Zobrazeno 1 - 10
of 11
pro vyhledávání: '"Yuejie Cao"'
Publikováno v:
Metals, Vol 9, Iss 5, p 584 (2019)
The rational pre-stretching can contribute to obtaining better mechanical properties. This paper studies the effect of creep stain, mechanical properties, and microstructures of 7055 alloy under different pre-stretching conditions. The results show t
Externí odkaz:
https://doaj.org/article/f2b14409d17b45fd99ef9347cc1b1f00
Publikováno v:
OAJRC Social Science. 4:18-22
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cbb355bd03ac4d08f51cb1fa8956eab6
https://doi.org/10.26855/oajrcss.2023.02.005
https://doi.org/10.26855/oajrcss.2023.02.005
Publikováno v:
Composite Structures. 316:117046
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b54e2fa64a7941454d5f40b2db6bc4f2
https://doi.org/10.1016/j.compstruct.2023.117046
https://doi.org/10.1016/j.compstruct.2023.117046
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 236:607-622
The decrease of stress amplitude is generally believed as the mechanism of fatigue life enhancement in interference fit joints under cyclic loading for each load cycle. In order to exactly estimate it, a new analytical model was presented. In this mo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::73e2419fba8badce1fd0efc637bc6b76
https://doi.org/10.1177/09544100211016601
https://doi.org/10.1177/09544100211016601
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science. 234:2881-2894
A new mathematical model-based on aging-stress relaxation forming for heterogeneous stiffened panel that is T-welded together is developed. The corresponding theoretical method for calculating its neutral layer positions and forming die shapes in vis
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1234136bd7800ebb35f9e7f789d97e33
https://doi.org/10.1177/0954406220910766
https://doi.org/10.1177/0954406220910766
Publikováno v:
The International Journal of Advanced Manufacturing Technology. 103:3495-3512
A 3D transient computational thermal model is developed to investigate the heat transfer effects arising during friction stir welding (FSW) in dissimilar alloys with a T-joint. Specifically, a dual-heat-source-based mathematic model is derived on the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c0e95403f89b065e3afc30989f185895
https://doi.org/10.1007/s00170-019-03465-z
https://doi.org/10.1007/s00170-019-03465-z
Publikováno v:
Xibei Gongye Daxue Xuebao, Vol 36, Iss 4, Pp 701-708 (2018)
Cold Expansion and Interference Fit are two well-known techniques in hole strengthening, having been widely used in aviation industry. Double cold expansion is a new strengthening process which effectively combined with the two techniques. A modellin
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::2d4311e74864772ab4e429ce9c2b1e26
https://www.jnwpu.org/articles/jnwpu/pdf/2018/04/jnwpu2018364p701.pdf
https://www.jnwpu.org/articles/jnwpu/pdf/2018/04/jnwpu2018364p701.pdf
Publikováno v:
Aerospace Science and Technology. 78:461-470
CFRP/Ti bolted joints are increasingly used in aircraft structures. Optimizing the joint design is vital for overall composite structure designs. Therefore, a progressive damage model was developed for investigating the effects of clearance and inter
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2adc209034cbeae6d8f2252f1f6a3eea
https://doi.org/10.1016/j.ast.2018.04.042
https://doi.org/10.1016/j.ast.2018.04.042
Publikováno v:
Composite Structures. 184:362-371
CFRP/Ti pinned joints are widely applied on main load-bearing structures of aircrafts. Understanding the dynamic behavior of the joints is important for optimal joint designs. Therefore, a dynamic test platform based on electromagnetic loading method
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::64d84eca8f0edfc2e4282e2d6bfd34e9
https://doi.org/10.1016/j.compstruct.2017.09.079
https://doi.org/10.1016/j.compstruct.2017.09.079
Publikováno v:
Composite Structures. 261:113565
Thin-ply laminated composites have recently gained increasing attention in the aerospace engineering field, due to enhanced design possibilities and positive size effects with regard to decreasing ply thickness. In this paper, the mechanical behavior
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::22768fa8a9ec10da0cdf85826f439f64
https://doi.org/10.1016/j.compstruct.2021.113565
https://doi.org/10.1016/j.compstruct.2021.113565