高齐宏，南京航空航天大学能源与动力学院长空博士后。2024年获南京航空航天大学博士学位。参与军委科技委基础加强计划重点基础研究项目、两机专项基础研究重点课题等科研项目。主要研究方向为箔片动压气体轴承的流动与传热特性以及内燃波转子泄漏密封特性等课题。共发表论文10余篇，公开2项发明专利。

发表学术论文/出版专著情况：

1. 1. Gao Q H, Sun W J, Zhang J Z. Numerical assessment on a hybrid axial throughflow cooling scheme applied to the thermal management of bump-type gas foil bearings [J]. Applied Thermal Engineering, 2025, 260:125044

2. 2. Gao Q H, Sun W J, Zhang J Z. A comparative study on inflow schemes of radial throughflow cooling for thermal management of a specific multi-layer gas foil thrust bearing [J]. International Journal of Heat and Mass Transfer, 2023, 216: 124564.

3. 3. Gao Q H, Sun W J, Zhang J Z. Thermo-elasto-hydrodynamic analysis of a specific multi-layer gas foil thrust bearing under thermal-fluid-solid coupling [J]. Chinese Journal of Aeronautics, 2023, 36(12): 231-246.

4. 4. Gao Q H, Sun W J, Zhang J Z. Prediction of aerodynamic and thermal performances for gas foil journal bearing with an axial cooling throughflow by machine learning method [J]. Thermal Science and Engineering Progress, 2023, 44: 102044.

5. 5. Gao Q H, Sun W J, Zhang J Z. Optimal design of top-foil wedge shape for a specific multi-layer gas foil thrust bearing by considering aerodynamic and thermal performances [J]. Thermal Science and Engineering Progress, 2023, 44: 102060.

6. 6. Gao Q H, Zhang J Z, Sun W J. Effects of annular-cooler surface-roughness on wind resistance and thermal environment in a high-speed geotechnical centrifuge chamber [J]. Case Studies in Thermal Engineering, 2021, 28: 101464.

7. 7. Gao Q H, Sun W J, Zhang J Z, et al. Fluid-solid coupled simulation on thermal management of hydrodynamic gas foil bearing with an axial cooling throughflow [J]. Case Studies in Thermal Engineering, 2022, 37: 102238.

8. 8. Gao Q H, Zhang J Z, Lyu Y W, et al. An experimental investigation of chevron-nozzle jet impingement heat transfer on a confined conical-concave surface [J]. Journal of Enhanced Heat Transfer, 2021, 28: 19-33.

9. 9. Sun W J, Zheng Y Q, Gao Q H*, Zhang J Z. Numerical simulations on film cooling performance of turbine blade before and after particles deposition [J]. Thermal Science and Engineering Progress, 2024, 49: 102504.

10. 10. 高齐宏，孙文静，王宇婕, 等. 带轴向通流冷却的动压气体轴承静承载力和气动热多参数影响分析[J]. 航空动力学报, 2022, DOI:10.13224/j.cnki.jasp.20220393.

11. 11. 高齐宏，张靖周，孙文静. 径向入流冷却箔片型气体动压止推轴承气动和热特性数值研究[J]. 推进技术, 2022, 43(11): 260-271.

12. 12. 高齐宏，张靖周，谭晓茗. 旋转盘腔轴向通流的压降和温升数值研究[J]. 推进技术, 2021, 42(9): 2062-2070.

13. 13. Gao Q H, Sun W J, Zhang J Z. Prediction of aerodynamic and thermal performances for gas foil journal bearing with an axial cooling throughflow by machine learning method [C]. 4th International Conference of Thermal Fluid Dynamics and Control, 2023.

14. 14. Sun W J, Gao Q H, Zhang J Z, et al. Aerosol infrared stealth technology: theory and development of infrared suppression and particle dispersion in aircraft plume [J]. Thermal Science and Engineering Progress, 2023, 39: 101695.

科研成果获奖及专利：

1. 1. 高齐宏，孙文静，王宇婕，等. 用于旋转空心轴通道的引气管道多股射流冲击冷却装置. (申请号：CN202210794765.1)

2. 2.  王宇婕，高齐宏，孙文静，等. 一种适用于旋转空心轴的带导流槽的纵向肋冷却结构. (申请号：CN202210708738.8)

航空发动机先进燃烧技术

负责人：李建中 教授
团队成员：金武、姚倩、秦琼瑶、巩二磊、高齐宏
研究方向：主要从事航空发动机高油气比燃烧、清洁燃烧、爆震燃烧、波转子燃烧等基础理论和关键技术研究。