模型的刷式密封泄漏特性研究[J]. 西安交通大学学报, 2020, 54(9): 72-80.

[12] 方志，李志刚，李军. 孔型参数对流体孔型密封泄漏特性和转子耗功的影响[J]. 西安交通大学学报, 2020, 54(9): 81-88.

[13] 袁韬，李志刚，李军*，袁奇. 螺旋槽结构对SCO2压气机轴端干气密封性能影响的数值研究[J]. 西安交通大学学报, 2020, 54(11): 37-45.

[14] 张元桥，李军*，马登骞，何院，计京津，孙博，李志刚，晏鑫. 螺旋篦齿-刷式密封泄漏特性实验和数值研究[J]. 西安交通大学学报, 2020, 54(11): 1-9.

[15] 张元桥，刘璐园，马登骞，李军*，李志刚，晏鑫. 迷宫刷式密封泄漏特性的实验和数值研究[J]. 工程热物理学报, 2020, 41(10): 2411-2419

 

2019年

英文期刊论文

[1] Zhigang Li, Zhi Fang, Jun Li*, Numerical Investigations on the Leakage and Rotordynamics Characteristics for Three Types of Annular Gas Seals in Wet Gas Conditions[J]. ASME Journal of Engineering for Gas Turbines and Power, 2019, 141(3): 032504-1-16.

[2] Kun Du, Zhigang Li, Jun Li*, Bengt Sunden, Influence of a multi-cavity tip on the blade tip and the over casing aerothermal performance in a high pressure turbine cascade[J]. Applied Thermal Engineering, 2019, 147: 347-360.

[3] Kaiyuan Zhang, Jun Li*, Zhigang Li, Liming Song, Effects of simulated swirl purge flow and mid-passage gap leakage on turbine blade platform cooling and scution surface phantom cooling performance[J]. International Journal of Jeat and Mass Transfer, 2019, 129: 618-634.

[4] Kaiyuan Zhang, Zhigang Li, Jun Li*, Effect of gas turbine endwall misalignment with slashface leakage on the blade endwall aerothermal performance[J]. International Journal of Heat and Mass Transfer, 2019, 131: 1247-1259.

[5] Zhendong Guo, Hongyan Bu, liming Song, Jun Li, Zhenping Feng, Experiment test of a 3D parameterized vane cascade with non-axisymmetrica endwall[J]. Aerospace Science and Technology, 2019, 85: 429-442.

[6] Junfei Zhou, Xinjun Wang, Jun Li, Weitao Hou, Effects of Target Channel Shapes on Double Swirl Cooling Performance at Gas Turbine Blade Leading Edge[J]. ASME Journal of Engineering for Gas Turbines and Power, 2019, 141(7): 071004.

[7] Junfei Zhou, Xinjun Wang, Jun Li, Influence of effusion hole diameter on impingement/effusion cooling performance at turbine blade leading edge[J]. International Journal of Heat and Mass Transfer, 2019, 134: 1101-1118.

[8] Shuxian Cheng, Zhigang Li, Jun Li*, Investigations on the Sealing Effectiveness and Unsteady Flow Field of 1.5-Stage Turbine Rim Seals[J]. ASME Journal of Engineering for Gas Turbines and Power, 2019, 141(8): 081003.

[9] Qinghua Deng, Yu Jiang, Zhifeng Hu, Jun Li, Zhenping Feng, Condesnsation and expansion characteristics of water steam and carbon dioxide in a Laval Nozzle[J]. Energy, 2019, 175: 694-703.

[10] Shijie Jiang, Zhigang Li, Jun Li*, Effects of the squealer winglet structures on the heat transfer characteristics and aerodynamic performance of turbine blade tip[J]. International Journal of Heat and Mass Transfer, 2019, 139: 860-872.

[11] Chao Zhang, Jie Wang, Xin Luo, Liming Song, Jun Li, Zhenping Feng, Experimentally measured effect of height and location of the vortex generator on flow and heat transfer characteristics of the flat plate film cooling[J]. International Journal of Heat and Mass Transfer, 2019, 141: 995-1008.

[12] Weidong SHAO, Jun LI*, Review of Lattice Boltzmann Method Applied to Computational Aeroacoustics[J]. Archives of Acoustics, 2019, 44(2): 215-238.

[13] Junfei Zhou, Xinjun Wang, Jun Li*, Weitao Hou. Comparison between impingement/effusion and double swirl/effusion cooling performance under different effusion hole diameter[J]. International Journal of Heat and Mass Transfer, 2019, 141: 1097-1113.

[14] Kun Du, Zhigang, Jun Li*, Effects of Trenched Film Hole Configurations on the Endwall Film Cooling and Scution Side Phantom Cooling[J]. Journal of Thermal Sceince, 2019, 28(5): 905-914.

[15] Kaiyuan Zhang, Zhigang Li, Jun Li*, Effect of inflow swirl on the vane ednwall aerothermal performance with endwall misalignment at transonic condition[J]. International Journal of Heat and Mass Transfer, 2019, 144: 118662-1-17.

[16] Cheng SHuxian, Li ZHigang, Li Jun*, Effects of endwall profiling near the blade leading edge on the sealing effectiveness of turbine rim seal[J]. Proc. IMechE Part A: J. Power and Energy, 2019, 233(7): 821-833.

 

中文期刊论文

[1] 方志，李志刚，李军，孔型几何参数对孔型密封泄漏和鼓风加热特性影响研究[J].西安交通大学学报，2019, 53(1): 135-141,147.

[2] 程舒娴，李志刚，李军*，端壁造型对轮缘密封流场和封严效率的影响[J], 西安交通大学学报, 2019, 53(3): 20-27.

[3] 张元桥，李志刚，李军*，晏鑫，刷式-迷宫密封泄漏流动和转子动力特性数值研究[J]. 西安交通大学学报, 2019, 53(3): 28-35.

[4] 姚韵嘉，祝培源，陶志，宋立明，李军，间隙射流对端壁气膜冷却性能影响的实验研究[J]. 西安交通大学学报, 2019, 53(3): 43-49.

[5] 李琛玺，郭振东、宋立明，李军，丰镇平，凹槽状叶顶气膜冷孔优化设计与知识挖掘[J],推进技术，2019, 40(2): 276-284.

[6] 李军，李志刚，张元桥，王凌峰，刘璐园，刷式密封技术的研究进展[J]. 航空发动机，2019, 45(2): 74-84.

[7] 杜昆，李军*，微肋片结构的涡轮静叶端壁气动和冷却特性的数值研究[J]. 工程热物理学报，2019, 40(3): 520-528.

[8] 陶志，郭振东，李琛玺，宋立明，李军，丰镇平，基于Kriging的不确定性量化及鲁棒性优化的研究[J]. 工程热物理学报，2019， 40(3): 537-542.

[9] 刘璐园，张元桥，李军*，基于流固耦合方法的刷式密封刷丝束变形及接触力特性的数值研究[J]. 燃气轮机技术， 2019，32(1): 1-7.

[10] 邵卫东，李军*，间断伽辽金玻尔兹曼方法中的基于完全耦合层技术的吸收边界条件研究[J].工程热物理学报, 2019, 40(4): 767-775.

[11] 张凯垣，杜昆，宋立明，李军*，预旋槽缝流及间隙射流对端壁冷却性能的影响[J]. 工程热物理学报，2019, 40(8): 1250-1255.

[12] 李志刚，袁涛，方志，李军*，超临界二氧化碳旋转机械动密封技术研究进展[J]. 热力透平, 2019, 48(3): 166-174,191.

[13] 姜世杰，李志刚，李军*， 凹槽状小翼对涡轮动叶叶顶气动和传热性能的影响[J]. 西安交通大学学报, 2019, 53(9):7-14.

[14] 马登骞，张元桥，李军*，晏鑫，考虑刷丝变形的后夹板结构对刷式密封泄漏和传热特性影响的研究[J].西安交通大学学报, 2019, 53(9): 15-25.

[15] 高庆，屈杰，马汀山，居文平，李军*，惠涛，轴向轮缘密封导流段几何结构对涡轮级气动冷却特性影响的数值研究[J]. 西安交通大学学报, 2019m 53(9): 26-33.

[16] 邓清华，胡乐豪，李军，丰镇平，超临界二氧化碳发电技术现状及挑战[J]. 热力透平，2019, 48(3): 159-165.

[17] 邓清华，胡乐豪，李军，丰镇平，大型发电技术发展现状及趋势[J].热力透平，2019, 48(3): 175-181.

 

国际学术会议论文

 [1] Yao Yunjia, Zhu Peiyuan, Tao Zhi, Song Liming, Li Jun, Experimental Study on the effect of Slot Jet on Film Cooling Performance on the Cascade Endwall With Purge Flow[C]. GT2019-90667, Proceedings of ASME Turbo Expo 2019: Turbomachinert Technical Conference and Exposition, GT2019, June 17-21, 2019, Phoenix, Arizon, USA.

[2] Chao Zhang, Jie Wang, Xin Luo, Liming Song, Jun Li, Zhenping Feng, Experimental Investigation on the Flat Plate Film Cooling Enhancement Using Vortex Generator Downstream fir the Cylinder Hole and Fan-Shaped Hole Configuration[C], GT2019-90671.

[3] Zigang Li, Zi Fang, Jun Li*, Zhenping Feng, Numercial Comparison of Static and Rotordynamics Characteristics for a Grooved-Stator/Smooth-Rotor and a Smooth-Stator/Groove-Rotor Liquid Annular Seals[C]. GT2019-90781.

[4] Shuxian Cheng, ZHigang Li, Jun Li*, Xin Yan, Liming Song, Numerical Investigations on the Sealing Effectiveness of Turbine Groove Radial Rim Seal[C]. GT2019-90205.

[5] Zhi Fang, Zhigang Li, Jun Li, Zhenping Feng, Numercial Investigations on the Static and Rotordynamic Characteristics of Hole-Pattern Seals with Annular of Pocket Grooves on Seal Stator[C]. GT2019-90776.

[6] ZHigang Li, Zhi Fang, Jun Li*, Zhenping Feng, Numercial Modelling of Static and Rotordynamic Characteristics for three Types of Hellically-Grooves Liquid Annular Seals[C]. GT2019-90779.

[7] Yuanqiao Zhang, Dengqian MA, Jun LI*, Yuan HE, Jingjin JI, Bo Sun, Zhigang LI, Xin YAN, EFfects of the Fence Height on the Leakage Flow Characteristics of Brush Seals[C]. GPPS-BJ-2019-0021, Proceedings of Global Power and Propulsion Society, Beijing Conference, 2019, Sept. 16-18, China

[8] Yuanqiao ZHANG, Jun LI*, Zhigang LI, Liming SONG, Xin YAN, Effect of Upstream Deflector Plate on the Leakage Flow and Heat Transfer Characteristics of Brush Seal with Annular Groove in Backing Plate[C]. ISABE-2019-24096, 24th International Society for Air Breathing Engines(ISABE), Conference, 22-27, Sept., 2019, Canberra, Australia.

[9] SHuxian CHENG, Jun LI*, Zhigang LI, Liming SONG, Numercial Investigations on the Sealing Effectiveness of Rim Seal and Heat Transfer Characteristics in Wheel-Space Cavity of Turbine Stage[C]. ISABE-2019-24097, 24th International Society for Air Breathing Engines(ISABE), Conference, 22-27, Sept., 2019, Canberra, Australia.

 

 2018年

英文期刊论文

[1] Zhigang Li, Jun Li*, Zhenping Feng, Numerical Investigation on the Leakage and Static Stability Characteristics of Pocket Damper Seals at High Eccentricity[J]. ASME Journal of ENgineering for Gas Turbines and Power, 2018, 140(4): 042503.

[2] Shunsen Wang, Chuang Wu, Jun Li, Exergoeconomic Analysis Optimization of Single-Pressure Single-Stage and Multi-Stage CO2 Transcritical Cycles for Engine Waste Heat Recovery: A Comparative Study[J]. Energy, 2018, 142(1): 559-577.

[3] Liming Song, Zhendong Guo, Jun Li*, Zhenping Feng, Optimization and Knowledge Discovery of a Three-Dimensional Parameterized Vane with Nonaxisymmetric Endwall[J]. AIAA Journal of Propulsion and Power, 2018, 34(1): 234-246.

[4] Kun Du, Zhigang Li, Jun Li*, Bengt Sunden, Effects of the swirl coolant jet from the upstream slot on the vane endwall cooling and the vane suction side phantom cooling[J]. International Journal of Heat and Mass Transfer, 2018, 121: 852-966.

[5] Kun Du, Jun Li*, Bengt Sunden, Effects of the coolin configurations layout near the first-stage vane leading edge on the endwall cooling and phantom cooling of the vane suction side surface[J]. International Journal of Heat and Mass Transfer, 2018, 123: 1021-1034.

[6] Weidong Shao, Jun Li*, Three time inr=tegration methods for incompressible flows with discontinuous Galerkin Boltzmann method[J]. Computer and Mathematics with Applications, 2018, 75: 4091-4106.

[7] Chuang Wu, Shun-sen Wang, Jun Li, Parametric study on the effects of a recuperator on the design and off-design performance for a CO2 transcritical power cycle for low temperature geothermal plants[J]. Applied Thermal Engineering, 2018, 137: 644-658.

[8] Liming Song, Peiyuan Zhu, Jun Li*, Zhenping Feng, Effects of location and profile of upstream slot on the endwall aerothermal performance of a gas turbine blade[J]. Applied Thermal Engineering, 2018, 140: 637-656.

[9] Kun Du, Zhigang Li, Jun Li*, Bengt Sunden, Influence of the Pressure Side Injection Slot on the Cooling Performance of Endwall Surface[J]. Numerical Heat Transfer Part A: Applications, 2018, 73(8): 517-534.

[10] Chuang Wu, Shunsen Wang, Jun Li, Exergoeconomic analysis and optimization of a combined supercritical carbon dioxide recommpression Brayton/organic flash cycle for nuclear power plants[J]. Energy Conversion and Management, 2018, 171:936-952.

[11] Junfei Zhou, Xinjun Wang, Jun Li, Yandong Li, Effects of film cooling hole locations on flow and heat transfer characteristics of impingement/effusion cooling at turbine blade leading edge[J]. International Journal of Heat and Mass Transfer, 2018, 126: 192-205.

[12] Weidong SHAO, Jun LI*, An absorbing boundary condition based on perfectly matched layer technique combined with discontinuous Galerkin Boltzmann method for low Mach number flow noise[J]. Journal of Theoretical and Computational Acoustics, 2018, 26(4): 1850011-1-23.

[13] Zhigang Li, Luxuan Liu, Jun Li*, Ridge A. Sibold, Wing F. Ng, Hongzhou Xu, Michael Fox, Effects of Upstream Step Geometry on Axisymmerical Converging Vane Endwall Secondary Flow and Heat Transfer at Transonic Conditions[J]. ASME Journal of Turbomachinery, 2018, 140(12): 121008-1-14.

[14] Yan Gao, Xin Yan, Jun Li, Kun He, Investigations into film cooling and unsteady flow characteristics in a blade trailing edge cutback region[J]. Journal of Mechanical Science and Technology, 2018, 32(10): 5015-5029.

[15] Xin Yan, Xinbo Dai, Kang Zhang, Jun Li, Kun He, Effect of teeth bending and mushrooming damage on leakage performance of a labyrinth seal[J] Journal of Mechancial Science and Technology, 2018, 32(10): 4697-4709.

 

中文期刊论文

[1] 张元桥，闫嘉超，李军*，刷式密封泄漏和传热特性影响因素的数值研究[J]. 推进技术，2018, 39(1): 116-124.

[2] 陈尧兴，李志刚，晏鑫，李军*， 迷宫齿蘑菇型磨损时密封泄漏特性和转子动力特性系数研究[J].西安交通大学学报, 2018, 52(1): 40-46.

[3] 杜昆，李军*， 宋立明，晏鑫，李志刚. 涡轮端壁流动传热冷却性能研究进展[J]. 燃气轮机技术，2018, 1: 1-10.

[4] 李军，程舒娴，高庆，李志刚，晏鑫. 轮缘密封封严效率及结构设计研究进展[J]. 热力透平，2018, 47(1): 6-15.

[5] 邵卫东，李军*，格子玻尔兹曼方法中的特征无反射边界条件研究[J]. 工程热物理学报, 2018, 39(2): 277-284.

[6] 陈阳，李军*， 周帅，曹守洪，孔祥林，孙奇. 间隙泄漏对透平级气动性能影响的数值研究[J]. 西安交通大学学报, 2018, 52(4): 63-69.

[7] 程舒娴，李军*. 1.5级涡轮轮缘密封燃气入侵特性的数值研究[J].西安交通大学学报，2018， 52(5): 12-20,115.

[8] 李军，宋立明，孙皓，郭振东. 非轴对称端壁设计的高负荷涡轮气热性能研究进展[J]. 航空发动机，2018, 44(3): 1-11. 

[9] 邓清华，蒋宇，李军，丰镇平，超临界CO2动力循环实验关键技术研究：循环方案[J]. 热力透平，2018, 47(2): 92-98,144.

[10] 邓清华，蒋宇，李军，丰镇平，超临界CO2动力循环实验关键技术研究：动力部件[J]. 热力透平，2018, 47(2): 99-104.

[11] 张元桥，王妍，晏鑫，李军*，刷式密封泄漏流动及传热特性的研究 第二部分：传热特性[J].工程热物理学报，2018, 39(5): 970-976.

[12] 陈尧兴，李志刚，晏鑫，李军*，迷宫齿弯曲磨损时密封泄漏特性和转子动力特性系数研究[J].西安交通大学学报，2018, 52(6): 157-164.

[13] 张凯垣，李志刚，宋立明，李军*，槽缝射流旋流比和密度比对涡轮端壁冷却和吸力面泛冷却性能的影响[J].西安交通大学学报， 2018, 52(9): 95-101.

[14] 高炎，晏鑫，李军，尾缘开缝透平叶片内流动传热特性研究[J].西安交通大学学报, 2018, 52(10): 31-40.

 

国际会议论文

[1] Zhigang LI, Jun LI, Rotordynamic Characteristics Predictions for Annular Gas Seals Using the Transient CFD Method Based on a Multi-Frequency Whirling Model[C]. CITC201705053(Invited Lecture), The Thid Chinese International Turbomachinery Conference, APril 12-15, 2018, Chong Qing, China.

[2] Yaoxing CHEN, Zhigang LI, Xin YAN, Jun LI*, Effects of Mushroom-Shaped Tooth Wear on the Leakage Performance and Rotordynamic Coefficients of Labyrinth Seals[C]. Proceedings of ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition, GT2018-75147. Oslo, Norway.

[3] Zhigang LI, Luxuan LIU, Jun LI*, Rideg A. Sibold,Wing F. NG, Hongzhou XU, Michael Fox, Effects of Upstream Step Geometry on Axisymmetric Converging Vane Endwall Secondary Flow and Heat Transfer at Transonic Conditions[C]. GT2018-76236, Oslo, Norway.

[4] Junfei ZHOU, Xinjun WANG, Jun LI, Daren Zheng. Effects of Impinging Hole shapes on Double Swirl Cooling Performance at Gas Turbine Blade Leading Edge[C]. GT2018-75445.

[5] Xin Yan, Xinbo Dai, Kang Zhang, Jun Li, Kun He. Influence of Hole-Pattern Stator on Leakage Performance of Labyrinth Seals[C]. GT2018-75349.

[6] Zhigang Li, Zhi Fang, Jun Li*. Numerical Investigation on the Leakage and Rotordynamic Characteristics for Three Types of Annular Gs Seals in Wet Gas Conditions[C]. GT2018-75150.

[7] Yuanqiao Zhang, Jun Li*, Xin Yan, Zhigang Li. Investigations on the Leakage flow Characteristics of two Kinds of Brush Seals[C]. GT2018-76235.

[8] SHAO Weidong, LI Zhigang, SONG Liming, LI Jun*, Discontinuous Galerkin Boltzmann Method Combined With Absorbing Boundary Condition for Vane Noise in Low Reynolds Number Flow[C]. Proceedings of the 15th International Symposium on Unsteady Aerodynamics, Aeroacoustics & Aeroelasticity of Turbomachines. ISUAAAT15, 24-27, Sept. 2018, University of Oxford, UK.

[9] Jun Li, Zhigang Li, Liming Song, Qinghua Deng, Investigations on Unsteady Flow Excitation and Mechanical Performance of Last Turbine Stage Long Blade Using Fluid-Structure Interaction Method[C]. ASME 2018 IMECE International Mechanical ENgineering Congress & Exposition, Nov. 9-15, 2018, USA IMECE2018-86950.

 

2017年

英文期刊论文

[1] Liming Song, Peiyuan Zhu, Jun Li*, Zhenping Feng, Effect of purge flow on endwall flow and heat transfer characteristics of a gas turbine blade[J]. Applied Thermal Engineering, 2017, 110: 504-520.

[2] Feng Zhang, Xinjun Wang, Jun Li, Flow and heat transfer characteristics in rectangular channels using combination of convex-dimples with grooves[J]. Applied Thermal Engineering, 2017, 113: 926-936.

[3] Tieyu Gao, Junxiong Zeng, Jun Li, Jianying Gong, Numerical prediction on mist/stream cooling in a square ribbed channel at real gas turbine operational conditions[J]. International Journal of Heat and Mass Transfer, 2017, 108: 1089-1102.

[4] Chuang Wu, Shunsen Wang, Xihang Jiang, Jun Li, Thermodynamic analysis and performance optimization of transcritical power cycles using CO2-based binary zeotropic mixtures as working fluids for geothermal power plants[J]. Applied Thermal Engineering, 2017, 115: 292-304.

[5] Liming Song, Chao Zhang, Yingjie Song, Jun Li*, Zhenping Feng, Experimental investigations on the effects of inclindation angle and blowing ratio on the flat film cooling enhancement using the vortex generator downstream[J]. Applied Thermal Engineering, 2017, 119: 573-584.

[6] Kun Du, Zhigang Li, Jun Li*, Bengt Sunden, Influence of the upstream slot geometry on the endwall cooling and phantom cooling of vane suction side surface[J]. Applied Thermal Engineering, 2017, 121: 688-700.

[7] Kun Du, Liming Song, Jun Li*, Bengt Sunden, Effects of the mainstrea, turbulence intensity and slot injecton angle on the endwall cooling and phantom cooling of the vane scution side surface[J]. International Journal of Heat and Mass Transfer, 2017, 112: 427-440.

[8] Kun Du, Liming Song, Jun Li*, Bengt Sunden, Effects of the layout of film holes near the vane leading edge on the edneall cooling and phantom cooling of the vane scuution side surface[J]. Numerical Heat Transfer, Part A: Application, 2017, 71(9): 910-927.

[9] Chuang Wu, Shunsen Wang, Xuejia Feng, Jun Li. Eenergy, Exergy and exergoeconomic analyses of a combined supercritical CO2 recommpression Brayton/absorption refrigeration cycle[J]. Energy Conversion and Management, 2017, 148: 360-377.

[10] Feng Zhang, Xinjun Wang, Jun Li, Daren Zheng. Computations on the flow characteristics and sealing performance of a stator well cavity for the second stage in gas turbine[J]. Applied Thermal Engineering, 2017, 125: 1300-1319.

[11] Xinjun Wang, Feng Zhang, Daren Zheng, Jun Li. Effect of droplet characteristics and rotation speed on the flow and heat transfer characteristics of mist/air cooling in a rotational ribbed two-pass rectangular channel[J]. Proc. IMechE Part A: Journal of Power and Energy. 2017, 231(2): 119-132.

[12] Tieyu Gao, Junxiong Zeng, Qingfeng Xia, Jun Li. Jianying Gong. Effects of operating conditions on flow and heat transfer characteristics of mist cooling in a square ribbed channel[J]. Journal of Mechanical Science and Technology, 2017, 31(30： 1517-1530.

[13] Tieyu Gao, Jiangnan Zhu, Jun Li, Qingfeng Xia, Numerical study of the influenece of rib orientation on heat transfer enhancement in two-pass ribbed rectangukar channel[J]. Engineering Applications of Computational Fluid Mechanics, 2017, 12(1):117-136.

[14] Tieyu Gao, Junxiong Zeng, Jun Li, Jianying Gong, Effect of aspect ratio on the flow and heat transfer characteristics of mist steam in rectangular ribbed channel[J]. Numerical Heat Transfer Part A: Applications, 2017, 72(3): 255-273.

[15] Peiyuan Zhu, Liming Song, Jun Li, Zhenping Feng. Effects of upstream slot geometry on th eendwall aerothermal performance of a gas turbine blade under different ejection angle conditions[J]. International Journal of Heat and Mass Transfer, 2017, 115: 652-669.

[16] Feng Zhang, Xinjun Wang, Jun Li, Daren Zheng. Numerical investigation on the effect of radial location of sealing air inlet and its geometry on the sealing performance of a stator-well cavity[J]. International Journal of Heat and Mass Transfer, 2017, 115: 820-832.

[17] Zhou Junfei, Wang Xinjun, Li Jun, Lu Haikong. CFD analysis of mist/air film cooling on a flat plate with different hole types[J]. Numerical Heat Transfer, Part A: Applications, 2017, 71(11): 1123-1140.

 

国际会议论文

[1] Zhigang Li, Jun Li*, Qing Gao, Zhenping Feng, Effects of pressure ratio and rotational speed on the sealing effectiveness of turbine radial rim seal[C]. GPPF-2017-103, Proceedings of the 1st Global Power and Propulsion Forum, GPPF 2017, Jan. 16-18, 2017, Zurich, Switzerland.

[2] J. LI*, Z. LI, K. DU, K. WEN, X. YAN, L. SONG, Unsteady aerodynamic and Forces Characteristics of Dual Row Control Stage with Partial Admission Condition[C]. Proceedings of 12th European Conference on Turbomachinert Fluid Dynamics and Thermodynamics, Paper ID ETC2017-25, ETC12, April 3-7, 2017, Stockholm, Sweden.

[3] Minyan YIN, Jun LI*, Liming SONG, et al., Aerodynamic Optimization Design of Last Stage Long Blade for Steam Turbine Using Self-Adaptive Differential Evolutionary Algorithms and RANS Solution[C]. ASME Paper GT2017-63502.

[4] Zhigang LI, Jun LI*, Liming SON et al., Effect of Outer Fin Axial Gap on the Sealing Effectiveness and Fluid Dynamics of Radial Rim Seal[C]. ASME Paper GT2017-63505.

[5] Zhigang LI, Jun LI*, Zhenping FENG, Numerical Investigation on the Leakage and Static Stability Characteristics of Pocket Damper Seals at High Eccentricity Ratios[C]. ASME Paper GT2017-63562.

[6] Feng ZHANG, Xinjun WANG, Jun LI, et al., Numerical Study on the Flow and Heat Transfer Characteristics on Rectangular Channels with Grooves and Different Protrusions[C]. ASME Paper GT2017-63737.

[7] Chenxi LI, Zhendong GUO, Liming SONG, Jun LI, Zhenping FENG, Design Optimization of a 3D Parameterization Vane Cascade with Non-Axisymmetric Endwall Based on a Modifed EGO Algorihtm and Data Mining Technique[C]. ASME Paper GT2017-63738.

[8] Junfei ZHOU, Xinjun WANG, Jun LI, et al., Numerical Investigation on the Cooling Effectiveness among Air and Steam and Mist/Steam for a Gas Turbine Vane[C]. ASME Paper GT2017-63739.

[9] Yang CHEN, Zhuhai ZHONG, Jun LI*, et al., Effect of  Stage Axial Distance on the Aerodynmaic Performance of Three-Stage Axial Turbine using Experimental Measurements and Numerical Simulations[C]. ASME Paper GT2017-63790.

[10] Junxiong ZENG, Tieyu GAO, Jun LI et al., Numerical Investigatuion on Mist/Air Cooling in Rectangular Ribbed Channels with Various Aspect Ratios[C]. ASME Paper GT2017-63840.

[11] Yingjie SONG, Zhendong GUO, Liming SONG, Jun LI, Zhenping FENG, Knowledge-Based Aero-Thermal Multi-Disciplinary Design Optimization of a Hgh Temperature Blade[C]. ASME Paper Gt2017-63880.

[12] Meng LIU, Yang CHEN, Zhuhai ZHONG, Xiaodong ZHANG, Guoliang DENG, Mingyan YIN, Jun LI, Qi SUN, Numerical Tests on the Effect Factors of the Last Stage Blade for Low Pressure Exhaust Hood Simulation[C]. ASME Paper GT2-17-63964.

[13] David E. Mayo, Jr. Allan Arisi, Wing F. NG, Zhigang Li, Jun Li, Hee-Koo Moon, Luzeng Zhang, Effect of Combustor-Turbine Platform Misalignment on the Aerodynamics and Heat Transfer of an Axisymmetric Converging Vane Endwall at Transonic Conditions[C]. ASME Paper GT2017-65091.

[14] Mingyan YIN, Jun LI*, Liming SONG, et al., Numerical Investigations on the Long Blade Performance Using RANS Solution and FEA Method Coupled with One-way and Two-way Fluid-Structure Interaction[C]. ASME Paper PowerEnergy2017-3100.

[15] Jun Li, Yuanqiao Zhang, Xin Yan, Zhigang Li. Investigations on the Leakage Flow Characteristics of the Brush Seal with Annular Pressure Reduction Groove[C]. ISABE-2017-21331, ISABE 2017 Conference, Sept. 3-8, 2017, Manchester, UK.

[16] Jun Li, Qing Gao, Zhigang Li, Limig Song. Effect of RimSeal Purge Flow on the Aerodynamic Performance of Turbine Stage and Cooling Effectiveness of Rotor Blade Endwall Part I: Coolant Flow Rate[C]. ISABE-2017-21337, ISABE 2017 Conference, Sept. 3-8, 2017, Manchester, UK.

[17] Jun Li, Qing Gao, Zhigang Li, Limig Song. Effect of RimSeal Purge Flow on the Aerodynamic Performance of Turbine Stage and Cooling Effectiveness of Rotor Blade Endwall Part II: Inlet Preswirl[C]. ISABE-2017-21338, ISABE 2017 Conference, Sept. 3-8, 2017, Manchester, UK.

[18] Kang Zhang, Xinbo Dai, Xin Yan, Jun Li, Effect of Stator Rub Grooves on Leakage Performance of a Stepped Labyrinth Seal[C]. Global Power & Propulsion Society 2017 Conference, Oct. 31-Nov. 1, 2017. Shanghai China

 

中文期刊论文

[1] 邵卫东，李志刚，李军*，二维时间发展混合层噪声的直接数值模拟[J]. 西安交通大学学报，2017, 51(1): 38-44.

[2] 杜昆，李军*，涡轮叶片凹槽状叶顶非定常流动传热特性的数值研究[J]. 推进技术，2017, 38(3): 551-558.

[3] 张超，宋英杰，宋立明，李军，丰镇平，涡发生器高度对气膜冷却性能影响的实验研究[J].西安交通大学学报，2017, 51(3): 20-26.

[4] 张元桥，王妍，晏鑫，李军*， 刷式密封泄漏流动及传热特性的研究，第一部分：泄漏特性[J].工程热物理学报, 2017, 38(3): 482-489.

[5] 张元桥，闫嘉超，李军*，考虑闭合效应的刷式密封泄漏特性研究[J]. 润滑与密封，2017, 42(4): 36-42.

[6] 李琛玺，王静，宋立明，李军，丰镇平，高压比离心叶轮气动强度多学科优化与知识挖掘[J]. 西安交通大学学报，2017, 51(5): 102-111.

[7] 李志刚，陈尧兴，李军*. 高偏心率下旋转密封泄漏特性和静态动力特性研究[J]. 西安交通大学学报, 2017, 51(7): 1-7.

[8] 黄琰，晏鑫，何坤，李军，丰镇平. 压力面侧小翼结构对凹槽叶顶冷却传热性能的影响[J]. 西安交通大学学报, 2017, 51(7): 51-56.

[9] 高庆，廖高良，张永海，余小兵，高登攀，刘安，居文平，李军*. 透平级气动及运行参数对轮缘密封封严性能影响的数值研究[J]. 西安交通大学学报, 2017, 51(7): 62-72.

[10] 杜昆，宋立明，高铁瑜，李军*. 端壁相对运动对叶顶流动传热特性影响的研究[J].燃气轮机技术, 2017, 30(2): 11-16.

[11] 邵卫东，吴方松，李伯武，尹刚，张元林，宋立明，李军*. 汽轮机低压进汽结构气动性能分析与优化设计[J]. 热力透平，2017， 46(2): 69-75.

[12] 张峰，王新军，李军，丰镇平. 肋片-凹槽通道内的流动与换热特性数值研究[J]. 工程热物理学报, 2017, 38(7): 1512-1518.

[13] 冀大伟，李军*，宁宵，防旋板对迷宫密封转子动力特性影响的研究[J]. 热力透平，2017， 46(3): 164-168.

[14] 陈尧兴，李志刚，李军*，非均匀进汽时迷宫密封汽流激振动力特性的研究[J]. 西安交通大学学报, 2017, 51(9): 145-152.

[15] 李军，陈阳，宋立明，高庆，李志刚. 考虑轮缘密封射流与主流相互作用的透平级气热性能研究进展[J]. 燃气轮机技术, 2017, 30(3): 18-26,31.

[16] 祝培源，宋立明，李军，丰镇平. 间隙位置和几何对端壁冷却性能的影响[J]. 航空学报，2017, 38(9): 520942.

[17] 陶志，祝培源，宋立明，李军，丰镇平.三角形涡发生器综合换热性能全局优化和知识挖掘[J]. 推进技术, 2017, 38(10): 2298-2305.

[18] 陈尧兴，李志刚，李军*. 进口预旋对高压迷宫密封流体激振转子动力特性的影响[J]. 润滑与密封. 2017, 42(11): 1-6.

[19] 程淑娴，晏鑫，李志刚，宋立明，李军*. 径向轮缘密封预旋盘腔流动换热特性数值研究[J]. 工程热物理学报. 2017, 38(8): 1647-1654.

[20] 祝培源，陶志，宋立明，李军，丰镇平. 间隙射流对端壁冷却和传热特性影响的研究[J]. 推进技术, 2017, 38(9): 2029-2037.

[21] 颜勇，祝培源，宋立明，李军，丰镇平. 基于非平衡高斯过程的叶栅加工误差不确定量化[J]. 推进技术, 2017, 38(8): 1767-1775.

 

2016年

英文期刊论文

[1] Zhigang Li, Jun Li*, Zhenping Feng, Numerical Comparison of Rotordynamic Characteristics for a Fully Partitioned Pocket Damper Seal and a Labyrinth Seal With High Positive and Negative Inlet Preswirl[J]. ASME Journal of ENgineering for Gas Turbines and Power, 2016, 138(4): 042505-1-13.

[2] Zhigang Li, Jun Li*, Zhenping Feng, Comparison of Rotordynamic Characteristics Predictions for Annular Gas Seals Using the Transient Computational Fluid Dynamic Method based on Different Single-Frequency and Multi-Frequency Rotor Whirling  Models[J], ASME Journal of Tribology, 2016, 138(1): 011701-18.

[3] Song, L., Li, J.*, Wen, K., Aerodynamic performance analysis of partial admission dual row control stage at different working conditions[J]. J. of Mechanical Science and Technology, 2016, 39(1): 157-169.

[4] Zhang, F., Wang, X, Li, J., Numerical investigation of flow and heat transfer characteristics in radial preswirl system with different preswirl nozzle angles[J]. International Journal of Heat and Mass Transfer, 2016, 95:984-995.

[5] Song, L., Guo, Z., Li, J.*, Feng, Z., Research on Metamodel-Based Global Design Optimization and Data Mining Methods[J]. ASME Journal of Engineering for Gas Turbines and Power, 2016, 138(9): 092604-1-14.

[6] Du, K., Li, J.*, Numerical  Study on the effects of slot injection configuration and endwall alignment mode on the film cooling performance of vane endwall[J]. International Journal of heat and mass tranfer.2016， 98： 768-777.

[7] Li, J.*, Gao, Q., Feng, Z., Numerical investigations on the sealing effectiveness of Turbine Honeycomb radial rim seal[J]. ASME Journal of Engineering for Gas Turbines and Power, 2016, 138(10): 102601-1-16.

[8] Li, J., Du, K., Song, L., Effects of Tip cavity geometries on the aerodynamic performance of the transonic blade with cavity tip[J]. Proc. IMechE Part A: J. Power and Energy, 2016, 230(3): 319-331.

[9] Feng Zhang, Xinjun Wang, Jun Li, Numerical investigation on the flow and heat transfer characteristics in radial pre-swirl system with different fillet radius at the junction of inlet cavity and nozzle[J]. Applied Thermal Engineering, 2016, 106: 1165-1175.

[10] Feng Zhang, Xinjun Wang, Jun Li, Numerical investugation of the flow and heat transfer characteristics for a pre-swirl rotor-stator system with center inflow[J]. Applied Thermal Engineering, 2016, 105: 646-658.

[11] Feng Zhang, Xinjun Wang, Jun Li, The effects of upstream steps with unevenly spanwise distributed height on rectangular hole file cooling performance[J]. International Journal of Heat and Mass Transfer, 2016, 102: 1209-1221.

[12] Zhigang Li, Jun Li*, Zhenping Feng, Labyrinth Seal Rotordynamic Characteristics Part I: Operational Conditions Effects[J]. Journal of Propulsion and Power, 2016, 32(5): 1199-1211.

[13] Zhigang Li, Jun Li*, Zhenping Feng, Labyrinth Seal Rotordynamic Characteristics Part II: Geometrical Parameters Effects[J]. Journal of Propulsiona and Power, 2016, 32(5): 1281-1291.

[14] Kun Du, Zhigang Li, Jun Li*, Effects of the Leading Edge Injection Slot on the Film Cooling and Heat Trasfer Performance of the Vane Endwall[J]. International Joural of Heat and Mass Transfer, 2016, 102: 1308-1320.

[15] Xinjun Wang, Gaoliang Liao, Feng Zhang, Jun Li, Numerical investigation on the steady and unsteady flow characteristics of rim seal for the first stage in gas turbine[J]. Applied Thermal Engineering, 2016, 99:11-22.

[16] Zhigang Li, Jun Li*, Zhenping Feng, Numerical comparsions of rotordynamic characteristics for three types of labyrinth gas seals with inlet preswirl[J]. Proc. IMechE Part A: Journal of power and Energy, 2016, 230(7): 721-738.

 

国际会议论文

[1] Jun LI, Wenhao HUO, Zhenping FENG, Investigations on the Effect of Cooling Structure on the Steam Cooling Performance of the Ineermediate Pressure Turbine Stage[C]. ASME Paper 2016-56179.

[2] Jun LI, Bin LI, Liming SONG, et al., Multidisciplinary Optimization Design of Long Blade Turbine Stage Based on parallel Self-adaptive Multi-Objective Differential Evolution Algorithm[C]. ASME Paper GT2016-56180.

[3] Yang CHEN, Jun LI*, Chaoyang TIAN, et al., Experimenal and Numerical Inestigations on the Aerodynamic Performance of the Three-stage Turbine With Consideration of the Leakage Flow Effect[C]. ASME Paper GT2016-56407.

[4] Weidong SHAO, Jun LI*, Subsonic Flow Over Open Cavities Part 1: Analytical Models and Numerical Investigations[C]. ASME Paper GT2016-56414.

[5] Weidong SHAO, Jun LI*, Subsonic Flow Over Open Cavities Part 2: Passive Control Methods[C]. ASME paper GT2016-56415.

[6] Kun DU, ZHigang LI, Jun LI*, Numerical Investigation of the Blade Tip and Overtip Casing Aerothermal Performance in a High Pressure Turbine Stage[C]. ASME paper GT2016-56709.

[7] Liming Song, Zhigang Li, Jun Li*, Qing Gao, Tieyu Gao, Investigations on the Aerodynamic and Cooling Characteristics of Turbine Stahe With Consideration of The Rim Seal Purge Flow[C]. 6th EASN International Conference on Innovation in European Aeronautics Research, 18-21 Oct. 2016, Porto, Portugal.

[8] Liming Song, Zhigang Li, Jun Li*, Qing Gao, Tieyu Gao, Effect of Rim Seal Diversion Structure on the Aerodynamic and Coolig Performance of Turbine Rotor Blade and Endwall[C]. 6th EASN International Conference on Innovation in European Aeronautics Research, 18-21 Oct. 2016, Porto, Portugal

 

中文期刊

[1] 杜昆，宋立明，李军*，间隙和进口边界层厚度对跨音速涡轮叶顶流动换热特性影响的数值研究[J]. 燃气轮机技术，2015,4:22-27.

[2] 李志刚，李军*，丰镇平，进口预旋板对孔型密封非定常气流激振特性的影响[J]. 西安交通大学学报，2016,50（1）： 16-21.

[3] 李彬，宋立明，李军*，长叶片透平级非定常汽流激振数值研究[J].工程热物理学报，2016，37(1):56-61.

[4] 邵卫东，李军*，计算气动声学中的伽辽金玻尔兹曼方法研究[J].西安交通大学学报，2016，50(3):134-140.

[5] 高炎，晏鑫，李军，燃气透平叶片尾缘开缝结构冷却性能的数值研究[J]. 西安交通大学学报，2016,50(3): 29-37.

[6]陈秀秀，晏鑫，李军，蜂窝叶顶密封对透平级气动性能的影响研究[J]. 西安交通大学学报，2016, 50(4): 14-20.

[7]杜昆，李军*，跨音速涡轮叶顶间隙流动传热特性的数值研究[J]. 西安交通大学学报，2016,50（4）： 147-152.

[8] 高庆，李军*，涡轮蜂窝面径向轮缘密封封严性能的数值研究[J].推进技术，2016，37(5): 937-944.

[9] 程舒娴，高铁瑜，李军*，圆孔形预旋喷嘴转静盘腔内流动换热特性数值研究[J]。 热能动力工程，2016, 31（4）： 59-66.

[10]钟刚云，李军*，霍文浩，范小平，超超临界汽轮机合缸轴端漏汽量对中压第1级透平级冷却性能的影响[J].动力工程学报，2016, 36(5): 352-359.

 [11] 邵卫东，李军*，考虑对流效应的圆柱扰流气动噪声的预测[J].工程热物理学报，2016, 37(10): 2097-2102.

[12] 杜昆，李军*，宋立明，丰镇平，跨音速涡轮静叶上端壁结构对动叶顶部气动换热特性的影响[J].工程热物理学报，2016,37(11): 2319-2324.

[13] 宋英杰，郭振东，宋立明，李军，丰镇平，显著变量识别与高温叶片多学科设计优化方法[J].推进技术,2016, 37(7): 1215-1223.

[14] 李军，霍文浩，陈尧兴等,超超临界汽轮机中压缸冷却技术研究进展[J]。热力透平,2016, 45(3): 175-183.

[15] 张元桥，李彬，杨建道，史立群，李军*，丰镇平，末级长叶片透平级气动性能的数值研究[J].热力透平, 2016, 45(3): 200-206.

 

2015年

英文期刊论文

[1] Zhigang Li, Jun Li*, Zhenping Feng, Numerical Investigations on the Leakage and Rotordynamics Characteristics of Pocket Damper Seals - Part I: Effects of Pressure Ratio, Rotational Speed, and Inlet Preswirl[J], ASME Journal of Engineering for Gas Turbines and Power, 2015, 137(3): 032503-1-15.

[2] Zhigang Li, Jun Li*, Zhenping Feng, NUmerical Investigations on the Leakage and Rotordyamics Characteristics of Pocket Damper Seals - Part II: Effects of Partition Wall Type, Partition Wall Number, and Cavity Depth[J], ASME Journal of Engineering for Gas Turbines and Power, 2015, 137(3): 032503-1-13.

[3] Xin Yan, Kun Hem Jun Li*,Zhenping Feng, Numerical Investigations on Rotordynamic Characteristic of Hole-pattern Seals With Two Different Hole Diameters[J], ASME Journal of Turbomachinery, 2015, 137(7): 071011-1-18.

[4] Xin Yan, Kun He, Jun Li, Zhenping Feng, A Generalized Prediction Method for Rotordynamic Coefficients of Annular Gas Seals[J], ASME Journal of Engineering for Gas Turbines and Power, 2015, 137(9): 092506-1-12.

[5] Zhendong Guo, Liming Song, Zhiming Zhou, Jun Li, Zhenping Feng, Multi-Objective Aerodynamic Optimization Design and Data Mining of a High Pressure Ratio Centrifugal Impeler[J], ASME Journal of Engineering for Gas Turbines and Power, 2015, 137(9): 092602-1-14.

[6] Gaoliang Liao, Xinjun Wang, Jun Li, Junfei Zhou, Effect of Trench Width and Blowing Ratio on Double-Jet Film Cooling Embedded in Trenches[J], Proc. IMechE Part A: Journal of Power and Energy, 2015, 229(3): 256-269.

[7] Gaoliang Liao, XInjun WANG , Jun Li, et al., Numerical Investigation on the flow and Heat Transfer in a Rotor-Stator Disc Cavity[J], Applied Thermal Engineering, 2015, 87: 10-23.

[8] Feng Zhang, Xinjun Wang, Gaoliang Liao, Jun Li, Computational fluid dynamics analysisi for effect of length to diameter ratio of nozzles on performance of pre-swirl systems[J]. Proc. IMechE Part a: Journal of Power and Energy, 2015, 229(4): 381-392.

[9] Zhao Liu, Jun Li, Zhenping Feng, Terrence Simon, Numerical study on the effect of jet nozzle aspect ratio and jet angle on swirl cooling in a model of a turbine blade leading edge cooling passage[J]. International Journal of Heat and Mass Transfer, 2015, 90: 986-1000.

[10] Zhao Liu, Jun Li, Zhenping Feng, Numerical Study of Swirrl Cooling in a Turbine Blade Leading Edge Model[J]. Journal of Thermophysics and Heat Transfer, 2015, 29(1): 166-178.

[11] Feng Zhang, Xinjun Wang, Jun Li, Effects of coolants on the flow and heat transfer characteristics in a non-rotating and rotating two-pass rectangular channel[J], International Journal of heat and mass Transfer, 2015, 91:390-400.

 

国际学术会议

[1] zhendong Guo, Liming Song, Jun Li, Guojun Li, zhenping Feng, Research on Meta-model Based Global Design Optimization and Data Mining Method[C], GT2015-42554, ASME Turbo Expo 2015, June 15-19, Montreal, Canada.

[2] Weidong Shao, Jun Li*, Theoretical and Numerical Investigations on the Aeroacoustical Oscillation of Flow Past the Cavity[C], GT2015-42551, ASME Turbo Expo 2015, June 15-19, Montreal, Canada.

[3] Bo Qiu, Jun Li*, Heat Transfer Characteristics Analysis of Brush Seal using RANS and FEM Approach based on the Local Thermal Non-Equilibrium Porous Medium Model[C], GT2015-42550, ASME Turbo Expo 2015, June 15-19, Montreal, Canada.

[4] Zhigang Li, Jun Li*, Shizhu Wang et al. Numerical Investigations on the Aerodynamic Performance of Turbine Stage and Rotordynamic Characteristics of Stator Seal with Consideration of Supplementary Steam[C]， GT2015-42549, ASME Turbo Expo 2015, June 15-19, Montreal, Canada.

[5] Zhigang Li, Jun Li*, Zhenping Feng, Numerical Comparison of Rotordynamic Characteristics for a Fully-Partition Pocket Damper Seal and a Labyrinth Seal with high Positive and Negative Inlet Preswirl[C], GT2015-42923, ASME Turbo Expo 2015, June 15-19, Montreal, Canada.

[6] Jiangnan Zhu, Tieyu Gao, Jun Li, et al., Numerical Investigation of Secondary Flow Vortex Core Structure in the Two-pass Rectangular Channel with 45o Ribs[C]. GT2015-42782. ASME Turbo Expo 2015, June 15-19, Montreal, Canada.

[7] Jiangnan Zhu, Tieyu Gao, Jun Li, et al. Conjugate heat transfer analysis of rectangular cooling channel with 45-degree ribs[C]. Proceedings of the ASME-JSME-KSME Joint Fluids Engineering Conference 2015, AJK2015-02485, 1-6.

[8] Jun LI*, Qing GAO, Jiayin TAO, Zhenping ENG, Numerical investigation on the flow and heat transfer characteristics of turbine radial rim seal system[C], ISABE-2015-20051, Phoenix, AZ, USA.

[9] Jun LI*, Qing GAO, Jiayin TAO, Zhenping FENG, Effects of the sealing structures on the unsteady mainstram ingetion characteristics of turbine rim seal using URANS and an additional passive tracer method solutions[C], ISABE-2015-20052, Phoenix, AZ, USA.

[10] Jun L*, Kun Du, Liming Song et al. Effect of Inlet Temperature Distribution on the Heat Transfer and Film Cooling Performance of Squealer Blade Tip[C]. International Gas Turbine Congress 2015, Nov. 15-20, Tokyo, China

[11] Peiyuan Zhu, Zhendong Guo, Liming Song, Jun Li, et al. Gloabl Design Optimization and Knowledge Discovery Method of an Exhaust Hood[C]. International Gas Turbine Congress 2015, Nov. 15-20, Tokyo, China.

 

中文期刊论文

[1] 杜昆，李军*，晏鑫，槽缝射流对静叶端壁冷却性能的影响[J], 西安交通大学学报，2015, 49(1): 21-26.

[2] 郭振东，宋立明，李军，丰镇平，基于子元模型的全局优化与设计空间知识挖掘方法[J]，推进技术，2015，36(2): 207-216.

[3] 杨建道，陈涛文，宋立明，李军*，低压排汽缸气动优化设计[J]，西安交通大学学报，2015, 49(3): 19-24.

[4] 高庆，李军*，间隙结构对轮缘密封封严性能及透平级气动性能影响的数值研究[J], 西安交通大学学报，2015，49(3): 25-31, 128.

[5] 霍文浩，李军*，钟刚云等，冷却结构对中压透平级蒸汽冷却性能影响的研究[J], 西安交通大学学报，2015, 49(5): 36-42.

[6] 王世柱，李志刚，李军*等，补汽对透平级气动性能和静叶汽封转子动力特性影响的数值研究[J]，西安交通大学学报，2015,49(5): 56-61.

[7] 邱波，李军*，基于多孔介质局部非热平衡方法的刷式密封耦合传热特性[J]，航空动力学报，2015, 30(5): 1067-1075.

[8] 李志刚，宁宵，晏鑫，李军*，蜂窝面迷宫密封泄漏特性和鼓风加热特性研究[J]. 工程热物理学报，2015， 36(6)： 1196-1200.

[9] 王世柱，李志刚，李军*， 等，旋转动密封非定常气流激振转子动力特性研究[J], 工程热物理学报，2015, 36(8): 1672-1676.

[10] 宋英杰，聂俊，郭振东，宋立明，李军，丰镇平,高温叶片换热性能不确定性量化[J], 工程热物理学报, 2015, 36(8): 1666-1671.

[11] 张峰，王新军，李军，带肋U型通道中的汽雾/空气流动与换热数值研究[J], 西安交通大学, 2015, 49(9): 52-57.

 

2014年

中文期刊论文

[1] 李彬，宋立明，李军*，丰镇平，长叶片透平级多学科多目标优化设计[J], 西安交通大学学报， 2014， 48(1): 1-6.

[2] 陶加银，高庆，宋立明，李军*，涡轮轮缘密封非定常主流入侵特性的数值研究[J]，西安交通大学学报，2014, 48(1): 53-59.

[3] 李彬，宋立明，李军*，基于双向流固耦合的长叶片气动和强度性能的数值研究[J]，推进技术，2014, 35(2): 202-207.

[4] 廖高良，王新军，李军，带槽双射流气膜冷却数值研究[J],西安交通大学学报，2014,48(3): 34-38.

[5] 杜昆，晏鑫，李军*，燃气透平凹槽状叶顶气膜冷却特性研究[J],燃气轮机技术，2014,27(1): 27-31.

[6] 李瑜，宁德亮，李亮，李军，汽轮机中湿汽损失的定量计算[J]，西安交通大学学报，2014, 48(1): 25-30.

[7] 杜昆，晏鑫，李军*，燃气透平凹槽状叶顶气膜冷却特性研究[J],燃气轮机技术，2014,27(1): 27-31.

[8] 晏鑫，李军，丰镇平，孔型阻尼密封非定常气流激振特性的研究[J],工程热物理学报，2014, 35(4): 651-654.

[9] 杜昆，宋立明，李军*，凹槽状叶顶涡轮叶片传热特性的数值研究[J],推进技术，2014, 35(5): 618-623.

[10] 薛志恒，李军，王伟锋，付昶，动力透平叶栅的多工况气动性能优化[J],热力发电，2014,43(3):  9-13,29.

[11]  文柯淞，杨建道，杨锐，史立群，李军*，丰镇平，超超临界二次再热高压缸流热固耦合特性研究[J]，热力透平，2014,43(2): 101-106.

[12] 高庆，李军*，径向轮缘密封封严效率的数值研究[J]，西安交通大学学报，2014, 48(9): 55-61.

[13] 何坤，晏鑫，李军，丰镇平，燃气透平叶栅端壁传热特性的数值研究[J],工程热物理学报，2014, 35(8): 1503-1507.

[14] 陶加银，高庆，宋立明，晏鑫，李军*，丰镇平，基于附加示踪变量法的涡轮轮缘密封非定常封严特性研究[J]，工程热物理学报，2014，35(11): 2154-2158.

[15] 李彬，宋立明，李军*，阻尼拉金结构的长叶片透平级气动性能数值研究[J]，东方汽轮机，2014， 4:12-16.

[16] 宋英杰，余广霖，宋立明，李军，丰镇平，高温叶片流热固耦合分析及多目标多学科设计优化[J]，工程热物理学报，2014,35（12）： 2367-2371.

 

国际会议论文

[1] Zhendong GUO, Zhiming ZHOU, Liming SONG, Jun LI, Zhenping FENG, Aerodynamic Analysis and Multi-Objective Optimization Design of a High Pressure Ratio Centrifugal Impeller[C], GT2014-25496, Proceedings of ASME Turbo Expo 2014, June 16-20, 2014, Duesseldorf, Germany.

[2] Gaoliang Liao, Xinjun Wang, Jun Li, Feng Zhang, Effects of Curvature on the Film Cooling Effectiveness of Double-Jet Film Cooling [C], GT2014-26263, Proceedings of ASME Turbo Expo 2014, June 16-20, 2014, Duesseldorf, Germany.

[3] Qing GAO, Jun LI*, Zhenping FENG, EFfects of Coolant Injection Configuration on the Cooling Performance of Gas Turbine Stage Using CFD and Conjugate Heat Transfer Method [C], GT2014-25486, Proceedings of ASME Turbo Expo 2014, June 16-20, 2014, Duesseldorf, Germany.

[4] Jiandao Yang, Rui Yang, Liqun Shi, Hong Yang, Jun Li, Experimental and Numerical Investigation on Performance and Flow in the Last Stage Group of a Wet Steam Turbine[C], GT2014-25584, Proceedings of ASME Turbo Expo 2014, June 16-20, 2014, Duesseldorf, Germany.

[5] Yingjie SONG, Zhendong GUO, Liming SONG, Jun LI, Zhenping FENG, Multi-Objective and Multi-Disciplinary Optimization of Gas Turbine Blade Profile and Cooling System Using Conjugate Heat Transfer Analysis[C], GT2014-25495, Proceedings of ASME Turbo Expo 2014, June 16-20, 2014, Duesseldorf, Germany.

[6] Hao SUN, Jun LI*, Liming SONG, Zhenping FENG, Non-Axisymmetric Turnine Endwall Aerodynamic Optimization Design Part I: Turbine Cascade Design and Experimental Validations[C], GT2014-25362, Proceedings of ASME Turbo Expo 2014, June 16-20, 2014, Duesseldorf, Germany.

[7] Hao SUN, Liming SONG, Jun LI*, Zhenping FENG, Non-Axisymmetric Turnine Endwall Aerodynamic Optimization Design Part II: Turbine Stage Design and Unsteady Flow Characteristics Analysis[C], GT2014-25364, Proceedings of ASME Turbo Expo 2014, June 16-20, 2014, Duesseldorf, Germany.

[8] Zhigang LI, Jun LI*, Zhenping FENG, Numerical Investigations on the Leakage and Rotordynamic Characteristics of Pocket Damper Seals Part I: Effects of Pressure Ratio, Rotational Speed and Inlet Preswirl[C], GT2014-25300, Proceedings of ASME Turbo Expo 2014, June 16-20, 2014, Duesseldorf, Germany.

[9] Zhigang LI, Jun LI*, Zhenping FENG, Numerical Investigations on the Leakage and Rotordynamic Characteristics of Pocket Damper Seals Part II: Effects of Partition Wall Type, Partition Wall Number and Cavity Depth[C], GT2014-25301, Proceedings of ASME Turbo Expo 2014, June 16-20, 2014, Duesseldorf, Germany.

[10] Jiandao YANG, Taowen CHEN, Jun LI*, Zhenping FENG, Aerodynamic Optimization Design of Exhaust Hood Diffuser for Steam Turbine with Three-dimensional Reynolds-Averaged Navier-Stokes Solutions[C], GT2014-25299, Proceedings of ASME Turbo Expo 2014, June 16-20, 2014, Duesseldorf, Germany.

[11] Jiangnan Zhu, Tieyu Gao, Jun Li, Guojun Li, Jianying Gong, The Effect of Vortex Core Distribution on Heat Transfer in a Steam Cooling of Gas Turine Blade Internal  Ribbed Channels[C], GT2014-25324, Proceedings of ASME Turbo Expo 2014, June 16-20, 2014, Duesseldorf, Germany.

[12] Kun Du, Jun Li*, Numerical Investigations on the Film Cooling Characteristics of Gas Turbine Blade With Squealer Tip[C], 2014-ISJPPPE-3001, the 5th International Symposium on Jet Propulsion and Power Engineering(ISJPPE), Sept. 15-19, 2014, Beijing, China.

[13] Kun Du, Jun Li*, Investigations on Film Cooling and Slot Purge Flow Cooling of the Gas Turbine Vane Endwall[C], 2014-ISJPPE-3005, the 5th International Symposium on Jet Propulsion and Power Engineering(ISJPPE), Sept. 15-19, 2014, Beijing, China.

[14] Qinghua Deng, Jun Li, Zhenping Feng, Numerical Investigation on Flow and Heat Transfer Characteristics of Blade Tip Gap in Gas Turbines[C], 2014-ISJPPE-3004, the 5th International Symposium on Jet Propulsion and Power Engineering(ISJPPE), Sept. 15-19, Beijing, China.

[15] Xin Yan, Kun He, Jun LI*, Effect of Rub Mushrooming Damage on the Leakage Flow Characteristucs of Labyrinth Seal[C], Eleventh International Conference on Flow Dynamics, Oct. 8-10, 2014, Sendai, Japan.

[16] Jun, Nie, Yingjie Song, Liming Song, Jun Li, Non-Intrusive Polyomial Chaos based on Uncertainty Quantification of Heat Transfer Performance of High Temperature Blade[C], Eleventh Internationa Conference on Flow Dynamics, Oct. 8-10,2014, Sendai, Japan.

[17] Bin, Li, Jun Li*, Numerical Investigations on the Aerodynamic Performance of Last Stage Buckets with Part-Span Connector[C], IMECE2014-38039, Nov. 14-20, 2014, Montreal, Canada.

 

2013年

英文期刊论

[1] Zhigang LI, Jun LI*, XIn YAN, Multiple Frequencies Elliptical Whirling Orbit Model and Transient RANS Solution Approach to Rotordynamic Coefficients of Annual Gas Seals Prediction[J], ASME Journal of Vibration and Acoustics, 2013, 135(3): 031005-1-14.

[2] Xiongwen Zhang, Siew-Chong Tan, Guojun Li, Jun Li, ZHenping Feng, Componnents Sizing of hybrid energy systems via the optimization of power dispatch simulaton[J], Energy, 2013, 52: 165-172.

[3] Guanghui Bai, Jun Li, Pengfei Fan, Guojun Li, Numerical investigations of th effects of different arrays on power extractions of horizontal axis tidal current turbines[J], Renewable Energy, 2013, 53: 180-186.

[4] Bo Qiu, Jun Li*, Numerical Investigations on the Heat Transfer Behavior of Brush Seals Using Combined Computational Fluid Dynamics and Finite Element Method[J], ASME Journal of Heat Transfer,  2013, 135: 122601-1-10.

[5] Yu Li, Liang Li, Tong Zhao, Jun Li, Aerodynamic optimization of a low-pressure multistage turbine using the response-surface method[J], Journal of Mechanical 

Science and Technology, 2013, 27(8): 2537-2546.

 

中文期刊论文

[1] 霍文浩，晏鑫，李军*，等，超超临界汽轮机高压缸旁路冷却系统流动特性的研究[J]，西安交通大学学报，2013，47(3): 42-47.

[2] 李军*，李志刚，晏鑫等，汽轮机排汽缸性能分析和气动设计的研究进展[J]，热力透平，2013, 42(1): 1-8.

[3] 霍文浩，晏鑫，李军*，等，超超临界汽轮机高压缸旁路冷却系统冷却特性的研究[J]，西安交通大学学报，2013，47(5): 24-30.

[4] 高庆，陶加银，宋立明，李军*，涡轮轮缘密封封严效率的数值研究[J]，西安交通大学学报，2013,47(5): 12-17.

[5] 宋立明，郭振东，李军，丰镇平，小展弦比调节级三维多目标气动优化设计[J], 工程热物理学报，2013，34(3): 431-434.

[6] 邱波，李军*，冯增国，江生科，孔祥林，两级刷式密封泄漏特性的实验和数值研究[J]，西安交通大学学报,2013, 47(7): 7-12.

[7] 孙皓，宋立明，李军*，丰镇平，非轴对称端壁透平级气动性能的数值研究[J]，西安交通大学学报，2013，47(7): 29-35.

[8] 孙皓，宋立明，李军*，透平叶栅非轴对称端壁优化设计[J]，西安交通大学学报，2013,47(9): 35-40.

[9] 邱波，李军*，刷式密封流动与换热及力学特性的研究进展[J]，热力透平，2013,42(3): 141-149.

[10] 邵卫东，杨建道，杨锐，史立群，李军*，汽轮机低压末三级耦合排汽缸的气动性能研究[J],热力透平，2013,42(3): 150-155.

[11] 邱波，李军*，丰镇平，考虑刷丝变形的刷式密封摩擦热效应研究[J]，工程热物理学报，2013,34(11): 2030-2034.

 

国际会议论文

[1] Wenhao HUO, Jun LI*, Jiandao Yang, Liqun Shi, Zhenoing Feng, Numerical Investigations on the Cooling Performance of the Internal Bypass Cooling System on the Ultra-Supercriical Steam Turbine[C], GT2013-94375, ASME Turbo Expo 2013, San Antonio, USA.

[2] Jun LI*, Zhigang LI, Zhenping FENG, Effects of the Last Stage Rotor Tip Leakage Flow on the Aerodynamic Performance of the exhaust hood for Steam Turbines[C], GT2013-94377, ASME Turbo Expo 2013, San Antonio, USA.

[3] LIU, Z., LI, J., FENg, Z., Numerical Study on the Effect of Jet Slot Height on Flow and Heat Transfer of Swirl Cooling in LEading Edge Model for Gas Turbine Blade[C], GT2013-94819, ASME Turbo Expo 2013, San Antonio, USA.

[4] Taowen CHEN, Jiandao YANG, Zhigang LI, Jun LI*, Numerical Investigations on the Aerodynamic Performance of the Full Last stage and Exhaust Hood of Steam Turbine[C]. Proceedings of the International Conference on Power Engineering (ICOPE-13), Oct. 23-27, 2013, WuHan, China.

[5] Jun LI*, Kesong WEN, Shizhu WANG, Xin YAN, Experimental and Numerical Investigations on the Leakage Flow Characteristics of Labyrinth Honeycomb Seal[C]. Proceedings of the International Conference on Power Engineering(ICIOPE-13), Oct. 23-27, 2013, WuHan, China.

[6] Yuci WANG, Bo QIU, Jun LI*, Effects of Pressure Ratios, Bristle pack Widths and Rotational Speeds on the Leakage Flow Characteristics of Brush Seal[C]. Proceedings of the International Conference on Power Engineering(ICOPE-13), Oct. 23-27, 2013, WuHan, China.

[7] Weidong SHAO, Jiandao YANG, Zhigang Li, Jun LI*, Numerical Investigations on the Aerodynamic Performance of the Low Pressure Cylinder with Five Stages for Large Power Steam Turbines[C]. Proceedings of the International Conference on Power Engineering(ICOPE-13), Oct. 23-27, 2013, WuHan, China.

[8] Xin YAN, Lijie LEI, Jun LI, Zhenping FENG, Effect of Bending and Mushrooming Damages on Heat Transfer Characteristic in Labyrinth Seals[C], TBTS2013-2012, ASME 2013 Turbine Blade Tip Symposium & Course Week, Sept. 30-Oct. 3, 2013, Hamburg, Germany.

  

2012年
英文期刊论文
[1] Liming SONG, Chang LUO, Jun LI, Zhenping FENG, Automated multi-objective and multidisciplinary design optimization of a transonic turbine stage, Proc. IMechE Part A: Journal of Power and Energy, 2012, 226: 262-276.

[2] Chang LUO, Liming SONG, Jun LI, Zhenping FENG, A Study on Multidisciplinary Optimization of an Axial Compressor Blade based on Evolutionary Algorithms[J], ASME Journal of Turbomachinery, 2012, 134:054501-1-5.

[3] Hao SUN, Jun LI*, Zhenping FENG, Investigations on Aerodynamic Performance of Turbine Cascade at Different Flow Conditions[J], Engineering Applications of Computational Fluid Mechanics, 2012, 6(2): 214-223.

[4] Kun HE, Jun LI, Xin YAN, Zhenping FENG, Investigations of the Conjugate heat transfer and windage effect in stepped labyrinth seals[J], International Journal of heat and Mass Transfer, 2012,55:4526-4657.

[5] Zhigang LI, Jun LI*, Xin YAN, Zhenping FENG, Numerical investigations on the leakage flow characteristics of pocket damper labyrinth seals[J], Proc. IMechE Part A: Journal of Power and Energy, 2012, 226(7): 932-948.

[6] Jun Li, Bo Qiu, Zhenping Feng, Experimental and Numerical Investigations on the leakage Flow Characteristics of the Labyrinth Brush Seal[J], ASME Journal of Engineering for Gas Turbines and Power, 2012, 134(10): 102509-1-9.

[7] Jun Li, Zhigang Li, Zhenping Feng, Investigations on the Rotordynamic Coefficients of Pocket Damper Seals Using the Multifrequency, One-Dimensional, Whirling Orbit Model and RANS Solutions[J], ASME Journal of Engineering for Gas Turbines and Power, 2012, 134(10): 102510-1-11.

[8] Xin YAN, Kun HE, Jun LI*, Zhenping FENG, Rotordynamic performance prediction for surface-roughened seal using transient CFD and elliptical orbit model[J], Journal of Power and energy, 2012, 226(8): 975-988.

国际会议论文
[1] Jun LI, Xin YAN, Liming SONG, et al., Effects of Squealer Rim Thickness on the Leakage Flow and Heat Transfer Characteristics of the GAs Turbine Blade Tip, AJCPP-009, Asian Joint Conference on Propulsion and Power, march 1-4, 2012, Xi'an China.
[2] Jia LIU, Xin YAN, Jun LI*, Zhenping FENG, Effect of Rotor Tip Cavity Flow on Aerdynamic Performance of Turbine Stages, AJCPP-049, Asian Joint Conference on Propulsion and Power, March 1-4, 2012, Xi'an China. 

[3] Jun LI, Bo QIU, Zhenping FENG et al., Experimental and Numerical Investigations on the Leakage Flow Characteristics of the Labyrinth Brush Seal[C], GT2012-69293.

[4] Jun LI, Jiandao YANG, Zhenping FENG et al., Analytical Investigations on the Contact Force Between Bristle pakcs and Shaft Surface of Brush Seals[C], GT2012-69305.

[5] Zhigang LI, Jun LI*, Xin YAN, et al., Investigations on the Flow Pattern and Aerodynamic Performance of Last Stage and Exhaust Hood for Large Power Steam Turbines[C], GT2012-69291.

[6] Xin YAN, Yizhi FAN, Xanyu SHANG, Kun HE, Jun LI, et al., Theoretical Investigations on Water Condensation in Main Steam Pipe[C], GT2012-69567.

[7] Wenhao HUO, Jun LI*, Xin YAN et al., Numerical Investigations on the Steam Cooling Performance of the First Two Middle Pressure Turbine Stages for Ultra-Supercritical Steam Turbines[C], GT2012-69302.

[8] Jun LI, Zhigang LI, Zhenping FENG, Investigations on the Rotordynamic Coefficients of Pocket Damper Seals Using the Multi-Frequency, One-Dimensional Whirl Orbit Model and RANS Solutions[C], GT2012-69296.

[9] Qing GAO, Yangzi HUANG, Jun LI*, et al., Effects of the Axial Fins Distance and Cavity Depth on the Leakage Flow Characteristics of the labyrinth Seal[C], Asian Congress on Gas Turbines 2012, ACGT2012-1060, August, 20-22, Shanghai, China.

[10] LI, Z., LI, J.*, FENG, Z., Numerical Investigations on the Leakage Flow and Rotordynamic Charcateristics of Labyrinth Seal[C], Proceedings of 4th International Symposium on Jet Propulsion and Power Engineering, ISJPPE-2012-A0041, Sept. 10-12 Xi'an, China.

[11] Jun LI, Kesong WEN, SHizhu WANG, Shengke JIANG, Xianglin KONG, Experimental and numerical investigations on the leakage flow characteristics of labbyrinth seal, paper No. FG-46, 7th international Symposium on Multiphase flow, heat mass transfer and energy conversion, Xi'an China, 26-30 Oc., 2012

 

中文期刊论文

[1] 孙皓，李军*，李国君等，非轴对称端壁造型技术在透平中的应用和发展[J]，热力透平，2012,41(1): 18-25.

[2] 李志刚，李军*，丰镇平，袋型阻尼密封转子动力特性的多频单向涡动预测模型[J], 西安交通大学学报,2012, 46(5): 13-18,19.

[3] 晏鑫，李军，丰镇平，迷宫密封传热特性的数值研究[J], 西安交通大学学报，2012，46(11): 1-5.

[4] 孙皓，宋立明，李军，丰镇平，小展弦比叶栅非轴对称端壁造型及气动性能的数值研究[J]，西安交通大学学报，2012, 46(11): 6-11.

[5] 晏鑫，李军，丰镇平，蜂窝密封内耦合传热特性的研究[J]，工程热物理学报，2012,33(10): 1683-1686.

[6] 李志刚，李军*，丰镇平，高转速袋型阻尼蜜蜂呢个泄漏的特性[J]，航空动力学报，2012，27(12);2828-2835.

[7] 邱波，李军*，陈春新，丰镇平，基于CFD和FEM的方法的刷式密封传热特性研究[J]，工程热物理学报，2012,33(12): 2067-2071.

2011年
英文期刊论文
[1] Song, L., Luo C. Li, J, Feng, Z., Aerodynamic optimization of axial turbomachinery blades using parallel adaptive range differential evolution and Reynolds-averaged Navier-Stokes solutions[J], INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN BIOMEDICAL ENGINEERING, 2011, 27:283-303.(Corresponding author)
[2] Yan, X., Li, J., Feng, Z., Investigations on the Rotordynamic Characteristics of a Hole-Pattern Seal Using Transient CFD and Periodic Circular Orbit Model[J], ASME Journal of Vibration and Acoustics, 2011, 133(4): 041007.(Corresponding author)
[3] zhigang Li, Jun Li, Xin Yan, Zhenping Feng, Effects of Pressure Ratio and Rotational Speed on Leakage Flow and Cavity Pressure in the Staggered Labyrinth Slea, ASME Journal of Engineering for Gas Turbine and Power, 2011,133(11): 114503.
[4] X Yan, J Li, Z Feng, Effects of sealing clearance and stepped geometries on discharge and heat transfer characteristics of stepped labyrinth seals, Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy, 2011, 225: 521-538.
[5] Jun LI, Hao SUN, Jinshan WANG, Zhenping FENG, Numerical Investigations on the STeady and Unsteady Leakage Flow and Heat Transfer Characteristics of Rotor Blade Squealer Tip, Journal of Thermal Science, 2011, 20(4): 304-311.

中文期刊论文
[1] 李志刚，李军，丰镇平，蜂窝密封泄漏特性的数值研究和泄漏量计算公式的构造[J], 机械工程学报，2011, 47(2): 142-148.
[2] 李志刚，郞骥，李军，丰镇平，迷宫密封泄漏特性的试验研究[J], 西安交通大学学报，2011, 45(3): 48-52.
[3] 晏鑫，李军，丰镇平，蜂窝密封内流动传热及转子流动特性的研究进展[J]，力学进展，2011,41(2):201-216.
[4] 阳虹，杨建道，李军等，汽轮机调节级气动性能分析和结构优化设计[J],热力透平,2011,40(1):5-10.
[5] 钟刚云，冯玲，吴其林，李军，大功率汽轮机调节级级段气动特性研究[J],热力透平,2011,40(1): 11-15.
[6] 李军，孙皓，李彬等，透平机械高负荷叶片和大焓降级的研究进展[J],热力透平,2011,40(1): 16-21.
[7] 陈春新，邱波，李军，丰镇平，刷式密封迟滞特性的数值研究[J], 西安交通大学学报，2011,45(5): 36-41.
[8] 霍文浩，祁明旭，李军，丰镇平，超临界汽轮机中压透平级流动传热特性研究[J]，西安交通大学学报，2011,45(7): 9-14.
[9] 邱波，李军，刷式密封传热特性研究[J], 西安交通大学学报，2011，45(9): 94-100.
[10] 李军，李志刚，袋型阻尼密封泄漏流动和转子动力特性的研究进展[J]，力学进展，2011,41(5): 519-536.


国际会议论文
[1] Zhigang LI, Jun LI, Zhenping FENG, et al., Numerical Investigations on the Leakage Flow Characteristics of Pocket Damper Seals, GT2011-45114, Proceedings of ASME Turbo Expo 2011, Vancouer, Canada.
[2] Zhong Gangyun,LI Jun, LI Zhigang, YAN Xin, WU Qilin, Numerical Investigations on Aerodynamic Performance of Nozzle Control Stage for a 600MW Steam Turbine Under Different Backing Pressures Conditions, ASME Power 2011 & ICOPE-2011,Junly 12-14, 2011, Denver, USA.
[3] YANG Rui, YANG Jiandao, PENG Zeying, SHI Liqun, HE Aping, YANG Hong, ZHOU Daiwei, LI Jun et al., Numerical Investigations on the Aerodynamic Performance of Last Stage-Exhaust Hood for Steam Turbines, ASME Power 2011 & ICOPE-2011, July 12-14, 2011, Denver, USA.
[4] Jun LI, Yangzi HUANG, Bo Qiu, Zhenping FENG, Numerical Investigations on the Leakage Flow and Pressure Distributions of the Conventional and Low-Hysteresis Brush Seal with Four Clearances, ISABE-2011-1828, 20th ISABE Conference, Sept. 13-18, 2011, Gothenburg, Sweden.
[5] Jun LI, Chunxin CHEN, Bo Qiu, Zhenping FENG, Effects of Bristle Lay Angle, Bristle Diameter and Length on the Hysteresis Characteristics of Brush Seals, ISABE-2011-1833, 20th ISABE Conference, Sept. 13-18, 2011, Gothenburg, Sweden.
[6] Jun LI, Xin YAN, Liming SONG, Shaojun LI, Zhenping FENG, Effects of Rotor Tip Leakage on the Unsteady Flow Fields of Stator Blade in a One and Half Turbine Stage, 10th International Gas Turbine Congress in Japan, IGTC’11 Osaka, Nov. 13-18, 2011.
[7] Jun LI, Xin YAN, Liming SONG, Shengru KONG, Zhenping FENG, Numerical Investigations on the Leakage Flow Characteristics of Different Honeycomb Seal Configurations, 10th International Gas Turbine Congress in Japan, IGTC’11 Osaka, Nov. 13-18, 2011.
[8] Liming SONG, Hiroharu Ohyama, Jun LI, Ming ZHANG, Zhenping FENG, Multilevel Design Optimization for Long Blade of Steam Turbine Using Self-adaptive Differential Evolutionary Algorithms, 10th International Gas Turbine Congress in Japan, Nov. 13-18, 2011.


2010年
英文期刊论文
[1] Jun LI, Shengru Kong, Xin YAN, et al, Numerical Investigations on Leakage Performance of the Rotating Labyrinth Honeycomb Seal, ASME Journal of Engineering for Gas Turbine and Power, 2010, 132(6): 062501.
[2] Zhang, Xiongwen, Chan, S. H., Li, Guojun, Ho, H. K., Li, Jun, FEng, Zhenping, A Review of Intergration Strategies for Solid Oxide Fuel Cells, Journal of Power Sources, 2010, 195(3): 685-702.
[3] Xin Yan, Jun Li, Zhenping Feng, Effects of Inlet Preswirl and Cell Diameter and Depth on Honeycomb Seal Characterictics, ASME Journal of Engineering for Gas Turbine and Power, 2010, 132(12): 122506.

中文期刊论文
[1] 孙皓，薛志恒，李军，丰镇平，低雷诺数对透平叶片间隙泄漏流动影响的研究，西安交通大学学报，2010，44(3):11-15,31.
[2] 李志刚，李军，丰镇平，迷宫密封泄漏特性影响因素的研究，西安交通大学学报，2010,44(3): 16-20.
[3] 李军，王金山，蒋勇，丰镇平，凹槽状动叶顶部非定常气膜冷却性能的研究，西安交通大学学报，2010,44(5): 5-9,25.
[4] 李军，刘立军，李国君，丰镇平，空化数对离心泵水力性能影响的数值研究，工程热物理学报，2010,31(5): 773-776.
[5] 李军，孙皓，罗常等，轴流透平机械通流部分泄漏流动及控制技术研究进展，热力透平，2010, 39(2): 83-89.
[6] 陈春新，李军，丰镇平，刷式密封刷丝束与转子接触力的数值研究，西安交通大学学报，2010, 41(7): 23-27.

国际会议论文
[1] J, LI, J.S. WANG, Z.P.FENG, Numerical Investigations on Leakage Flow and Heat Transfer Characteristics of Squealer Tip Under Stator/Rotor Interatcion, Asian Joint Conference on Propulsion and Power 2010, Miyazaki city, 2010, March 4-6, Japan.
[2] LI, J. HUANG, Y., LI, Z. et al., Effects of Clearance on the Leakage Flow Characteristics of Two Kinds of Brush Seals and Referenced Labyrinth Seal, GT2010-2287, Galsgow, UK.
[3] Chang LUO, Liming SONG, Jun LI, Zhenping FENG et al, Numerical Study of Internal Flow Fields in Steam Turbines with Balance Holes, GT2010-23704, Glasgow, UK.
[4] Yan SHI, Jun LI, Zhenping FENG, Influence of Rotor Blade Fillets on Aerodynamic Performance of Turbine Stage, GT2010-23721, Glasgow, UK.
[5] Jun LI, Yong JIANG, Xin YAN, et al., Numerical Investigations on the Aerodynamic Performance of Throttle Governing Stage for Large Power Steam Turbines, Seventh International Conference on Flow Dynamics, Nov., 1-3, Sendai International Center, Sendai, JAPAN.
[6] Jun LI, Zhigang LI, Liming SONG, et al., Effects of Cell Diameter and Depth on the Leakage Flow Characteristcs of Honeycomb Seal, Seventh International Conference on Flow Dynamics, Nov., 1-3, Sendai International Center, Sendai, JAPAN.

国内会议论文
[1] 李志刚，李军，转子轴向偏移对迷宫密封泄漏特性影响的数值研究，中国科技论文在线，2001007-16.
[2] 李志刚，李军，袋型阻尼密封泄漏特性影响因素研究，中国科技论文在线，201007-542.
[3] 阳虹，杨建道，李军等，大功率汽轮机喷嘴配汽调节级全三维气动性能和结构优化设计的研究，2010年透平专委会，上海.
[4] 李军，孙皓，李彬等，高负荷叶片和大焓降级在叶轮机械通流部分设计和优化中应用的研究进展，2010年透平专委会，上海.
[5] 钟刚云，吴其林，李军，大功率汽轮机调节级段气动特性研究，2010年透平专委会，上海.
[6] 黄阳子，李军，丰镇平，低迟滞刷式密封泄漏特性的研究，2010年工程热物理学会热机气动热力学学术会议，No102037，2010年11月8日至10日，南京，中国
[7] 孙皓，薛志恒，李军，丰镇平，攻角对透平叶栅气动性能影响的研究，2010年工程热物理学会热机气动热力学学术会议，No102036，2010年11月8日至10日，南京，中国
[8] 薛志恒，孙皓，李军，丰镇平，动力透平叶栅负攻角下的气动性能研究，2010年工程热物理学会热机气动热力学学术会议，No102035，2010年11月8日至10日，南京，中国


2009年
英文期刊论文
[1] Xin YAN, Jun LI, Liming Song, Zhenping Feng, Investigations on the Discharge and Total Temperature Increase Characteristics of the Labyrinth Seals with Honeycomb and Smooth Lands, ASME Journal of Turbomachinery, 2009, 131(4): 041009.
[2] Li, J., Obi, S., Feng, Z., The effects of clearance sizes on labyrinth brush seal leakage performance using aReynolds-averaged Navier-Stokes solver and non-Darcian porous medium model, Journal of Power and Energy, 2009, 223(8): 953-964.
[3] Xiongwen Zhang, Jun Li, Guojun Li, Zhenping Feng, Numerical study on the thermal characteristics in a tubular solid oxide fuel cell with indirect internal reformer, International Journal of Thermal Science, 2009, 48(4): 805-814.

国内期刊论文
[1] 李军，晏鑫，丰镇平等，透平机械阻尼密封技术及其转子动力特性研究进展，热力透平，2009, 3891):5-9.
[2] 李军，刘立军，李国君，丰镇平，基于汽相/液相界面跟踪方法的弯管内空化流动的数值预测，工程热物理学报，2008,29(12): 2037-2039.
[3] 罗常，宋立明，李军，丰镇平，三维跨音速叶栅自动气动优化设计，工程热物理学报，200929(12): 2019-2021.
[4] 晏鑫，李军，丰镇平，孔型气体密封的转子动力特性研究，动力工程，2009,29(1):31-35.
[5] 晏鑫，李军，丰镇平，BULK FLOW方法分析孔型密封转子动力特性的有效性，西安交通大学学报，2009,4391):24-28.
[6] 晏鑫，李军，丰镇平，预旋对蜂窝密封和迷宫密封内柳丁传热特性影响，航空动力学报，2009, 24(40: 772-776.
[7] 石龑，李少军，邓清华，李军，丰镇平，透平级轴向间隙对非定常流动干涉影响的研究，西安交通大学学报，2009, 43(9): 9-13.
[8] 阳虹，杨建道，李军等，刷式密封技术及其在汽轮机优化设计中的应用，热力透平，2009, 29(8):737-742,764.
[9] 石龑，邓清华，李军，丰镇平，一级半轴流式透平的非定常流动干涉与时序效应，动力工程，2009, 29(2): 111-116.
[10] 宋立明，罗常，李军，丰镇平，透平叶栅自动气动优化设计方法，机械工程学报，2009, 45(9): 109-113.
[11] 晏鑫，蒋玉娥，李军，丰镇平，迷宫密封转子动力特性的数值模拟，热能动力工程， 2009, 24(5): 566-570.

国际会议论文
[1] Hao SUN, Jun LI, Zhenping FENG, Effects of Tip Clearance on Unsteady Flow Characteristics in a Axial Turbine Stage, GT2009-59828, Florida, USA.
[2] Chang LUO, Liming SONG, Jun LI, ZHenping FENG, Multiobjective Optimization Approach to Multidisciplinary Design of a Three-dimensional Transonic Compressor Blade, GT2009-59982, Florida, USA.
[3] Jun LI, Yan ZHANG, Zhenping FENG, Analysis of the Unsteady Aerodynamic Performance with the Shroud Flow of a One and Half Axial Turbine Stage, ISABE-2009-1257, Montreal, Canada.

国内会议论文
[1] 李军，孙皓，罗常等，轴流透平机械通流部分泄漏流动及其控制技术研究进展，2009透平专委会，北京.
[2] 李军，刘立军，李国君，丰镇平，空化数对离心泵水力性能影响的数值研究，中国工程热物理学会热机气动分会，大连.
[3] 王金山，李军，丰镇平，动静干涉对凹槽状叶顶泄漏流动和换热特性影响的研究，中国工程热物理学会热机气动分会，大连.
[4] 罗常，宋立明，李军等，带平衡孔的太平间内部流动的数值研究，中国工程热物理学会热机气动分会，大连.

2006-2008英文期刊论文
[1] X. W. Zhang, S. H. Chan, H. K., Ho, Jun Li, Guojun Li, Zhenping Feng, Nonlinear model predictive control based on the moving horizon state estimation for the solid oxide fuel cell, International Journal of Hydrogen Energy, 2008, 33(9): 2355-2366.
[2] Xiongwen Zhang, Guojun Li, Jun Li, Zhenping Feng, Numerical study on electric characteristics of solid oxide fuel cells, Energy Conversion and Management, 2007, 48(3): 977-989.
[3] Xiongwen Zhang, Jun Li, Guojun Li, Zhenping Feng, Cycle analysis of an integrated solid oxide fuel cell and recuperative gas turbine with an air reheating system, Journal of Power Sources, 2007, 164(2): 752-760.
[4] Xiongwen Zhang, Jun Li, Guojun Li, Zhenping Feng, Dynamic modeling of a hybrid system of the solid oxide fuel cell and recuperative gas turbine, Journal of Power Sources, 2007, 163(1): 523-531.
[5] Jun Li, Lijun Liu, Zhenping Feng, Numerical Prediction of the Hydrodynamic Performance of a Centrifugal Pump in Cavitating Flows, Communications in Numerical Methods in Engineering, 2007, 23(5): 363-384.
[6] Xiongwen Zhang, Jun Li, Guojun Li, Zhenping Feng, Development of a control oriented model for the solid oxide fuel cell, Journal of Power Sources, 2006, 169(1): 258-267.
[7] Xiongwen Zhang, Jun Li, Hui Xu, Guojun Li, Numerical study of self-adaptive vibration suppression for flexible structure using interior inlay viscous fluid unit method, Journal of Sound and Vubration, 2006, 297:627-634.
[8] Liu LJ, Li J, Feng ZP, A Numerical method for simulation of attached cavitation flows, International Journal for Numerical Methods in Fluids, 2006, 52:639-658.
[9] Li J, Liu LJ, Feng ZP, Two-dimensional analysis of cavitaing flows in acentrifugal pump using a single phase RANS solver and cavitation model, Journal of Power and Energy, 2006, 220(7): 783-791.