主要从事先进飞行器总体设计，飞行器流固耦合分析与设计等方面的研究。在国内外重要学术刊物上发表学术论文40余篇，其中被SCI和EI收录30余篇；授权国家发明专利7项；2019年获中国科学技术协会青年人才托举工程资助，主持国家自然科学基金项目等纵向项目5项及研究院所横向项目多项。
[1] Luo J, Meng J, Yu N, et al. Configuration Optimization of a Skippable Anti-Ship Missile Considering Initial Kinematic Parameters[J]. AIAA Journal, 2024, 62(3): 1094-1104.（学生第一作者）
[2] Nianhui Y E, Teng L, Junhui M*, et al. Surrogate-assisted optimization for anti-ship missile body configuration considering high-velocity water touching[J]. Chinese Journal of Aeronautics, 2023, 36(12): 268-281.
[3]Ma N, Liu L, Meng F, Meng J*. Structural design and modal behaviors analysis of a new swept baffled inflatable wing[J]. Defence Technology, 2023, 24: 382-398.
[4]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.
[5]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.
[6]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.
[7]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.
[8]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.
[9]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.
[10]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.
[11]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.
[12]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.
[13]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.
[14]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.
[15]罗剑桥, 解春雷, 金泽华, 孟军辉*. 跨介质飞行器近水面滑跳流固耦合仿真及可滑跳区域研究, 航空学报, 2023, 44(21)
[16]马文朝, 孟繁敏, 马诺, 孟军辉*, 邹汝平. 跨介质飞行器头部外形优化及入水性能分析, 兵工学报,2022, 43(10): 2588-2597
[17]孟繁敏, 马诺, 马文朝, 孟军辉*, 李文光. 斜掠气梁充气翼湿模态分析与试验研究, 航空学报,2023, 44(2): 227098-1-227098-15
[18]孟军辉, 马诺, 胡睿, 金泽华, 李文光, 刘莉. 具有非对称褶皱结构的自生长软体机器人设计与运动特性, 兵工学报, 2022, 43(12): 3186-3199
教学工作
1. 主讲《结构力学A》本科生课程（48学时）
2. 主讲《飞行器结构分析与设计A》本科生课程（48学时）
3. 主讲《飞行器结构优化设计》研究生课程（32学时）
