北航飛行器設計學科責任教授，博士生導師。擔任國家某重點飛行器的副總指揮兼副總設計師，取得的多項研究成果已獲得武器裝備型號應用。先后主持國家高分專項項目1項、國防科技創新特區項目4項、國家“863”項目10項、國防預研項目6項、航天創新基金項目6項、及航空航天院所項目30余項等科研項目，包括：“***總體與試驗技術”、“***飛行器總體與試驗技術”、“超材料隱身技術”、“***可見光智能偽裝技術”、“****多功能復合材料結構技術”、“***輕量化防彈復合材料艙體一體化技術”等。發表SCI/EI論文100余篇，獲授權國家發明專利20余項，獲國防科技進步三等獎2項、全軍武器裝備科學技術獎1項。培養碩士研究生40余名、博士研究生20余名。

部分代表性論文

(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)孟軍輝,張一,劉東旭,呂明云,武哲.升力體式浮升混合飛艇設計及參數分析.航空學報,2015,36(05):1500-1510.

(22)肖厚地,劉龍斌,呂明云. X型尾翼臨近空間飛艇隱身特性仿真[J].北京航空航天大學學報,2015,41(01):181-186.

(23)呂明云,黃敏杰,武哲.封閉式隱身桅桿的初步設計與效果評估[J].電波科學學報,2010,25(05):833-838.

(24)蒙志君,呂明云,武哲,祝明.頻率選擇表面A夾層雷達罩的傳輸特性[J].光學精密工程,2010,18(05):1175-1181.

(25)黃敏杰,呂明云,黃俊,武哲.單元形狀的微小改變對頻率選擇表面電性能的影響[J].系統工程與電子技術,2009,31(07):1611-1614+1671.