基本信息
朱俊强 男 博导 中国科学院工程热物理研究所
电子邮件： zhujq@mail.etp.ac.cn
通信地址： 北京市北四环西路11号
邮政编码： 100190
电子邮件： zhujq@mail.etp.ac.cn
通信地址： 北京市北四环西路11号
邮政编码： 100190
招生信息
招生专业
080703-动力机械及工程080704-流体机械及工程
招生方向
航空发动机内流气动热力学
教育背景
1987-09--1990-06 西北工业大学 博士1984-09--1987-06 西北工业大学 硕士1980-09--1984-06 西北工业大学 学士
工作经历
工作简历
2004-07~现在, 中国科学院工程热物理研究所, 研究员2001-07~2004-06,加拿大Carleton大学 机械与航空工程学院, 高级访问学者1997-07~2001-06,西北工业大学 航空发动机系, 教授1994-07~1997-06,西北工业大学 航空发动机系, 副教授1990-07~1994-06,西北工业大学 航空发动机系, 讲师
专利与奖励
出版信息
发表论文
[1] 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, [2] 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-, [3] 程泓智, 王名扬, 周创鑫, 赵胜丰, 卢新根, 朱俊强. 低雷诺数下高负荷轴流压气机表面粗糙度流动调控机制. 航空动力学报[J]. 2022, 37(2): 283-295, http://lib.cqvip.com/Qikan/Article/Detail?id=7107154467.[4] Ziliang Li, Xingen Lu, Ge Han, Junqiang Zhu. Investigation on flow mechanism of an advanced transonic centrifugal compressor with free-form impeller at design and off-design speeds. Engineering Applications of Computational Fluid Mechanics[J]. 2022, 16(1): https://doaj.org/article/401f8f619fd7495abbb6cf95d1d31e0b.[5] 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-, [6] Lu Xingen, Cheng Hongzhi, Zhao Shengfeng, Huang Song, Zhu Junqiang. Effect of tip clearance variation in the transonic axial compressor of a miniature gas turbine at different Reynolds numbers. Aerospace Science and Technology[J]. 2022, 128: http://dx.doi.org/10.1016/j.ast.2022.107793.[7] Li Ziliang, Li Qingkuo, Han Ge, Lu Xingen, Zhu Junqiang. The flow mechanism of the shock structure and secondary flow control in transonic centrifugal compressors with leading edge sweep. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART C-JOURNAL OF MECHANICAL ENGINEERING SCIENCE[J]. 2022, 236(14): 7717-7731, http://dx.doi.org/10.1177/09544062221081347.[8] Zhao, Qianpeng, Liu, Fuqiang, Wang, Shaolin, Yang, Jinhu, Liu, Cunxi, Mu, Yong, Xu, Gang, Zhu, Junqiang. Experimental investigation on spark ignition of multi-swirl spray flames under sub-atmospheric pressures and low temperatures. FUEL[J]. 2022, 326: http://dx.doi.org/10.1016/j.fuel.2022.125004.[9] 李子良, 韩戈, 朱俊强, 卢新根. 掠型设计调控跨声速离心压气机内部流动机理. 航空动力学报[J]. 2022, 37(4): 826-835, http://lib.cqvip.com/Qikan/Article/Detail?id=7107261529.[10] 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.[11] Zhou, Chuangxin, Li, Ziliang, Huang, Song, Han, Ge, Lu, Xingen, Zhao, Shengfeng, Zhu, Junqiang. Numerical investigation on the aerodynamic performance and flow mechanism of a fan with a partial-height booster rotor. AEROSPACE SCIENCE AND TECHNOLOGY[J]. 2021, 109: http://dx.doi.org/10.1016/j.ast.2020.106411.[12] Sun Qi, Wang Huishe, Zhu Junqiang, Ji Chunjun, Li Chunyang, Yao Ka. Influence of Tip Clearance on Centrifugal Compressor IGV Regulation and Improvement. JOURNAL OF THERMAL SCIENCE[J]. 2021, 30(3): 1025-1033, http://dx.doi.org/10.1007/s11630-020-1343-x.[13] 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, [14] Xiao, Xiangtao, Wang, Pei, Du, Qiang, Xu, Qingzong, Liu, Jun, Zhu, Junqiang. Numerical Investigations of Film Cooling Characteristics of Interrupted Slot and Trench Holes on a Vane Endwall. JOURNAL OF THERMAL SCIENCE[J]. 2021, 30(3): 1010-1024, http://dx.doi.org/10.1007/s11630-021-1468-6.[15] 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.[16] 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.[17] Wang, Ruonan, Du, Qiang, Liu, Guang, Lian, Zengyan, Xie, Lei, Zhu, Junqiang. Influence of Secondary Sealing Flow on Performance of Turbine Axial Rim Seals. JOURNAL OF THERMAL SCIENCE[J]. 2020, 29(3): 840-851, http://lib.cqvip.com/Qikan/Article/Detail?id=7101852809.[18] Li, Gang, Jiang, Xi, Jiang, Lei, Lei, Zhijun, Zhu, Junqiang, Mu, Yong, Xu, Gang. Design and experimental evaluation of a plasma swirler with helical shaped actuators. SENSORS AND ACTUATORS A-PHYSICAL[J]. 2020, 315: http://dx.doi.org/10.1016/j.sna.2020.112250.[19] 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.[20] Li, Ziliang, Lu, Xingen, Han, Ge, Huang, Enliang, Yang, Chengwu, Zhu, Junqiang. Numerical and experimental investigation of flow mechanism and application of tandem-impeller for centrifugal compressor. AEROSPACE SCIENCE AND TECHNOLOGY[J]. 2020, 100: http://dx.doi.org/10.1016/j.ast.2020.105819.[21] 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.[22] 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.[23] 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.[24] Li, Ziliang, Zhao, Shengfeng, Lu, Xingen, Han, Ge, Yang, Chengwu, Zhu, Junqiang. Inducer/Exducer Matching Characteristics inside Tandem Impellers of a Highly Loaded Centrifugal Compressor. JOURNAL OF THERMAL SCIENCE[J]. 2020, 29(4): 928-944, http://lib.cqvip.com/Qikan/Article/Detail?id=7102368066.[25] Fu, Jinglun, Cao, Ying, Zhang, Chao, Zhu, Junqiang. Investigation of the Conjugate Heat Transfer and Flow Field for a Flat Plate with Combined Film and Impingement Cooling. JOURNAL OF THERMAL SCIENCE[J]. 2020, 29(4): 955-971, http://lib.cqvip.com/Qikan/Article/Detail?id=7102368068.[26] 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.[27] 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.[28] 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.[29] 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.[30] 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.[31] 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.[32] 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.[33] Li, Gang, Jiang, Xi, Zhu, Junqiang, Yang, Jinhu, Liu, Cunxi, Mu, Yong, Xu, Gang. Combustion control using a lobed swirl injector and a plasma swirler. APPLIED THERMAL ENGINEERING[J]. 2019, 152: 92-102, http://dx.doi.org/10.1016/j.applthermaleng.2019.02.042.[34] 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.[35] 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.[36] WANG Yi, BAN Ge, LU Xingen, ZHU Junqiang. The Influence of Wedge Diffuser Blade Number and Divergence Angle on the Performance of a High Pressure Ratio Centrifugal Compressor. 热科学学报：英文版[J]. 2018, 27(1): 17-24, http://lib.cqvip.com/Qikan/Article/Detail?id=676042190.[37] Li Guoqing, Zhang Qian, Guo Lei, Yu Qiangpeng, Xu Gang, Zhu Junqiang. Leakage and wear characteristics of finger seal in hot/cold state for aero-engine. TRIBOLOGY INTERNATIONAL[J]. 2018, 127: 209-218, http://dx.doi.org/10.1016/j.triboint.2018.06.008.[38] 王奉明, 朱俊强, 陈博, 徐纲. 水平起降Ma4高速飞机用涡轮冲压组合发动机研制关键技术难点解析及对策研究. 推进技术[J]. 2018, 39(10): 2303-2312, http://lib.cqvip.com/Qikan/Article/Detail?id=676482628.[39] 王奉明, 朱俊强, 徐纲. 基于整机试车的涡轮叶片高低循环复合疲劳试验技术. 航空动力学报[J]. 2018, 33(10): 2343-2350, http://lib.cqvip.com/Qikan/Article/Detail?id=72756873504849564948484853.[40] 王奉明, 贺进, 朱俊强. 高转速小尺寸涡轮叶片动应力测量方法与应用. 推进技术[J]. 2018, 39(6): 1406-1411, http://lib.cqvip.com/Qikan/Article/Detail?id=675443762.[41] 李紫良, 柴猛, 朱俊强. 某超高负荷低压涡轮叶型气动性能分析. 工程热物理学报[J]. 2018, 39(12): 2603-2610, http://lib.cqvip.com/Qikan/Article/Detail?id=6100035284.[42] Wang, Yi, Han, Ge, Lu, Xingen, Zhu, Junqiang. The influence of wedge diffuser blade number and divergence angle on the performance of a high pressure ratio centrifugal compressor. JOURNAL OF THERMAL SCIENCE[J]. 2018, 27(1): 17-24, http://lib.cqvip.com/Qikan/Article/Detail?id=676042190.[43] 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.[44] 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, [45] 韩建涛, 王晏根, 阳诚武, 李紫良, 朱俊强. 跨音速涡轮平面叶栅风洞收缩段设计方法研究. 燃气轮机技术[J]. 2017, 30(2): 17-22, http://lib.cqvip.com/Qikan/Article/Detail?id=672578477.[46] Huang Enliang, Zhao Shengfeng, Gong Jianbo, Lu Xingen, Zhu Junqiang. Numerical Investigation of the Bowed Stator Effects in a Transonic Fan at Low Reynolds Number. JOURNAL OF THERMAL SCIENCE[J]. 2017, 26(1): 25-29, https://www.webofscience.com/wos/woscc/full-record/WOS:000391416800004.[47] 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.[48] Mu Yong, Wang Chengdong, Liu Cunxi, Liu Fuqiang, Hu Chunyan, Xu Gang, Zhu Junqiang. Numerical Study of Effect of Compressor Swirling Flow on Combustor Design in a MTE. JOURNAL OF THERMAL SCIENCE[J]. 2017, 26(4): 349-354, https://www.webofscience.com/wos/woscc/full-record/WOS:000404949700008.[49] 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.[50] 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.[51] 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.[52] Sun Shuang Lei Zhijun Lu Xingen Zhang Yanfeng and Zhu Junqiang. The Effect of FSTI to the Combined Separation Control Strategy of Surface Roughness With Upstream Wakes. 2016, http://ir.etp.ac.cn/handle/311046/115706.[53] 孙爽, 雷志军, 卢新根, 赵胜丰, 朱俊强. 来流条件对超高负荷低压涡轮附面层非定常特性影响的实验研究. 推进技术[J]. 2016, 37(4): 653-661, [54] 王奉明, 朱俊强, 徐纲. 航空发动机加速任务与等效应力试验方法研究. 燃气涡轮试验与研究[J]. 2016, 29(3): 1-6, http://lib.cqvip.com/Qikan/Article/Detail?id=7000000970.[55] Lu, Xingen, Ge, Han, Zhu, Junqiang. Flow and Loss Mechanisms Within an Interturbine Duct. JOURNAL OF PROPULSION AND POWER[J]. 2016, 32(3): 734-742, https://www.webofscience.com/wos/woscc/full-record/WOS:000376672600020.[56] 孙爽, 李伟, 雷志军, 卢新根, 付宇, 朱俊强. 来流湍流度对超高负荷低压涡轮附面层流动控制手段的影响. 航空动力学报[J]. 2016, 31(7): 1686-1694, [57] 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.[58] Liu Jun, Wang Pei, Du Qiang, Liu Guang, Zhu Junqiang. Effects of Rising Angle on Upstream Blades and Intermediate Turbine Duct. JOURNAL OF THERMAL SCIENCE[J]. 2016, 25(4): 293-301, http://ir.etp.ac.cn/handle/311046/112487.[59] Liu Guang, Du Qiang, Liu Jun, Wang Pei, Zhu JunQiang. Numerical investigation of radial inflow in the impeller rear cavity with and without baffle. SCIENCE CHINA-TECHNOLOGICAL SCIENCES[J]. 2016, 59(3): 456-467, http://ir.etp.ac.cn/handle/311046/112440.[60] 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.[61] Li, Guoqing, Zhu, Junqiang, Wang, Kai, Li, Haiwang, Zhang, Qian. Film cooling performance in a low speed 1.5-stage turbine: effects of mainstream Reynolds number and turbulence. HEAT AND MASS TRANSFER[J]. 2015, 51(6): 795-805, http://ir.etp.ac.cn/handle/311046/98920.[62] 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.[63] 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.[64] 孙爽, 雷志军, 卢新根, 李伟, 朱俊强. 超高负荷低压涡轮非定常特性实验. 航空动力学报[J]. 2015, 30(5): 1192-1199, [65] 康剑雄, 黄国平, 朱俊强, 温殿忠. 离心压气机失速模式及自循环机匣处理的作用机制. 航空动力学报[J]. 2015, 30(12): 2960-2969, [66] Sun Shuang, Lei Zhijun, Lu Xingen, Zhao Shengfeng, Zhu Junqiang. An Experimental Study of Separation Control on Ultra-Highly-Loaded Low Pressure Turbine Blade by Surface Roughness. JOURNAL OF THERMAL SCIENCE[J]. 2015, 24(3): 229-238, https://www.webofscience.com/wos/woscc/full-record/WOS:000354151500004.[67] 阳诚武, 赵胜丰, 韩戈, 卢新根, 朱俊强. 跨声速压气机多圆柱孔式处理机匣设计与扩稳机理研究. 推进技术[J]. 2015, 36(3): 385-391, [68] Zhao, Shengfeng, Lu, Xingen, Zhu, Junqiang, Ge, Han, Yang Chengwu. Effects of low Reynolds number on flow stability of a transonic compressor. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING[J]. 2015, 229(4): 601-611, http://ir.etp.ac.cn/handle/311046/98931.[69] 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.[70] Yin, Juan, Weng, Yiwu, Zhu, Junqiang. Numerical and Experimental Investigation on the Performance of Lean Burn Catalytic Combustion for Gas Turbine Application. JOURNAL OF THERMAL SCIENCE[J]. 2015, 24(2): 185-193, http://ir.etp.ac.cn/handle/311046/98934.[71] Wang Huishe, Zhu Junqiang. Stream Surface Theory of Bird-like Flapping Flight. JOURNAL OF THERMAL SCIENCE[J]. 2015, 24(5): 417-426, http://ir.etp.ac.cn/handle/311046/98958.[72] Liu Fuqiang, Zhang Kaiyu, Mu Yong, Liu Cunxi, Yang Jinhu, Xu Gang, Zhu Junqiang. Experimental Investigation on Ignition and Lean Blow-out Performance of a Multi-sector Centrally Staged Combustor. JOURNAL OF THERMAL SCIENCE[J]. 2014, 23(5): 480-485, http://ir.etp.ac.cn/handle/311046/105998.[73] Liu Jun, Du Qiang, Liu Guang, Wang Pei, Zhu Junqiang. Effects of Nozzle-Strut Integrated Design Concepton on the Subsonic Turbine Stage Flowfield. 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发表著作
（1） 航空发动机进排气系统气动热力学, 上海交通大学出版社, 2015-07, 第 1 作者
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