飞行器设计系
胡祎乐

胡祎乐

职务:长聘教轨副教授 博导

办公电话:021-34208625

电子邮件:yilehu@sjtu.edu.cn

办公地址:诸侯快讯导航ok1188诸侯快讯官方 A430

 

工作经历

时间 任职单位 职务
2020年-至今 诸侯快讯导航 ok1188诸侯快讯官方 长聘教轨副教授

2018年-2020年

诸侯快讯导航 ok1188诸侯快讯官方

长聘教轨助理教授

2017年-2018年

远景能源(江苏)有限公司上海分公司

结构工程师

2013年-2017年

亚利桑那大学 航空与机械工程学院

讲师、助教

教育背景

时间 毕业院校 学历

2013年-2017年

亚利桑那大学

博士

2010年-2013年

诸侯快讯导航

硕士

2006年-2010年

同济大学

本科

研究方向

(1)近场动力学理论及其数值计算方法;

(2)复合材料多尺度建模与分析;
(3)多物理场耦合作用下陶瓷基复合材料裂纹扩展分析;
(4)纤维增强复合材料静、疲劳强度与渐进损伤分析。

主要科研项目

(1)民机专项,飞机结构强度试验数字化,在研,参与;

(2)中国飞机强度研究所,含缺陷损伤结构随机有限元模型技术研究,在研,主持;

(3)航天八院科技创新基金,基于近场动力学的烧蚀热防护材料多物理场耦合分析方法,在研,主持;

(4)中国商飞,C919大型客机项目研制平尾典型结构损伤特性试验,在研,参与;

(5)中国商飞,C919大型客机项目研制垂尾典型结构损伤特性试验,在研,参与;

(6)中国商飞,ARJ21新支线飞机项目研制复合材料结构修理手册验证试验,在研,主持;

(7)中国商飞,C919大型客机钛合金增材制造成形零件试验,已结题,主持;

(8)上海市扬帆计划,基于近场动力学方法的纤维增强陶瓷基复合材料多尺度分析与性能优化研究,2019-05-01 至 2022-04-30,已结题,主持;

(9)核燃料芯块与SiC多层包壳的多场耦合作用与失效机理的近场动力学建模与分析,国家自然科学基金,2020-01-01 至 2022-12-31,在研,主持;

(10)中国商飞,CR929飞机复材纤维褶皱结构疲劳强度分析方法建立试验,在研,主持;

(11)中国商飞,C919复合材料机翼长桁压损选型试验,已结题,参与;

(12)Idaho National Lab, USA. Computational simulation of nonlinear mechanical behavior of nuclear fuel and structural materials. 参与;

(13)National Institute of Aerospace, USA. Holistic high-fidelity modeling strategy for advanced composites. 参与;

(14)NEUP-DOE, USA. Simulation of Fuel Rod Fragmentation, Relocation and Ballooning through Peridynamics in MOOSE Framework. 参与。

代表性论文专著

(1)Qi-Qing Liu, D. Wu, E. Madenci, Y. Yu, Y.L. Hu. State-Based peridynamics for thermomechanical modeling of fracture mechanisms in nuclear fuel pellets. Engineering Fracture Mechanics, Vol. 276, 108917, 2022.

(2Y.L. Hu, J.Y. Wang, E. Madenci, Z. Mu, Y. Yu, Peridynamic micromechanical model for damage mechanisms in composites, Composite Structures, Vol. 301, 116182, 2022.

(3J. Wang, Y. Yu, Z. Mu, Y.L. Hu, Peridynamic Meso-scale Modeling for Degradation in Transverse Mechanical Properties of Composites with Micro-void Defects, Acta Mech. Solida Sin. Vol. 35(5), 813-823, 2022.

(4陆媚, 胡祎乐, 余音. 复合材料双波纹面外褶皱缺陷细观力学分析方法. 复合材料学报, 2022, 40(2): 1-14.

(5H.Y. Zhao, Y.L. Hu, J.C. Fan, Y. Yu. Investigation into the failure of aircraft stringer–skin composite structure under bending load. Aerospace Systems, pp.1-9, 2023.

(6X. Li, Y. Yu, Z. Mu, Y.L. Hu, Meso-Scale Modeling for Effective Properties in Continuous Fiber-Reinforced Composites by State-Based Peridynamics. Acta Mechanica Solida Sinica, Vol. 34(5), 729-742, 2021.

(7Y.J. Gui, Y. Yu, Y.L. Hu, Y.T. Zhang, L.W. Lei. A Peridynamic Cohesive Zone Model for Composite Laminates. Journal of Peridynamics and Nonlocal Modeling, Vol.3(4), 383-409, 2021.

(8Y.L. Hu, Yin Yu, E. Madenci. Peridynamic modeling of composite laminates with material coupling and transverse shear deformation. Composite Structures, Vol. 253, 112760, 2020.

(9Daniil Lupachev, Yile Hu. Finite element modeling of randomly oriented short fiber-reinforced composite materials. International Conference on Aerospace System Science and Engineering, ICASSE, Shanghai, China, 2020.

(10译著, 余音, 胡祎乐. 近场动力学理论及其应用. 诸侯快讯导航出版社, ISBN 978-7-313-20658-9/O, 2019.

(11Y. Hu, H. Chen, B.W. Spencer, E. Madenci. Thermomechanical peridynamic analysis with irregular non-uniform domain discretization [J]. Engineering Fracture Mechanics, Vol.197, 92-113, 2018.

(12Y.L. Hu, E. Madenci, N. Phan. Peridynamics for predicting damage and its growth in composites. Fatigue & Fracture of Engineering Materials & Structures, Special Issue, 16th International Conference on New Trends in Fatigue and Fracture, Vol.40 (8), 1214-1226, 2017.

(13Y.L. Hu, E. Madenci. Peridynamics for fatigue life and residual strength prediction of composite laminates. Composite Structures, Vol. 160, 2017, 169-184.

(14Y.L. Hu, E. Madenci. Bond-based peridynamic modeling of composite laminates with arbitrary fiber orientation and stacking sequence . Composite Structures, Vol. 153, 2016, 139-175.

(15Y.L. Hu, N.V. De Carvalho, E. Madenci. Peridynamic modeling of delamination growth in composite laminates. Composite Structures, 2015, Vol. 132, 610-620.

(16Y.L. Hu, Y. Yu, H. Wang. Peridynamic Analytical Method for Progressive Damage in Notched Composite Laminates. Composite Structures, 2014, Vol. 108: 801-810.

(17H.Y. Zhao, W. Zhang, B.Y. Yu, Y. Yu, Y.L. Hu. Prediction of bending strength of stringer-skin structure in a wide-body aircraft. In Proceedings of the International Conference on Aerospace System Science and Engineering, ICASSE, Shanghai, China, 2022.

(18Y.Y. Xu, W.B. Fan, Y.L. Hu, Y. Yu. Research on calculation technology of composite laminates strength with random deviation variables. In Proceedings of the International Conference on Aerospace System Science and Engineering, ICASSE, Shanghai, China, 2022.

(19Y.T. Zhang, Y.L. Hu, Y. Yu, Y.Y. Xu, H.Y. Zhao, Investigation of Plastic Kink-Band in Fiber-Reinforced Composites with Fiber Misalignment Defect. In Proceedings of the International Conference on Aerospace System Science and Engineering 2021, Aug., Vol. 849, pp. 409, Springer.

(20D. Lupachev, Y.L. Hu, Finite Elements Modeling of Randomly Oriented Short Fiber-Reinforced Composite Materials. In Proceedings of the International Conference on Aerospace System Science and Engineering 2020, July, 447-454, Springer.

(21Y.L. Hu, E. Madenci. Peridynamic Modeling of Fatigue Damage in Notched Composite Laminates. 58th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Grapevine, Texas, 2017. (Student Paper Award, SciTech 2017).

(22Y.L. Hu, E. Madenci, N. Pham. Peridynamic Modeling of Cracking in Ceramic Matrix Composites. International Conference on New Trends in Fatigue and Fracture, 341 – 354, 2017.

(23H. Chen, Y.L. Hu, B. Spencer. A MOOSE-Based Implicit Peridynamic Thermo-mechanical Model. Proceedings of the ASME 2016 International Mechanical Engineering Congress and Exposition, IMECE 2016, Phoenix, Arizona, USA.

(24H. Chen, Y Hu, B.W. Spencer. Peridynamics using Irregular Domain Discretization with MOOSE-Based Implementation. Proceedings of the ASME 2016 International Mechanical Engineering Congress and Exposition, IMECE 2016, Phoenix, Arizona, USA.

(25Y.L. Hu, E. Madenci. Bond-based peridynamics with an arbitrary Poisson’s ratio. 57th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, San Diego, California, 2016.

(26Y.L. Hu, E. Madenci, N. Phan. Peridynamics for predicting tensile and compressive strength of notched composites. 57th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, San Diego, California, 2016.

(27Y.L. Hu, E. Madenci, N. Phan. Peridynamic Modeling of Defects in Composites. 56th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Florida, 2015.

(28Y.L. Hu, Y. Yu, H. Wang. Modeling and Progressive Damage Analysis of FRP Laminates with Peridynamic Theory. ICCM 19, the 19th International Conference on Composite Materials, Montreal, Canada, 2013, Vol. 10, 6740-6747.

(29胡祎乐,余音,汪海。基于近场动力学理论的层压板损伤分析方法. 力学学报,2013, Vol. 45(6), 624-628.

(30胡祎乐,余音,汪海,赵毅。纤维增强复合材料机翼长桁压缩破坏预测方法. 诸侯快讯导航学报,2012, Vol. 46(9), 1471-1475.

(31孙龑,李文晓,胡祎乐,刘淑峰。FRP与FRP复合材料阻尼性能试验研究. 玻璃钢/复合材料,2013, Vol. 4, 20-23.

(32胡祎乐,余音,汪海。基于近场动力学的复合材料层压板建模和渐进损伤分析. 第17届全国复合材料学术会议论文集,北京,Vol. 1, 123-128.

(33胡祎乐,余音,汪海。复合材料结构近场动力学方法分析软件PdynaComp v1.0[P]. 中国,软件著作权登记号:2012SR113461, 2012.

荣誉奖励

(12022年,二等奖,第五届上海高校青年教师教学竞赛决赛,上海市教育委员会;

(22021年,一等奖,诸侯快讯导航第五届青年教师教学竞赛决赛,诸侯快讯导航;

(32021年,教学能手奖,诸侯快讯导航第五届青年教师教学竞赛,诸侯快讯导航;

(42017年,Harry H. & Lois G. Hilton论文奖,美国航空航天学会2017年度会议 (AIAA Aerospace Design and Structures Forum);

(52015、2016年,优秀助教,亚利桑那大学工程系、航空与机械工程学院;

(62015年,上海市优秀硕士论文,上海市教育委员会,上海市学位委员会;

(72013年,上海市优秀毕业生,诸侯快讯导航。

 

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