Tel:+86-10-62773424

E-mail address:gedy@tsinghua.edu.cn

Education background

l Ph.D., Solid Mechanics, Northwestern Polytechnical University, Xi’an, Shaanxi, China, 1999

l M.S., Solid Mechanics, Northwestern Polytechnical University, Xi’an, Shaanxi, China, 1996

l B.S., Aircraft StructureDesign, Northwestern Polytechnical University, Xi’an, Shaanxi, China, 1993

Experience

l Postdoctor, Department of Engineering Mechanics, Tsinghua University,

1999.5-2001.6

l Lecture, Department of Engineering Mechanics, Tsinghua University, 2001.7-2004.12

l Associate Professor, School of Aerospace Engineering, Tsinghua University, 2005.1 -date

Areas of Research Interests/ Research Projects

Impact Dynamic Mechanics;Composite Mechanics ;Experimental Mechanics; Composite Structure Design

Recent publications

[1] Dang Zhangchi,Yan Li, Gan Xuedong, Ge, Dongyun, Prediction on the fatigue behavior of Ti-6Al-4V components treated by split sleeve cold expansion with different final reaming depth,EUROPEAN JOURNAL OF MECHANICS A-SOLID, Volume 111(2025):105578

[2] Du Xuzhen ,Ge Dongyun, Dang, Zhangchi, Wang, Xiangming, Rapid aerodynamic estimation of annular wings based on multiple linear regression, AEROSPACE SCIENCE AND TECHNOLOGY, Volume 158(2024):109887

[3] Dang Zhangchi,Peng Yehao, Yang Rongjuan ,Yan Li, Gan, Xuedong, Ge Dongyun. Experimental study on the effect of reaming on the fatigue life of split-sleeve cold-expanded Ti-6Al-4V alloy components,INTERNATIONAL JOURNAL OF FATIGUE, Volume 188(2024): 108521

[4] Liu, Y ; Chen, JS ; Hu, CH ; Ma, Y; Ge, DY. Vision-Based Method for Automatic Quantification of Parkinsonian Bradykinesia. IEEE TRANSACTIONS ON NEURAL SYSTEMS AND REHABILITATION ENGINEERING. Volume27 (10)2019, Page1952-1961

[5] He Boling,Ge Dongyun, Dynamic analysis of single-lap, adhesively bonded composite-titanium joints subjected to solid projectile impact, Journal of Adhesion science and Technology, Volume 32 (11), 2018, Pages1176-1199, ISSN: 0169-4243.

[6] He, Boling; Ge, Dongyun, Dynamic strength of adhesively bonded composite joints with similar and dissimilar assembled adherends.Journal of Reinforced Plastics and composites. Volume 36 (23), Pages 1683-1692, Dec 2017, ISSN: 0731-6844

[7] He, Boling; Ge, Dongyun, Coupled continuum damage mechanics and failure envelope method for failure prediction of composite multi-bolt joints . Journal of Reinforced Plastics and composites, Volume: 36(8), April 2017, Pages: 563-578 ,ISSN: 0731-6844

[8] Dongyun Ge, Yuming Mo, Boling He, Yiting Wu, Xuzhen Du, Experimental and numerical investigation of stiffened composite curved panel under shear and in-plane bending, Composite Structures, Volume 137, March 2016, Pages 185-195, ISSN 0263-8223

[9] Yuming Mo, Dongyun Ge, Boling He, Experiment and optimization of the hat-stringer-stiffened composite panels under axial compression, Composites Part B: Engineering, Volume 84, January 2016, Pages 285-293, ISSN 1359-8368

[10] Yuming Mo, Dongyun Ge, Jiangfan Zhou, Experiment and analysis of hat-stringer-stiffened composite curved panels under axial compression, Composite Structures, Volume 123, May 2015, Pages 150-160, ISSN 0263-8223

[11] Wu Yiting, GE Dongyun, LI Chen, Dynamic compressive mechanical properties of carbon fiber laminates under hygrothermal environment, Acta Materiae Compositae Sinica, 2016.2

[12] Dongyun Ge, Yuming Mo, Boling He, Xuzhen Du,, Experiment and theoretical load prediction of hat-stiffened composite panel under axial compression, 2016

[13] Boling He,Dongyun Ge, Yuming Mo, Xuzhen Du, Experiment and engineering approach for double-lap, single-bolt joint in T800 carbon/epoxy laminate,Acta Materiae Compositae Sinica, 2016