Zobrazeno 1 - 7
of 7
pro vyhledávání: '"Lubin Huo"'
Publikováno v:
Chinese Journal of Aeronautics.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::847c564ca68a458b63d90f8f8603f64b
https://doi.org/10.1016/j.cja.2023.01.015
https://doi.org/10.1016/j.cja.2023.01.015
Publikováno v:
Composite Structures, 303
To further investigate the effects of in-plane and out-of-plane stresses on the delamination initiation for composite laminates under out-of-plane loading, this paper reports a joint experimental and numerical study, in which the fully clamped rectan
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::98fc44b08d4c1b4148fb1df46746e0c3
https://doi.org/10.2139/ssrn.4194103
https://doi.org/10.2139/ssrn.4194103
Publikováno v:
SSRN Electronic Journal.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::58a8182be58beed2a670ddae2f6f153f
https://doi.org/10.2139/ssrn.4149408
https://doi.org/10.2139/ssrn.4149408
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:
Journal of Aircraft. Sep2024, Vol. 61 Issue 5, p1490-1500. 11p.