个人简历

胡晓安，男，博士，副教授，主要研究航空发动机结构破坏理论和寿命预测方法和微小型航空发动机设计方法。
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：主讲航空发动机强度与振动；航空动力工程导论
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/973计划/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

近期论文

[1]XiaoanHu,QiangZhang,YunJiang,GuoFengRao,GuoLeiMiao,WeiFengHe,XiangFanNie.TheeffectofcyclicloadingonthecreepfatiguelifeandcreepstrengthofaDSsuperalloy:damagemechanismandlifemodeling[J].InternationalJournalofFatigue.2020.(SCIaccepted)
[2]HuXiaoAn,XueZhiYuan,JiangYun,etal.OnthefatiguecrackgrowthbehaviorofselectivelasermeltingfabricatedInconel625:effectsofbuildorientationandstressratio.Fatigue&FractureofEngineeringMaterials&Structures.2020.(SCIaccepted)
[3]HuXiaoAn,ZhaoGaoLe,JiangYun,HuangJia.ExperimentalinvestigationontheLCFbehavioraffectedbymanufacturingdefectsandcreepdamageofoneSelectiveLaserMeltingnickelbasesuperalloyat815℃.ActaMetallurgicaSinica(EnglishLetters).2020.(SCIaccepted)
[4]ZhaoGaoLe,JiangYun*,HuXiaoAn*,HuangJia,WuJinWu,WangYun.Hightemperaturemechanicalpropertiesofnickel-basedsuperalloysmanufacturedbyadditivemanufacturing.[J]Materialsscienceandtechnology.2020.(通讯，SCIaccepted)
[5]XiaoAnHu,GaoLeZhao,FenChengLiu,WeiXiongLiu.MicrostructureandmechanicalbehaviorofInconel625alloyprocessedbyselectivelasermeltingathightemperatureupto1000°C.Raremetals.2020.(SCIaccepted)
[6]HuXiaoan,ZhaoGaole,HuangJia*,WangXiangyi,YangXiaoguang.OutofPhaseThermalMechanicalFatiguebehaviorofaNiCrAlYSicoatedsuperalloy[J].JournalofMaterialsEngineeringandPerformance,2019,28(8):4582-4592
[7]XiaoAnHu,ZhiYuanXue,GaoLeZhao,etal.LaserweldingofaselectivelasermeltedNi-basesuperalloy:microstructureandhightemperaturemechanicalproperty.MaterialsScience&EngineeringA,2019,745,335-345.
[8]HuXiaoAn,ZhangQiang,YangXiao-Guang*,ShiDuo-Qi.Viscoplasticanalysismethodofanaeroengineturbinebladesubjectedtotransientthermalmechanicalloading.InternationalJournalofMechanicalSciences.,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]HuXiaoan,ZhaoGaole,YangXiaoguang,etal.Finiteelementanalysisandlifemodelingofanotchedsuperalloyunderthermalmechanicalfatigueloading[J].InternationalJournalofPressureVessels&Piping,2018,165:51-58.
[14]XiaoanHU，XiaoGuangYang，DuoqiShi.ThermomechanicalfatigueexperimentalstudyonanotcheddirectionallysolidifiedNi-basesuperalloy.MaterialsScience&EngineeringA.2016.674(30).451-458.
[15]XiaoAnHu*,XiaoGuangYang,DuoQiShi,HuiChenYu.Constitutivemodelingofadirectionallysolidifiednickel-basedsuperalloyDZ125subjectedtothermalmechanicalcreepfatigueloadings.RareMetals,2019,38(10):922-936.
[16]XiaoanHU,XiaoguangYANG,DuoqiSHI,HuichenYU.OutofphasethermalmechanicalfatigueinvestigationofdirectionallysolidifiedsuperalloyDZ125.ChineseJournalofAeronautics.2016.29(1).257-267.
[17]X.A.Hu,X.G.YANG,J.K.WANG,D.Q.SHI,J.HUANG.Asimplemethodtoanalysethenotchsensitivityofspecimensinfatiguetests.Fatigue&FractureofEngineeringMaterialandStructures.2013.36(10):2009-1016.
[18]Shi,Duoqi;Hu,Xiaoan;Yang,Xiaoguang;Liu,Jinlong.Continuumdamagemechanism-basedlifepredictionforNi-basedsuperalloyundercomplexloadings.Materialathightemperatures.2013.30(4):287-294.
[19]D.Q.SHI,X.A.Hu,J.K.WANG,X.G.YANG,H.C.YU,J.HUANG.Effectofnotchonfatiguebehaviorofadirectionallysolidifiedsupeeralloyathightemperature.Fatigue&FractureofEngineeringMaterialandStructures.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.