[1]. Meng J, Li M, Zhang L, et al. Effect of flight parameters on thermal performance of a hybrid air vehicle for cargo transportation[J]. Applied Thermal Engineering, 2020, 168: 114807.
[2]. Meng J, Liu S, Yao Z, et al. Optimization design of a thermal protection structure for the solar array of stratospheric airships[J]. Renewable energy, 2019, 133: 593-605.
[3]. Zhang L, Lv M, Meng J, Du H. Optimization of solar-powered hybrid airship conceptual design. Aerospace Science and Technology 2017, 65: 54-61.
[4]. Zhang L, Lv M, Meng J*, Du H. Conceptual design and analysis of hybrid airships with renewable energy. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 2017: Published Online.
[5]. Meng J, Zhang L, Li J, Lv M. Dynamic modeling and simulation of tethered stratospheric satellite with thermal effects. Applied Thermal Engineering 2017, 110: 181-189.
[6]. Meng J, Yao Z, Du H, Lv M. Thermal protection method of the solar array for stratospheric airships. Applied Thermal Engineering 2017, 111: 802-810.
[7]. Meng J, Qu Z, Zhu W, Lv M. Fatigue damage mechanical model of the envelope material for stratospheric airships. Applied Composite Materials 2017, 24(4): 837-848.
[8]. Meng J, Lv M, Qu Z, Li P. Mechanical properties and strength criteria of fabric membrane for the stratospheric airship envelope. Applied Composite Materials 2017, 24(1): 77-95.
[9]. Meng J, Lv M. The constitutive relation of a fabric membrane composite for a stratospheric airship envelope based on invariant theory. Computers Materials & Continua 2017, 53(2): 73-89.
[10]. Meng J, Li P, Ma G, Du H, Lv M. Tearing behaviors of flexible fiber-reinforced composites for the stratospheric airship envelope. Applied Composite Materials 2017, 24(3): 735-749.
[11]. Meng J, Hu J, Xiao H, Lv M. Hierarchical optimization of the composite blade of a stratospheric airship propeller based on genetic algorithm. Struct Multidiscip Optim 2017, 56(6): 1341-1352.
[12]. Meng J, Cao S, Qu Z, Li J, Lv M. Thermoelasticity of a fabric membrane composite for the stratospheric airship envelope based on multiscale models. Applied Composite Materials 2017, 24(1): 209-220.
[13]. Lv M, Yao Z, Zhang L, Du H, Meng J, Li J. Effects of solar array on the thermal performance of stratospheric airship. Applied Thermal Engineering 2017, 124: 22-33.
[14]. Lv M, Li J, Zhu W, Du H, Meng J, Sun K. A theoretical study of rotatable renewable energy system for stratospheric airship. Energy Conversion and Management 2017, 140: 51-61.
[15]. Lv M, Li J, Du H, Zhu W, Meng J. Solar array layout optimization for stratospheric airships using numerical method. Energy Conversion and Management 2017, 135: 160-169.
[16]. Meng J, Lv M, Tan D, Li P. Mechanical properties of woven fabric composite for stratospheric airship envelope based on stochastic simulation. J Reinf Plast Compos 2016, 35(19): 1434-1443.
[17].糜攀攀,孟军辉,吕明云.浮升混合飞艇气动性能及总体参数分析.北京航空航天大学学报2015, 41(6): 1108-1116.
[18].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(5): 1500-1510.
[19].孟军辉,曹帅,吕明云.平流层飞艇蒙皮材料撕裂性能分析方法.宇航学报2015, 36(2): 230-235.
[20].曹帅,刘龙斌,孟军辉,吕明云.杆模型的平流层飞艇蒙皮撕裂扩展分析.哈尔滨工业大学学报2015, 47(11): 58-62.
[21].孟军辉,张艳博,吕明云.平流层飞艇蒙皮材料织物纤维拔出过程分析.北京航空航天大学学报2013, 40(8): 1149-1153.
教学工作
1. 主讲《结构力学A》本科生课程(48学时)
2. 主讲《飞行器结构优化设计》研究生课程(32学时)