航空发动机气动热力学

叶轮机械高精度测试

叶轮机械气动弹性

CFD高精度湍流模拟与气动优化

招收航空发动机气动热力学研究、叶轮机械内流高精度测量技术、CFD高精度湍流计算、气动优化方向学生，欢迎有志于航空发动机叶轮机械研究的同学加入。

082502-航空宇航推进理论与工程
080701-工程热物理
080703-动力机械及工程

航空发动机气动热力学与高精度测试技术
叶轮机械气动弹性
CFD高精度湍流计算与气动优化

2007-09--2010-06   加拿大 Carleton 大学   联合培养博士
2005-09--2010-07   西北工业大学   博士
2001-09--2005-07   西北工业大学   学士

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2014-07~现在, 中国科学院工程热物理研究所, 研究员
2012-07~2014-06,加拿大 National Research Council Canada, Research Associate
2010-07~2012-06,加拿大 National Research Council Canada, Research Assistant

吸气式发动机

   

   

[1] Zhang, Jianshe, Li, Lin, Dong, Xu, Zhang, Ziqing, Zhang, Yanfeng, Lu, Xingen. A discrete adjoint framework coupled with adaptive PCE for robust aerodynamic optimization of turbomachinery under flow uncertainty. AEROSPACE SCIENCE AND TECHNOLOGY[J]. 2023, 142: http://dx.doi.org/10.1016/j.ast.2023.108592.
[2] Xiangcan Kong, Yanfeng Zhang, Guoqing Li, Xingen Lu, Junqiang Zhu, Jinliang Xu. Simulation on the effect of impinging distance for the aerodynamic and heat transfer characteristics of sweeping jet and film composite cooling. APPLIED THERMAL ENGINEERING. 2023, 227: http://dx.doi.org/10.1016/j.applthermaleng.2023.120382.
[3] 刘浩, 李国庆, 张深, 李昂, 张燕峰, 卢新根. 机器学习在涡轮机械中的应用进展. 工程热物理学报[J]. 2023, 44(4): 938-950, [4] Wang, Mingyang, Lu, Xingen, Zhao, Shengfeng, Zhang, Yanfeng. Numerical investigations of vortex dynamics and loss generation in the corner separation region of a high subsonic compressor blade. PHYSICS OF FLUIDS[J]. 2023, 35(2): http://dx.doi.org/10.1063/5.0134670.
[5] 康忠, 李国庆, 张深, 王晓东, 张燕峰, 卢新根. 收缩型双射流孔气膜冷却特性与损失机理研究. 航空动力学报[J]. 2023, 38(2): 335-343, [6] Xiangcan Kong, Yanfeng Zhang, Guoqing Li, Xingen Lu, Junqiang Zhu, Jinliang Xu. Effects of Mainstream Velocity and Turbulence Intensity on the Sweeping Jet and Film Composite Cooling. MACHINES[J]. 2023, 11(356): https://doaj.org/article/5587502a56274e63be1f6c67eaeefea6.
[7] Dong, Xu, Zhang, Yanfeng, Lu, Xingen. Fan Flutter Mechanisms Related to Blade Mode Shape and Acoustic Properties. JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME[J]. 2023, 145(9): http://dx.doi.org/10.1115/1.4062806.
[8] 康忠, 李国庆, 张深, 王晓东, 张燕峰, 卢新根. 收缩型双射流孔气膜冷却特性与损失机理. 航空动力学报[J]. 2023, 38(2): 335-343, http://lib.cqvip.com/Qikan/Article/Detail?id=7109405270.
[9] Li, Ming, Lei, Zhijun, Deng, Hanliu, Ouyang, Xiaoqing, Zhang, Yanfeng, Lu, Xingen, Xu, Gang, Zhu, Junqiang. Numerical Research on the Jet-Mixing Mechanism of Convergent Nozzle Excited by a Fluidic Oscillator and an Air Tab. ENERGIES[J]. 2023, 16(3): http://dx.doi.org/10.3390/en16031412.
[10] Zhang, ZiQing, Li, PeiJing, Li, QingKuo, Dong, Xu, Lu, XinGen, Zhang, YanFeng. Dynamic Machine Learning Global Optimization Algorithm and Its Application to Aerodynamics. JOURNAL OF PROPULSION AND POWER[J]. 2023, http://dx.doi.org/10.2514/1.B38782.
[11] Kong Xiangcan, Zhang Yanfeng, Li Guoqing, Lu Xingen, Zeng Jun, Zhu Junqiang, Xu Jinliang. Analysis of sweeping jet and film composite cooling using the decoupled model. OPEN PHYSICS[J]. 2023, 21(1): 500-9, https://doaj.org/article/cba7130caf944b24ab4a333f2470f6ea.
[12] Hang Yuan, Yunfeng Wu, Shiji Zhou, Mingyang Wang, Xingen Lu, Yanfeng Zhang. Nonuniform height endwall fence optimization of a low-pressure turbine cascade. INTERNATIONAL JOURNAL OF MECHANICAL SCIENCES. 2023, 250: http://dx.doi.org/10.1016/j.ijmecsci.2023.108301.
[13] Lin Li, Wei Tan, Jianshe Zhang, Ge Han, Yanfeng Zhang. Unsteady Effects of Wake on Downstream Rotor at Low Reynolds Numbers. ENERGIES[J]. 2022, 15: https://doaj.org/article/11a6b9ae89e24f2aa1d2630f37b87d58.
[14] Zhang Yingjie, Lu Xingen, Zhang Yanfeng, Zhang Ziqing, Dong Xu, Han Ge. Stall Behavior in an Ultra-High Pressure Ratio Centrifugal Compressor: Backward Traveling Rotating Stall. JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME[J]. 2022, [15] Dong Xu, Zhang Yanfeng, Lu Xingen, Zhang, Yingjie, Gan Jiuliang. Numerical Investigation of the Fan Flutter Mechanism Related to Acoustic Propagation Characteristics. JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME[J]. 2022, [16] Li Guoqing, Zhang Shen, Kang Zhong, Zhang Yanfeng, Lu Xingen, Zhu Junqiang. Leakage and wear characteristics of carbon seals for aero-engines. Chinese Journal of Aeronautics[J]. 2022, 35(22): 389-400, [17] Xiangcan Kong, Yanfeng Zhang, Guoqing Li, Xingen Lu, Junqiang Zhu. Simulation of Flow Structure and Heat Transfer of Sweeping Jet and Film Composite Cooling on a Flat Plate. Applied Thermal Engineering[J]. 2022, 213: 118741-, [18] Mingyang Wang, Xingen Lu, Yang Chengwu, Shengfeng Zhao, Yanfeng Zhang. Control of separated flow transition over a highly loaded compressor blade via dynamic surface deformation. International Journal of Mechanical Sciences[J]. 2022, 241(2023): [19] Xiangcan Kong, Yanfeng Zhang, Guoqing Li, Xingen Lu, Junqiang Zhu, Jinliang Xu. Heat transfer and flow structure characteristics of film-cooled leading edge model with sweeping and normal jets. INTERNATIONAL COMMUNICATIONS IN HEAT AND MASS TRANSFER[J]. 2022, 138: http://dx.doi.org/10.1016/j.icheatmasstransfer.2022.106338.
[20] Ziqing Zhang, Yanfeng Zhang, Yingjie Zhang, Xu Dong, Xingen Lu. Numerical investigation of the purge flow mechanisms and heat-transfer characteristics of turbine rim seals. CASE STUDIES IN THERMAL ENGINEERING[J]. 2022, 40: 102484-, http://dx.doi.org/10.1016/j.csite.2022.102484.
[21] Xiangcan Kong, Yanfeng Zhang, Guoqing LI, Xingen Lu, Junqiang Zhu. Numerical Simulation of the Flow and Heat Transfer Characteristics of Sweeping and Direct Jets on a Flat Plate with Film Holes. Energies[J]. 2022, 15(12): 4470-, [22] 康忠, 李国庆, 张深, 王晓东, 张燕峰, 卢新根. 主流马赫数对气膜冷却效果与掺混损失的影响. 工程热物理学报[J]. 2022, [23] Hang Yuan, Mingyang Wang, Jianshe Zhang, Yanfeng Zhang, Xingen Lu. Integrated optimization of a high-lift low-pressure turbine cascade based on dynamic support vector regression. Aerospace Science and Technology[J]. 2022, 131(3): [24] Li, Qingkuo, Zhang, Yingjie, Wang, Yi, Han, Ge, Zhang, Yanfeng, Lu, Xingen. Numerical investigation of the diffuser throat length effect on a transonic centrifugal compressor. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART C-JOURNAL OF MECHANICAL ENGINEERING SCIENCE[J]. 2022, 236(7): 3790-3803, http://dx.doi.org/10.1177/09544062211040101.
[25] 张英杰, 韩戈, 李庆阔, 张子卿, 张燕峰, 卢新根. 超高压比离心压气机失速机理探究. 工程热物理学报[J]. 2022, 43(2): 309-315, http://lib.cqvip.com/Qikan/Article/Detail?id=7106701991.
[26] Wang, Mingyang, LI, Ziliang, Han, Ge, Yang, Chengwu, Zhao, Shengfeng, Zhang, Yanfeng, Lu, Xingen. Vortex dynamics and entropy generation in separated transitional flow over a compressor blade at various incidence angles. CHINESE JOURNAL OF AERONAUTICS[J]. 2022, 35(3): 42-52, http://dx.doi.org/10.1016/j.cja.2021.06.021.
[27] Lei, Zhijun, Liu, Hongrui, Li, Gang, Gong, Jianbo, Zhang, Yanfeng, Lu, Xingen, Xu, Gang, Zhu, Junqiang. Influence of Wake Intensity on the Unsteady Flow Characteristics of the Integrated Aggressive Interturbine Duct. APPLIED SCIENCES-BASEL[J]. 2022, 12(13): [28] 张子卿, 宋宇宽, 王名扬, 卢新根, 张燕峰. 基于动态XGBoost与MaxLIPO置信域算法的减重涡轮叶型气动优化设计. 工程热物理学报[J]. 2021, 42(11): 2804-2815, http://lib.cqvip.com/Qikan/Article/Detail?id=7106094214.
[29] 孔祥灿, 张子卿, 朱俊强, 徐进良, 张燕峰. 航空发动机气冷涡轮叶片冷却结构研究进展. 推进技术[J]. 2021, https://t.cnki.net/kcms/detail?v=3uoqIhG8C46NmWw7YpEsKHTPvOGrUOOqX1coEOzL8AFGAh45mbT7GzVCphcXXgmXteDdVIcVSnI-k5BQNTI9QB0oOlrObIVN.
[30] 李霖, 张燕峰, 韩戈, 李子良, 谭炜. 低雷诺数下周期性尾迹与压气机叶尖泄漏 涡的作用机理研究. 2021年热机气动热力学和流体机械学术会议年会[J]. 2021, [31] Li Lin, Zhang Yanfeng, Han Ge. The Effect of IGV Wake on Axial Compressor Rotor at Low Reynolds Numbers. Proceedings of Global Power and Propulsion Society[J]. 2021, [32] Qu, Xiao, Zhang, Yingjie, Lu, Xingen, Zhu, Junqiang, Zhang, Yanfeng. Unsteady fluidic oscillators for active controlling boundary layer separation in an ultra-high-lift low-pressure turbine. AEROSPACE SCIENCE AND TECHNOLOGY[J]. 2021, 119: http://dx.doi.org/10.1016/j.ast.2021.107130.
[33] 李庆阔, 张子卿, 张英杰, 韩戈, 张燕峰, 卢新根. 基于机器学习XGBoost算法的跨音速离心压气机扩压器气动优化设计. 工程热物理学报[J]. 2021, 42(8): 1970-1978, http://lib.cqvip.com/Qikan/Article/Detail?id=7105402277.
[34] 董旭, 张燕峰, 张英杰, 张子卿, 卢新根. 宽弦高速跨音风扇颤振特性研究. 工程热物理学报[J]. 2021, 42(1): 56-63, http://lib.cqvip.com/Qikan/Article/Detail?id=7103788809.
[35] 孔祥灿, 张子卿, 李国庆, 朱俊强, 徐进良, 张燕峰. 扫掠冲击-气膜冷却结构的气动传热特性数值研究. 推进技术[J]. 2021, [36] Tan Wei, Li Lin, Qu, Xiao, Zhang, Ziqing, Zhang Yanfeng. Investigation of staggered labyrinth tip shroud on flow mechanism of low-pressure turbine. Proceedings of Global Power and Propulsion Society[J]. 2021, [37] 谭炜, 张子卿, 屈骁, 张英杰, 卢新根, 张燕峰. 跨音速涡轮定常与非定常叶尖泄漏流机理分析. 风机技术[J]. 2021, 1-11, [38] Xiangcan Kong, Ziqing Zhang, Guoqing Li, Yanfeng Zhang. NUMERICAL SIMULATION ON INTERNAL FLOW AND HEAT TRANSFER OF SWEEPING JET AND FILM COMPOSITE COOLING ON A FLAT PLATE. GPPSnull. 2021, [39] Han, Ge, Yang, Chengwu, Zhao, Shengfeng, Zhang, Yanfeng, Lu, Xingen. Investigation of a High Pressure Ratio Centrifugal Compressor with Wedge Diffuser and Pipe Diffuser. INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES[J]. 2021, 38(1): 1-13, https://www.webofscience.com/wos/woscc/full-record/WOS:000621716800001.
[40] Wang, Mingyang, Lu, Xingen, Yang, Chengwu, Zhao, Shengfeng, Zhang, Yanfeng. Numerical investigation of distributed roughness effects on separated flow transition over a highly loaded compressor blade. PHYSICS OF FLUIDS[J]. 2021, 33(11): [41] Wang, Mingyang, Yang, Chengwu, Li, Ziliang, Zhao, Shengfeng, Zhang, Yanfeng, Lu, Xingen. Effects of surface roughness on the aerodynamic performance of a high subsonic compressor airfoil at low Reynolds number. CHINESE JOURNAL OF AERONAUTICS[J]. 2021, 34(3): 71-81, http://dx.doi.org/10.1016/j.cja.2020.08.020.
[42] Wang, Mingyang, Lu, Xingen, Zhu, Junqiang, Han, Ge, Yang, Chengwu, Zhao, Shengfeng, Zhang, Yangfeng. Wall Cooling Effect on Separated Flow Transition over a Highly Loaded Compressor Blade. INTERNATIONAL JOURNAL OF MECHANICAL SCIENCES[J]. 2021, 209: http://dx.doi.org/10.1016/j.ijmecsci.2021.106709.
[43] Wang, Mingyang, Li, Ziliang, Yang, Chengwu, Zhao, Shengfeng, Zhang, Yanfeng, Lu, Xingen. Large eddy simulation of the separated flow transition on the suction surface of a high subsonic compressor airfoil. PHYSICS OF FLUIDS[J]. 2020, 32(3): https://www.webofscience.com/wos/woscc/full-record/WOS:000522041100001.
[44] Li, Ziliang, Lu, Xingen, Han, Ge, Zhang, Yanfeng, Zhao, Shengfeng, Zhu, Junqiang. The performance of a centrifugal compressor with a tandem impeller in off-design conditions. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY[J]. 2020, 234(2): 156-172, https://www.webofscience.com/wos/woscc/full-record/WOS:000503649300003.
[45] 王名扬, 赵胜丰, 李紫良, 卢新根, 张燕峰, 朱俊强. 低雷诺数下高亚声速压气机叶型流动损失机理研究. 推进技术[J]. 2020, 41(5): 1046-1054, https://kns.cnki.net/KCMS/detail/detail.aspx?dbcode=CJFQ&dbname=CJFDLAST2020&filename=TJJS202005011&v=MDI4ODhITkhNcW85RVpZUjhlWDFMdXhZUzdEaDFUM3FUcldNMUZyQ1VSN3FlWitSdkZpcmtWci9LTVNmQmZiRzQ=.
[46] Dong, Xu, Zhang, Ziqing, Zhang, Yingjie, Zhang, Yanfeng, Lu, Xingen. High-frequency unsteady flow near the tip in a transonic fan rotor with a small clearance. AEROSPACE SCIENCE AND TECHNOLOGY[J]. 2020, 106: http://dx.doi.org/10.1016/j.ast.2020.106211.
[47] 董旭, 张燕峰, 卢新根, 甘久亮, 朱俊强. 叶轮机械颤振研究进展. 推进技术[J]. 2020, 42(1): 53-67, http://lib.cqvip.com/Qikan/Article/Detail?id=7104247002.
[48] 张英杰, 韩戈, 李紫良, 阳诚武, 张燕峰, 卢新根. 高负荷离心压气机扩压器叶片前缘开槽流动机理研究. 推进技术[J]. 2020, 41(3): 559-565, https://kns.cnki.net/KCMS/detail/detail.aspx?dbcode=CJFQ&dbname=CJFDLAST2020&filename=TJJS202003010&v=MTMzNDZZUzdEaDFUM3FUcldNMUZyQ1VSN3FlWitkcEZpbmxWcjNKTVNmQmZiRzRITkhNckk5RVpJUjhlWDFMdXg=.
[49] Qu, Xiao, Zhang, Yanfeng, Lu, Xingen, Zhu, Junqiang. Unsteady experimental and numerical investigation of aerodynamic performance in ultra-high-lift LPT. CHINESE JOURNAL OF AERONAUTICS[J]. 2020, 33(5): 1421-1432, http://lib.cqvip.com/Qikan/Article/Detail?id=7102484274.
[50] Qu, Xiao, Zhang, Yanfeng, Liy, Xingen, Zhu, Junqiang. Unsteady wakes -secondary flow interactions in a high-lift low-pressure turbine cascade. CHINESE JOURNAL OF AERONAUTICS[J]. 2020, 33(3): 879-892, http://lib.cqvip.com/Qikan/Article/Detail?id=7101817731.
[51] Zhang, Ziqing, Zhang, Yingjie, Dong, Xu, Qu, Xiao, Lu, Xingen, Zhang, Yanfeng. Flow mechanism between purge flow and mainstream in different turbine rim seal configurations. CHINESE JOURNAL OF AERONAUTICS[J]. 2020, 33(8): 2162-2175, http://lib.cqvip.com/Qikan/Article/Detail?id=7102998811.
[52] 王名扬, 李紫良, 卢新根, 赵胜丰, 张燕峰, 朱俊强. 低雷诺数下粗糙度对高亚声速压气机叶型气动性能的影响. 推进技术[J]. 2020, 41(7): 1510-1519, http://lib.cqvip.com/Qikan/Article/Detail?id=7102494020.
[53] Dong, Xu, Zhang, Yingjie, Zhang, Ziqing, Lu, Xingen, Zhang, Yanfeng. Effect of Tip Clearance on the Aeroelastic Stability of a Wide-Chord Fan Rotor. JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME[J]. 2020, 142(9): http://dx.doi.org/10.1115/1.4048020.
[54] Wang, MingYang, Li, ZiLiang, Zhao, ShengFeng, Zhang, YanFeng, Lu, XinGen. Effects of Reynolds number and loading distribution on the aerodynamic performance of a high subsonic compressor airfoil. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY[J]. 2020, 234(8): 1069-1083, https://www.webofscience.com/wos/woscc/full-record/WOS:000507196500001.
[55] 张英杰, 韩戈, 李紫良, 张燕峰, 卢新根. 扩压器叶片前缘开槽结构对高负荷离心压气机性能影响研究. 工程热物理学报[J]. 2020, 41(7): 1617-1626, http://lib.cqvip.com/Qikan/Article/Detail?id=7102364348.
[56] Zhang, Yingjie, Zhang, Ziqing, Dong, Xu, Han, Ge, Zhang, Yanfeng, Lu, Xingen. Effects of unsteady interaction on the performance of an ultra-high-pressure-ratio centrifugal compressor. AEROSPACE SCIENCE AND TECHNOLOGY[J]. 2020, 105: http://dx.doi.org/10.1016/j.ast.2020.106036.
[57] Dong, Xu, Zhang, Yanfeng, Zhang, Yingjie, Zhang, Ziqing, Lu, Xingen. Numerical simulations of flutter mechanism for high-speed wide-chord transonic fan. AEROSPACE SCIENCE AND TECHNOLOGY[J]. 2020, 105: http://dx.doi.org/10.1016/j.ast.2020.106009.
[58] Qu, Xiao, Zhang, Yingjie, Lu, Xingen, Zhu, Junqiang, Zhang, Yanfeng. Unsteady influences of blade loading distribution on secondary flow of ultra-high-lift LPT. AEROSPACE SCIENCE AND TECHNOLOGY[J]. 2020, 96: http://dx.doi.org/10.1016/j.ast.2019.105550.
[59] Qu, Xiao, Zhang, Yanfeng, Lu, Xingen, Zhu, Junqiang. Unsteady effects of periodic wake passing frequency on aerodynamic performance of ultra-high-lift low pressure turbine cascades. PHYSICS OF FLUIDS[J]. 2019, 31(9): https://www.webofscience.com/wos/woscc/full-record/WOS:000489883500011.
[60] 屈骁, 张燕峰, 卢新根, 朱俊强. 上游尾迹对高负荷低压涡轮非定常气动性能的影响. 工程热物理学报[J]. 2019, 40(9): 2004-2011, http://lib.cqvip.com/Qikan/Article/Detail?id=7002878029.
[61] 张英杰, 韩戈, 董旭, 赵胜丰, 张燕峰, 卢新根. 高负荷离心压气机扩压器叶片前缘开槽参数化研究. 西安交通大学学报[J]. 2019, 53(9): 34-41, http://lib.cqvip.com/Qikan/Article/Detail?id=7002780308.
[62] Qu, Xiao, Zhang, Yanfeng, Lu, Xingen, Lei, Zhijun, Zhu, Junqiang. The effect of endwall boundary layer and incoming wakes on secondary flow in a high-lift low-pressure turbine cascade at low Reynolds number. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING[J]. 2019, 233(15): 5637-5649, https://www.webofscience.com/wos/woscc/full-record/WOS:000490896900012.
[63] Qu, Xiao, Zhang, Yanfeng, Lu, Xingen, Lei, Zhijun, Zhu, Junqiang. Effect of periodic wakes and a contoured endwall on secondary flow in a high-lift low-pressure turbine cascade at low Reynolds numbers. COMPUTERS & FLUIDS[J]. 2019, 190: 1-14, http://dx.doi.org/10.1016/j.compfluid.2019.05.016.
[64] Zhang, Yingjie, Lu, Xingen, Zhang, Yanfeng, Han, Ge, Zhu, Junqiang. Parametric study of slotted diffuser effects on a highly loaded centrifugal compressor. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY[J]. 2019, 233(6): 702-714, https://www.webofscience.com/wos/woscc/full-record/WOS:000483844500003.
[65] Zhang Yingjie, Dong Xu, Zhang Yanfeng, Lu Xingen. Flow control of hub corner stall in a highly loaded axial compressor cascade. INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW[J]. 2019, 78: 108434-, http://dx.doi.org/10.1016/j.ijheatfluidflow.2019.108434.
[66] Qu, Xiao, Zhang, Yanfeng, Lu, Xingen, Han, Ge, Li, Ziliang, Zhu, Junqiang. Effects of periodic wakes on the endwall secondary flow in high-lift low-pressure turbine cascades at low Reynolds numbers. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING[J]. 2019, 233(1): 354-368, https://www.webofscience.com/wos/woscc/full-record/WOS:000454948300026.
[67] Li, Ziliang, Lu, Xingen, Zhao, Shengfeng, Han, Ge, Yang, Chengwu, Zhang, Yanfeng. Numerical investigation of flow mechanisms of tandem impeller inside a centrifugal compressor. CHINESE JOURNAL OF AERONAUTICS[J]. 2019, 32(12): 2627-2640, http://lib.cqvip.com/Qikan/Article/Detail?id=7100901994.
[68] Zhang, Yingjie, Zhang, Yanfeng, Lu, Xingen, Han, Ge, li, Ziliang. Effects of a slotted diffuser on the aerodynamic performance of a highly loaded centrifugal compressor. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART C-JOURNAL OF MECHANICAL ENGINEERING SCIENCE[J]. 2019, 233(19-20): 6879-6891, [69] Yang Chengwu, Han Ge, Zhao Shengfeng, Lu Xingen, Zhang Yanfeng, Li Ziliang, ASME. DESIGN AND TEST OF A NOVEL HIGHLY-LOADED COMPRESSOR. PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2019, VOL 2Anull. 2019, http://apps.webofknowledge.com/CitedFullRecord.do?product=UA&colName=WOS&SID=5CCFccWmJJRAuMzNPjj&search_mode=CitedFullRecord&isickref=WOS:000501627800024.
[70] Xiao Qu, Yanfeng Zhang, Xingen Lu, Zhijun Lei, Junqiang Zhu. Effect of periodic wakes and a contoured endwall on secondary flow in a high-lift low-pressure turbine cascade at low Reynolds numbers. COMPUTERS AND FLUIDS. 2019, 1-14, http://dx.doi.org/10.1016/j.compfluid.2019.05.016.
[71] 陶文灿, 张子卿, 宋宇宽, 李紫良, 张燕峰. 高压涡轮封严流与主流相互作用的机理研究. 推进技术[J]. 2019, 40(11): 2473-2481, http://lib.cqvip.com/Qikan/Article/Detail?id=7100390632.
[72] 柴猛, 雷志军, 张燕峰, 卢新根, 朱俊强. 新型消旋波瓣混合器射流掺混机理研究. 推进技术[J]. 2018, 39(9): 1965-1973, http://lib.cqvip.com/Qikan/Article/Detail?id=676337340.
[73] Li, Ziliang, Lu, Xingen, Zhang, Yanfeng, Han, Ge, Yang, Chengwu, Zhao, Shengfeng. Numerical investigation of a highly loaded centrifugal compressor stage with a tandem bladed impeller. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY[J]. 2018, 232(3): 240-253, https://www.webofscience.com/wos/woscc/full-record/WOS:000435491500003.
[74] Zhang, Yanfeng, Hu, Shuzhen, Mahallati, Ali, Zhang, XueFeng, Vlasic, Edward. Effects of Area Ratio and Mean Rise Angle on the Aerodynamics of Interturbine Ducts. JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME[J]. 2018, 140(9): https://www.webofscience.com/wos/woscc/full-record/WOS:000447191900006.
[75] Han, Ge, Lu, Xingen, Zhang, Yanfeng, Zhao, Shengfeng, Yang, Chengwu, Zhu, Junqiang. Investigation of two pipe diffuser configurations for a compact centrifugal compressor. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING[J]. 2018, 232(4): 716-728, https://www.webofscience.com/wos/woscc/full-record/WOS:000429915700008.
[76] 王晏根, 韩建涛, 张燕峰. 超紧凑涡轮过渡段数值模拟研究. 科学技术与工程[J]. 2017, 17(15): 143-149, http://lib.cqvip.com/Qikan/Article/Detail?id=672231924.
[77] 张燕峰, 王晏根, 卢新根, 韩戈, 朱俊强. 几何参数对紧凑涡轮过渡段内部流动机理影响研究. 工程热物理学报[J]. 2017, 38(7): 1539-1548, [78] 李紫良, 卢新根, 张燕峰, 韩戈, 韩建涛, 朱俊强. 高压比离心压气机串列叶轮内部流动机理研究. 推进技术[J]. 2017, 38(10): 2393-2400, http://lib.cqvip.com/Qikan/Article/Detail?id=674625286.
[79] Sun Shuang, Lei Zhijun, Lu Xingen, Zhang Yanfeng, Zhu Junqiang. The Combined Effects of Surface Roughness with Upstream Wakes on the Boundary Layer Development of an Ultra-High-Lift LPT Blade. INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES[J]. 2017, 34(1): 63-73, https://www.webofscience.com/wos/woscc/full-record/WOS:000395854800008.
[80] 朱俊强, 屈骁, 张燕峰, 卢新根, 李伟. 高负荷低压涡轮内部非定常流动机理及其控制策略研究进展. 推进技术[J]. 2017, 38(10): 2186-2199, http://lib.cqvip.com/Qikan/Article/Detail?id=674625263.
[81] Lu, Xingen, Zhang, Yanfeng, Li, Wei, Hu, Shuzhen, Zhu, Junqiang. Effects of periodic wakes on boundary layer development on an ultra-high-lift low pressure turbine airfoil. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY[J]. 2017, 231(1): 25-38, https://www.webofscience.com/wos/woscc/full-record/WOS:000394966800003.
[82] Zhijun Lei Jianbo Gong Yanfeng Zhang Shangmei Su and Chunyan Hu. Numerical Research on the Mixing Mechanism of Lobed Mixer With New De-Swirling Structure. 2016, http://ir.etp.ac.cn/handle/311046/115765.
[83] Ge Han Xingen Lu Yanfeng Zhang Shengfeng Zhao Chengwu Yang and Junqiang Zhu. Study of Geometric Parameter Influence on Fishtail Pipe Diffuser Performance. 2016, http://ir.etp.ac.cn/handle/311046/115804.
[84] Lei, Zhijun, Zhang, Yanfeng, Zhu, Zihao, Zhu, Junqiang. Numerical research on the mixing mechanism of lobed mixer with inlet swirl in linear radial distribution. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY[J]. 2015, 229(3): 280-297, http://ir.etp.ac.cn/handle/311046/98949.
[85] Chengwu Yang, Xingen Lu, Shengfeng Zhao, Yanfeng Zhang, Junqiang Zhu. Numerical Investigation of a Cantilevered Compressor Stator at Varying Clearance Sizes. ASMEnull. 2015, http://ir.etp.ac.cn/handle/311046/111275.
[86] Ge Han, Xingen Lu, Yanfeng Zhang, Shengfeng Zhao, Junqiang Zhu. Study of a Highly Loaded Centrifugal Compressor With Pipe Diffuser at Design and Off-Design Operating Conditions. ASMEnull. 2015, http://ir.etp.ac.cn/handle/311046/111957.
[87] Zhang, Yanfeng, Lu, Xingen, Lei, Zhijun, Han, Ge, Zhu, Junqiang, Hu, Shuzhen. Parametric studying of low-profile vortex generators flow control in an aggressive inter-turbine duct. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY[J]. 2015, 229(8): 849-861, http://ir.etp.ac.cn/handle/311046/112309.
[88] Effects of Area Ratio and Mean Rise Angle on the Aerodynamics of Inter-Turbine Ducts. ASMEnull. 2014, http://ir.etp.ac.cn/handle/311046/96349.
[89] Experimental and Numerical Investigation of Corner Stall in a Highly-Loaded Compressor Cascade. ASMEnull. 2014, http://ir.etp.ac.cn/handle/311046/96105.
[90] Ali Mahallati, Edward Vlasic, Xue Feng Zhang, Yanfeng Zhang. Aerodynamic Design of Low Aspect Ratio Structural Airfoils within an Inter-Turbine Duct. ISABEnull. 2013, http://ir.etp.ac.cn/handle/311046/88811.
[91] 张燕峰. Aerodynamic Design of Low Aspect Ratio Structual Airfoils within an Inter-Turbine Duct. ISABE paper，2013-1149. 2013, [92] Yanfeng Zhang, Shuzhen Hu, Xue Feng Zhang, Michael Benner, Edward Vlasic. Flow Control in an Aggressive Inter-Turbine Duct Using Low Profile Vortex Generators. ASMEnull. 2012, http://ir.etp.ac.cn/handle/311046/46573.
[93] 张燕峰. Effects of Inlet Flow Conditions on the S-shape Inter-Turbine Duct. ISABE paper，2011-1711. 2011, [94] 张燕峰. Influnence of Inlet Swirl Distributions on an Inter-Turbine Duct-Part I: Casing Swirl Variation. ASME Paper, GT2011-45554. 2011, [95] Yanfeng Zhang, Shuzhen Hu, Xue Feng Zhang, Edward Vlasic. Influences of Inlet Swirl Distributions on an Inter-Turbine Duct: Part II—Hub Swirl Variation. ASMEnull. 2011, http://ir.etp.ac.cn/handle/311046/39616.
[96] Shuzhen Hu, Edward Vlasic, Xue Feng Zhang, Yanfeng Zhang. Effects of Inlet Flow Conditions on S-shaped Inter-Turbine Duct Performance. ISABEnull. 2011, http://ir.etp.ac.cn/handle/311046/82125.
[97] 张燕峰. Influnence of Inlet Swirl Distributions on an Inter-Turbine Duct- Part I I: Hub Swirl Variation. ASME Paper, GT2011-45555. 2011, [98] 胡书珍, 张燕峰, 卢新根, 张宏武, 朱俊强. 跨声速轴流压气机间隙泄漏流触发旋转失速. 推进技术[J]. 2010, 47-51, http://lib.cqvip.com/Qikan/Article/Detail?id=33313874.
[99] 张燕峰, 楚武利, 卢新根. 进口总压畸变对亚声速轴流压气机流场影响数值研究. 西北工业大学学报[J]. 2009, 12-17, http://lib.cqvip.com/Qikan/Article/Detail?id=1000626661.
[100] 吴艳辉, 楚武利, 张皓光, 张燕峰. 间隙流动特征对压气机转子失速起始的影响. 工程热物理学报[J]. 2008, http://lib.cqvip.com/Qikan/Article/Detail?id=1000251993.
[101] 张燕峰, 楚武利, 卢新根. 跨声速轴流压气机近失速状态的间隙泄漏流流动特性. 航空动力学报[J]. 2008, 23(7): 1293-1298, http://lib.cqvip.com/Qikan/Article/Detail?id=27696821.
[102] 张燕峰, 楚武利, 吴艳辉. 跨音速轴流压气机间隙泄漏流流动特性研究. 热能动力工程[J]. 2008, 23(5): 473-477, http://lib.cqvip.com/Qikan/Article/Detail?id=28278910.
[103] 吴艳辉, 楚武利, 张燕峰. 间隙大小对压气机转子间隙泄漏流场的影响. 西北工业大学学报[J]. 2007, 25(6): 838-842, http://lib.cqvip.com/Qikan/Article/Detail?id=26358837.
[104] 卢新根, 楚武利, 张燕峰. 跨音速压气机间隙流与处理机匣相互作用分析. 西安交通大学学报[J]. 2006, 40(11): 1357-1360,1364, http://sciencechina.cn/gw.jsp?action=detail.jsp&internal_id=2608500&detailType=1.
[105] Xiao QU, Liunan LI, Yingjie ZHANG, Xingen LU, Junqiang ZHU, Yanfeng ZHANG. Controlling secondary flow in high-lift low-pressure turbine using boundary-layer slot suction. CHINESE JOURNAL OF AERONAUTICS. http://dx.doi.org/10.1016/j.cja.2023.10.008.

   

已指导学生

王晏根  硕士研究生  080701-工程热物理  

韩建涛  硕士研究生  080701-工程热物理  

柴猛  硕士研究生  080703-动力机械及工程  

陶文灿  硕士研究生  080701-工程热物理  

董旭  博士研究生  080703-动力机械及工程  

屈骁  博士研究生  080701-工程热物理  

现指导学生

张子卿  博士研究生  080703-动力机械及工程  

谭炜  博士研究生  080703-动力机械及工程  

李霖  博士研究生  080701-工程热物理  

张建设  博士研究生  080703-动力机械及工程  

陈才艳  硕士研究生  085800-能源动力