个人简介
姓名：吕明云教授
所在单位：飞机系
研究方向：新概念飞行器设计，智能隐身技术，复合材料结构技术。
邮箱：lv503@buaa.edu.cn

详细介绍吕明云：教授，博士生导师；飞机系。
1969年7月生，中共党员，现担任军委科技委创新特区主题专家组专家，担任国家某重点飞行器的副总指挥兼副总设计师，取得的多项研究成果已获得武器装备型号应用。先后主持国家高分专项项目2项、国防科技创新特区项目3项、国家“863”项目10项、国防预研项目6项、航天创新基金项目6项、及航空航天院所项目30余项等科研项目，包括：“***总体与试验技术”、“***快速部署飞行器总体与试验技术”、“超材料隐身技术”、“***可见光智能伪装技术”、“****多功能复合材料结构技术”、“***大型复合材料舱体设计与一体化成型技术”等。发表SCI/EI论文100余篇，获授权国家发明专利20余项，获国防科技进步三等奖1项（排名1）、全军武器装备科学技术奖1项。培养硕士研究生40余名、博士研究生20余名。
联系方式：（办），（研究室办）
通讯地址：北京航空航天大学航空学院飞机系邮编：100083
Email:lv503@buaa.edu.cn
部分代表性论文：
(1) Xiao H, Qu Z,Lv M, et al. Optically transparent broadband and polarization insensitive microwave metamaterial absorber[J]. Journal of Applied Physics, 2019, 126(13): 135107.
(2) Du H,Lv M, Zhang L, et al. Energy management strategy design and station-keeping strategy optimization for high altitude balloon with altitude control system[J]. Aerospace Science and Technology, 2019, 93: 105342.
(3) Qu Z, Xiao H,Lv M, et al. Tear propagation behavior with a novel analytical model on envelope material[J].Materials Research Express, 2019, 6(10): 105320.
(4) Zhang L, Li J, Wu Y,Lv Met al.Analysis of attitude planning and energy balance of stratospheric airship[J].Energy, 2019, 183: 1089-1103.
(5) Qu Z, Xiao H,Lv M,et al. Influence of Strengthening Material Behavior and Geometry Parameters on Mechanical Behavior of Biaxial Cruciform Specimen for Envelope Material[J]. Materials, 2019,12(17): 2680.
(6) Du H,Lv M, Li J, et al. Station-keeping performance analysis for high altitude balloon with altitude control system[J].Aerospace Science and Technology, 2019,92: 644-652.
(7) Zhang L,Lv M, Zhu W, et al.Mission-based multidisciplinary optimization of solar-powered hybrid airship[J]. Energy conversion and management, 2019, 185: 44-54.
(8) Meng J, Liu S, Yao Z,Lv M, et al.Optimization design of a thermal protection structure for the solar array of stratospheric airships[J]. Renewable energy, 2019, 133: 593-605.
(9) H Du, J Li, W Zhu, Z Qu, L Zhang,M Lv.Flight performance simulation and station-keeping endurance analysis for stratospheric super-pressure balloon in real wind field[J]. Aerospace Science and Technology, 2019, 86: 1-10.
(10) Zhang L,Lv M, Sun C, et al. Flight performance analysis of hybrid airship considering added mass effects[J]. Journal of Dynamic Systems, Measurement, and Control, 2018, 140(11): 111001.
(11) Zhang L,Lv M, Meng J, et al. Conceptual design and analysis of hybrid airships with renewable energy[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2018, 232(11): 2144-2159.
(12) Qu Z, He W,Lv M, et al. Large-Strain Hyperelastic Constitutive Model of Envelope Material under Biaxial Tension with Different Stress Ratios[J]. Materials, 2018, 11(9): 1780.
(13) J Li, J Liao, Y Liao, H Du, S Luo, W Zhu,MLv. An approach for estimating perpetual endurance of the stratospheric solar-powered platform[J]. Aerospace Science and Technology, 2018, 79: 118-130.
(14) L Zhang, J Li,J Meng, H Du,M Lv, W Zhu. Thermal performance analysis of a high-altitude solar-powered hybrid airship[J].Renewable Energy, 2018, 125: 890-906.
(15) H Du, J Li, W Zhu, Z Yao, E Cui,M Lv.Thermal performance analysis and comparison of stratospheric airships with rotatable and fixed photovoltaic array[J]. Energy conversion and management,2018, 158: 373-386.
(16) Lv M., Li, J., Du, H., Zhu,W. and Meng, J. Solar array layout optimization for stratospheric airships using numerical method.Energy Conversion and Management,135, 2017. 160-169.
(17) Zhang, Lanchuan ,Lv, Mingyun, Meng,Junhui. Optimization of solar-powered hybrid airship conceptual design,Aerospace Science and Technology. 2017.
(18) Lv, M., Li, J., Zhu, W., Du,H., Meng, J. and Sun, K. A theoretical study of rotatable renewable energy system for stratospheric airship. Energy Conversion and Management, 104. 2017.51-61.
(19) Li, J.,Lv, M., Tan, D., Zhu, W. Output performance analyses of solar array on stratospheric airship with thermal effect. Applied Thermal Engineering, Vol. 104. 2016, 743-750.
(20) Meng J, Li P, Ma G, H Du,Lv M. TearingBehaviors of Flexible Fiber-Reinforced Composites for the Stratospheric Airship Envelope[J]. Applied Composite Materials, 2016:1-15.
(21) 孟军辉,张一,刘东旭,吕明云,武哲.升力体式浮升混合飞艇设计及参数分析.航空学报,2015,36(05):1500-1510.
(22) 肖厚地,刘龙斌,吕明云. X型尾翼临近空间飞艇隐身特性仿真[J].北京航空航天大学学报,2015,41(01):181-186.
(23) 吕明云,黄敏杰,武哲.封闭式隐身桅杆的初步设计与效果评估[J].电波科学学报,2010,25(05):833-838.
(24) 蒙志君,吕明云,武哲,祝明.频率选择表面A夹层雷达罩的传输特性[J].光学精密工程,2010,18(05):1175-1181.
(25) 黄敏杰,吕明云,黄俊,武哲.单元形状的微小改变对频率选择表面电性能的影响[J].系统工程与电子技术,2009,31(07):1611-1614+1671.