主要從事先進飛行器總體設計，飛行器流固耦合分析與設計等方面的研究。在國内外重要學術刊物上發表學術論文40餘篇，其中被SCI和EI收錄30餘篇；授權國家發明專利7項；2019年獲中國科學技術協會青年人才托舉工程資助，主持國家自然科學基金項目等縱向項目5項及研究院所橫向項目多項。
[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.（學生第一作者）
[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]羅劍橋, 解春雷, 金澤華, 孟軍輝*. 跨介質飛行器近水面滑跳流固耦合仿真及可滑跳區域研究, 航空學報, 2023, 44(21)
[16]馬文朝, 孟繁敏, 馬諾, 孟軍輝*, 鄒汝平. 跨介質飛行器頭部外形優化及入水性能分析, 兵工學報,2022, 43(10): 2588-2597
[17]孟繁敏, 馬諾, 馬文朝, 孟軍輝*, 李文光. 斜掠氣梁充氣翼濕模态分析與試驗研究, 航空學報,2023, 44(2): 227098-1-227098-15
[18]孟軍輝, 馬諾, 胡睿, 金澤華, 李文光, 劉莉. 具有非對稱褶皺結構的自生長軟體機器人設計與運動特性, 兵工學報, 2022, 43(12): 3186-3199
教學工作
1. 主講《結構力學A》本科生課程（48學時）
2. 主講《飛行器結構分析與設計A》本科生課程（48學時）
3. 主講《飛行器結構優化設計》研究生課程（32學時）
