1. 主持国防重点项目、173子课题及国自科青年基金等三项国家级课题；

2. 主持“江西省赣鄱俊才支持计划”人才项目；

3. 主持江西省自然青年/面上、北京市自然基金联合项目、国防重点实验室基金等七项省部级课题；

4. 主持多项国防/横向课题。

1. 入选江西省赣鄱俊才支持计划；

2. 入选江西省教学成果奖青年培育项目；

3. 指导学生获得第五届及第七届全国高校航空航天类专业本科毕业设计成果大赛一等奖。

代表性论文：

[1]  YH Mi, ZT Zhou*, TY Cao, et al. Cooling effect of multi-stage water injection on the rocket thermal environment[J]. Aerospace Science and Technology, 2026, 170: 111536.

[2]  ZT Zhou, TY Cao, RH Liang, et al. Influence of the fuel jet injection angle on the combustion process of a

gel scramjet[J]. Aerospace Science and Technology, 2025, 162: 110180.

[3]   ZT Zhou, YH Mi. Influence of the deflector surface configuration on thermal environment during rocket launching[J]. Applied Thermal Engineering, 2025, 270: 126277.

[4]   ZT Zhou,  TY Cao, YQ Li, et al.  Progress on Ablation of Nozzle Throat Inserts in Solid Rocket Motors[J]. Fluid Dynamics, 2025, 60(28), 1-34.

[5]   DH Wang, DH Cao, ZT Zhou*, et al. Numerical simulation of fluid–structure interaction for solid rocket engine nozzle ablation[J]. Advances in Aerodynamics, 2025, 7(2): 1-18.

[6]   ZT Zhou, SB Qv, B Liu. Influence of boron particle diameter on combustion process of gel scramjet[J]. Physics of Fluids, 2024, 36, 103321.

[7]  ZT Zhou, YY Bao. Investigating the rocket base flow characteristics and thermal environment of different nozzle configurations considering afterburning[J]. International Journal of Thermal Sciences, 2023, 185: 108073.

[8]  ZT Zhou, PJ Sun, YY Bao. Numerical simulations of thermal environment of the rocket impingement jet with afterburning under different water spray angles[J]. Aerospace Science and Technology, 2022, 121: 107308.

[9]  ZT Zhou, YY Bao, PJ Sun, et al. Cooling of rocket plume using aqueous jets during launching[J]. Engineering Applications of Computational Fluid Mechanics, 2022, 16(1): 20-35.

[10]  ZT Zhou, YY Bao, PJ Sun, et al. Afterburning effect on thermal environment of four engine liquid rockets at different altitudes[J]. Engineering Applications of Computational Fluid Mechanics, 2021, 15(1): 1134-1146.

[11]  ZT Zhou, X Wang, CY Lu, et al. Numerical analysis on thermal environment of liquid rocket with afterburning under different altitudes[J]. Applied Thermal Engineering, 2020, 178: 115584.

[12]  ZT Zhou, LJ Zhang, GG Le. Numerical study for the flame deflector design of four-engine liquid rockets[J]. Engineering Applications of Computational Fluid Mechanics, 2020, 14(1): 726-737.

[13]  ZT Zhou, CF Zhao, CY Lu, et al. Numerical studies on four-engine rocket exhaust plume impinging on flame deflectors with afterburning[J]. Defence Technology, 2020, 17(4): 1207-1216.

[14]  ZT Zhou, GG Le, LJ Zhang. Numerical studies of afterburning on impingement flowfield of the four-engine rockets[J]. Journal of Spacecraft and Rocket, 2020, 57(6): 1284-1294.

[15]  ZT Zhou, LM Wang, YQ Li. Effect of uplift angle on thermal environment of flame deflector during rocket launch[J]. Advances in Space Research, Available online 21 December 2022.

[16] ZT Zhou, CY Lu, CF Zhao, et al. Numerical simulations of water spray on flame deflector during the four-engine rocket launching[J]. Advances in Space Research, 2020, 65: 1296-1305.

[17] ZT Zhou, XY Liang, CF Zhao, et al. Investigations of base thermal environment on four-nozzle liquid launch vehicle at high altitude[J]. Journal of Spacecraft and Rocket, 2020, 57(1): 49-57.

[18] ZT Zhou, CF Zhao, CY Lu, et al. Numerical studies on flowfield characteristics of four-engine rockets impinging jet with different flame deflectors[C]. International Conference on Defence Technology, 2020.

[19] 周志坛, 李怡庆, 江平, 等. 二次燃烧对多喷管运载火箭底部热环境影响研究[J]. 航空动力学报, 2024, 39(6): 20210694.

[20] 周志坛, 乐贵高, 梁晓扬, 等. 多喷管运载火箭尾焰对导流槽的冲击特性研究[J]. 工程热物理学报, 2019, 40(9): 2027-2035.

[21] 周志坛, 丁逸夫, 乐贵高, 等. 高空飞行环境中液体运载火箭底部热环境研究[J]. 宇航学报, 2019, 40(5): 577-584.

希望招收性格开朗，对流体力学有兴趣的研究生，联系邮箱：ztzhou93@nchu.edu.cn