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江荣，南京航空航天大学教授、博士生导师。兼任“航空发动机及燃气轮机”基础科学中心结构强度专业组秘书，航空学会失效分会委员、机械工程学会材料分会委员、中国材料研究学会疲劳分会理事，《推进技术》、《南航学报》（英文版）、《失效分析与预防》编委，英国南安普顿大学客座教授。主要从事航空发动机涡轮转子强度与寿命设计、风扇/压气机叶片硬物损伤容限设计与维修性评估方法研究，先后主持国家自然科学基金（2项面上+1项青基）、装发预研领域基金、两机基础科学中心重点项目、民机专项专题，两机专项子课题、江苏省优秀青年基金等项目20余项，发表期刊论文80余篇，申请国家发明专利30余项，获国防科技进步一等奖、江苏省航空航天学会青年科学家等荣誉，研究成果为多个型号发动机结构强度与寿命设计提供支撑。诚挚欢迎具有航空宇航推进理论与工程、机械工程、力学或材料科学与工程等学科基础的同学加入本课题组！本人硕、博士招生方向：（1）0825 航空宇航科学与技术（2）0807 动力工程及工程热物理（3）0858 能源动力近5年代表性论文：[1] Jiang R*, Song YD, Reed PA*. Fatigue crack growth mechanisms in powder metallurgy Ni-based superalloys—A review. International Journal of Fatigue (中科院1区) 2020;141:105887.[2] Kim D, Jiang R*, Evangelou A, Sinclair I, Reed PAS. Effects of γʹ size and carbide distribution on fatigue crack growth mechanisms at 650 °C in an advanced Ni-based superalloy. International Journal of Fatigue (中科院1区) 2021;145:106086.[3] Jiang R*, Zhang LC, Zhang WT, Zhang Y, Chen Y, Liu JT, et al. Low cycle fatigue and stress relaxation behaviours of powder metallurgy Ni-based superalloy FGH4098. Materials Science and Engineering: A (中科院1区) 2021;817:141421.[4] Jia X, Zhang ZW, Ling C, Jiang R*, Song YD. Foreign object damage characteristics and their effects on high cycle fatigue property of Ni-based superalloy GH4169. Fatigue and Fracture of Engineering Materials and Structures (中科院2区), 2022, 45(4), pp. 1165–1178. [5] Zhang WT, Jiang R*, Zhao Y, Zhang LC, Zhang L, Zhao LG, Song YD. Effects of temperature and microstructure on low cycle fatigue behaviour of a PM Ni-based superalloy: EBSD assessment and crystal plasticity simulation. International Journal of Fatigue (中科院1区), 2022, 159, 106818[6] Jiang R*, Zhang WT, Zhao Y, Zhang LC, Zhang L, Song YD. Strain localization and crack initiation behavior of a PM Ni-based superalloy: SEM-DIC characterization and crystal plasticity simulation. Fatigue and Fracture of Engineering Materials and Structures (中科院2区), 2022, 45(6), pp. 1635–1651.[7] Zhao Y, Jiang R *, Harte A, Bull DJ, Reed PAS. Characterisation of strain localisation under cyclic loading at 450 °C by SEM-DIC in a PM Ni-based superalloy. Materials Science and Engineering A (中科院1区), 2022, 849, 143464[8] Jia X. Ling C, Zhang ZW, Jiang R *, Song YD. Effect of the notched foreign object damage depth on the HCF strength of titanium alloy TC11. Engineering Fracture Mechanics (中科院2区), 2022, 271, 108639[9] Zhang LC, Jiang R*, Wang YC, Zhang L, Liu JT, Zhang YW, Song YD. Effects of microstructure and temperature on short fatigue crack propagation behaviour of powder metallurgy superalloy FGH4098 in vacuum. Materials Science and Engineering A(中科院1区), 2022, 852, 143637[10] Wu CH, Jiang R*, Zhang LC, Wang YC, Chen Y, Song YD, Oxidation accelerated dwell fatigue crack growth mechanisms of a coarse grained PM Ni-based superalloy at elevated temperatures, Corrosion Science (中科院1区), 2022, 209:110702[11] Jiang R*, Wang YC, Zhang LC, Chen Y, Zhang H, Wang ZB, et al. Fatigue crack propagation behavior of the grain size transition zone in a dual microstructure turbine disc. International Journal of Fatigue (中科院1区), 2023, 172:107647[12] Y. Zhao, R. Jiang*, R.X. Wang, Z.H. Li L. Zhang, L.G. Zhao, LCF life prediction of turbine disc alloy using crystal plasticity and 3D representative volume element containing twin boundaries. International Journal of Fatigue (中科院1区), 2024, 179:108075更多论文发表情况请参见以下网址：https://www.scopus.com/authid/detail.uri?authorId=57203365675