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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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
Zhang, Lanchuan ,Lv, Mingyun, Meng,Junhui. Optimization of solar-powered hybrid airship conceptual design,Aerospace Science and Technology. 2017.
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.
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.
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.
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.
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