胡晓安
硕士生导师

副教授



hu_xiao_an@163.com

航空学院






个人简介
胡晓安，男，博士，副教授，江西省“青年井冈”****（2019），主要研究先进航空发动机的热端结构设计方法和微小型航空发动机整机设计与试验方法，参与xxx涡扇发动机、xxx涡轴发动机、xxx超燃冲压发动机、F级重型燃气轮机等多个国家重大型号研制，发表SCI/EI论文二十余篇，授权发明专利5项，获江西省自然科学一等奖1项。
教育经历：
2010/9-2015/6，北京航空航天大学，航空宇航推进理论与工程，博士
2004/9-2008/6，北京航空航天大学，飞行器动力工程，学士
工作经历：
2016/11-至今，南昌航空大学
2008/6-2016/11，XXXX部队(期间赴北航攻读硕/博士学位)
教学情况：本科生《航空发动机强度与振动》和《航空动力工程导论》；硕士生《航空发动机结构强度设计》
科研情况：主持课题：国家自然科学基金、省自然科学基金、“两机”重大专项/企业横向的外委课题若干
[1] 高瞬态高温升下薄壁结构破坏的寿命规律及其预测方法研究，国家自然科学基金，2020.01-2022.12
[2] 镍基定向凝固合金复杂热机械疲劳本构理论与精确建模方法，江西省自然科学基金， 2019.01-2021.12
近年来代表性论文：
[1] Xiaoan Hu, Qiang Zhang, Yun Jiang, GuoFeng Rao, GuoLei Miao, WeiFeng He, XiangFan Nie. The effect of cyclic loading on the creep fatigue life and creep strength of a DS superalloy: damage mechanism and life modeling [J]. International Journal of Fatigue. 2020. (SCI accepted)
[2] Hu XiaoAn, XueZhi Yuan, Jiang Yun, et al. On the fatigue crack growth behavior of selective laser melting fabricated Inconel 625: effects of build orientation and stress ratio. Fatigue & Fracture of Engineering Materials & Structures. 2020. (SCI accepted)
[3] Hu XiaoAn, Zhao GaoLe, Jiang Yun, Huang Jia. Experimental investigation on the LCF behavior affected by manufacturing defects and creep damage of one Selective Laser Melting nickel base superalloy at 815℃. Acta Metallurgica Sinica (English Letters). 2020. 33: 514–527
[4] Zhao GaoLe, Jiang Yun*, Hu XiaoAn*, Huang Jia, Wu JinWu, Wang Yun. High temperature mechanical properties of nickel-based superalloys manufactured by additive manufacturing.[J] Materials science and technology. 2020. (通讯，SCI accepted)
[5] XiaoAn Hu, GaoLe Zhao, FenCheng Liu, WeiXiong Liu. Microstructure and mechanical behavior of Inconel 625 alloy processed by selective laser melting at high temperature up to 1000 °C. Rare metals. 2020. (SCI accepted)
[6] Hu Xiaoan, Zhao Gaole, Huang Jia*, Wang Xiangyi, Yang Xiaoguang. Out of Phase Thermal Mechanical Fatigue behavior of a NiCrAlYSi coated superalloy[J]. Journal of Materials Engineering and Performance, 2019, 28(8): 4582-4592
[7] XiaoAn Hu, ZhiYuan Xue, GaoLe Zhao, et al. Laser welding of a selective laser melted Ni-base superalloy: microstructure and high temperature mechanical property. Materials Science & Engineering A, 2019, 745, 335-345.
[8] Hu XiaoAn, Zhang Qiang, Yang Xiao-Guang*, Shi Duo-Qi.Viscoplastic analysis method of an aeroengine turbine blade subjected to transient thermal mechanical loading. International Journal of Mechanical Sciences. , 2019, 152, 247-256.
[9] 胡晓安, 石多奇, 杨晓光, 于慧臣. TMF本构和寿命模型：从光棒到涡轮叶片[J]. 航空学报，2019. 40(3): 263-279 （EI）
[10] 胡晓安，张宇，阳海棠*，赵高乐，程穆威，姜云. 某3D-SiC/SiC陶瓷基复合材料拉伸和弯曲破坏行为研究[J]. 复合材料学报, 2019. 36(8)：1879-1885 （A1，EI）
[11] 薛志远，胡晓安*, 赵高乐, 饶国锋. 某涡扇发动机篦齿盘均压孔损伤容限分析方法[J]. 机械设计, 2019. 36(8): 66-71 (通讯作者，中文核心)
[12] 胡晓安, 石多奇, 庞学佳,等. 某涡轮叶片热障涂层的寿命预测方法[J]. 航空动力学报, 2018, 33(1):48-53.（EI）
[13] Hu Xiaoan, Zhao Gaole, Yang Xiaoguang, et al. Finite element analysis and life modeling of a notched superalloy under thermal mechanical fatigue loading[J]. International Journal of Pressure Vessels & Piping, 2018, 165:51-58.
[14] Xiaoan HU，XiaoGuang Yang，Duoqi Shi. Thermomechanical fatigue experimental study on a notched directionally solidified Ni-base superalloy. Materials Science & Engineering A. 2016. 674(30). 451-458.
[15] XiaoAn Hu*, XiaoGuang Yang, DuoQi Shi, HuiChen Yu. Constitutive modeling of a directionally solidified nickel-based superalloy DZ125 subjected to thermal mechanical creep fatigue loadings. Rare Metals, 2019, 38(10): 922-936.
[16] Xiaoan HU, Xiaoguang YANG, Duoqi SHI, Huichen YU. Out of phase thermal mechanical fatigue investigation of directionally solidified superalloy DZ125. Chinese Journal of Aeronautics. 2016.29(1).257-267.
[17] X. A. Hu, X. G. YANG, J. K. WANG, D. Q. SHI, J. HUANG. A simple method to analyse the notch sensitivity of specimens in fatigue tests. Fatigue & Fracture of Engineering Material and Structures. 2013. 36(10): 2009-1016.
[18] Shi, Duoqi;Hu, Xiaoan;Yang, Xiaoguang;Liu, Jinlong. Continuum damage mechanism-based life prediction for Ni-based superalloy under complex loadings. Material at high temperatures. 2013. 30(4): 287-294.
[19] D. Q. SHI, X. A. Hu, J. K. WANG, X. G. YANG, H. C. YU, J. HUANG. Effect of notch on fatigue behavior of a directionally solidified supeeralloy at high temperature. Fatigue & Fracture of Engineering Material and Structures. 2013. 36(12): 1288-1297.
[20] 胡晓安, 王井科, 杨晓光,石多奇, 黄佳.高温条件下DZ125缺口疲劳性能试验研究. 航空动力学报. 2013. 28(7): 1613-1617.
[21] 杨晓光, 胡晓安, 石多奇, 王井科, 黄佳. 概念设计时影响涡轮转子叶片强度的关键因素. 航空动力学报. 2012, 27(10): 2314-2320.







研究方向
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