1. 主持，江西省自然面上项目，含能凝胶燃料冲压发动机燃烧机理及性能优化研究；

2. 主持，江西省自然青年项目，可重复运载返回过程热流固耦合机制及热环境预示研究；

3. 主持，国防重点实验室基金，含金属粒子凝胶燃料冲压发动机燃烧特性研究；

4. 主持，横向课题，固体发动机内流场仿真分析与仿真样本库构建；

5. 主持，横向课题，相变膨胀做功过程仿真；

6. 主持，横向课题，液体发动机设计模块开发；

7. 主持，横向课题，湍流燃烧条件下含能工质反应机理及表征方法研究；

8. 参与，国家装备部项目，固体发动机点火准则和火焰传播机理研究（排名第二）。

2020年11月，获博士研究生国家奖学金；

2020年10月，获ICDT国际学术会议“优秀青年作者”荣誉称号；

2020年06月，获南京理工大学优秀博士培养基金；

2019年09月，获“开拓杯”未来飞行器设计大赛全国三等奖。

代表性论文：

[1]  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.

[2]  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.

[3]  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.

[4]  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.

[5]  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.

[6]  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.

[7]  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.

[8]  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.

[9]  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.

[10] 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.

[11] 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.

[12] 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.

[13] 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, 2022, 已录用.

[14] 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.

[15] 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