Zobrazeno 1 - 10
of 15
pro vyhledávání: '"Senqing Jia"'
Publikováno v:
Applied Sciences, Vol 9, Iss 6, p 1168 (2019)
The blow-off impulse effect of a composite reinforced panel subjected to lightning strike is studied combing electric-thermal coupling with explicit dynamic methods. A finite element model of a composite reinforced panel is established under the acti
Externí odkaz:
https://doaj.org/article/7aa1f8b303a24b4c8d1da319f807e83f
Publikováno v:
Fibers and Polymers. 22:1718-1730
The aim of this study is to characterize and assess failure modes and the effect of structural parameters of honeycomb sandwich structure. The semi-finite element model of honeycomb sandwich structure under four-point bending load is established by a
Lightning Damage Testing of Aircraft Composite-Reinforced Panels and Its Metal Protection Structures
Publikováno v:
Applied Sciences, Vol 8, Iss 10, p 1791 (2018)
In order to investigate the lightning damage behavior of an aircraft carbon fiber/epoxy composite-reinforced panel and its protection structures, four types of panels were selected to carry out a lightning experiment. Panels were without protection,
Externí odkaz:
https://doaj.org/article/b17976e96edc4e6ca7752bea6c7e2084
Publikováno v:
Mathematical Problems in Engineering, Vol 2020 (2020)
The influence of soil heterogeneity is studied on the bending of circular thin plates using two modified Vlasov foundation models. The model parameters are determined reasonably using an iterative technique. According to the principle of minimum pote
Publikováno v:
Composite Structures. 258:113421
SHPB system was widely used to investigate the dynamical mechanical performances of materials. In this study, the mechanical performances of T700/BA9916 composite material were investigated through experiment and numerical simulation. The true stress
Publikováno v:
European Journal of Mechanics - A/Solids. 85:104141
Lightning strikes generate large amounts of energy. Thus, composite structures subjected to lightning strikes undergo significant physicochemical changes. In this study, the thermal shock damage and three-phase transition of a composite reinforced pa
Publikováno v:
Applied Composite Materials. 23:953-972
In order to assess various design concepts and choose a kind of covering cap design scheme which can meet the requirements of airworthiness standard and ensure the safety of fuel tank. Using finite element software ANSYS/LS- DYNA, the impact process
Publikováno v:
Wang, Y, Wang, F, Jia, S & Yue, Z 2017, ' Experimental and numerical studies on the stability behavior of composite panels stiffened by tilting hat-stringers ', Composite Structures, vol. 174, pp. 187-195 . https://doi.org/10.1016/j.compstruct.2017.04.039
Due to the existence of sweepback angle of aircraft, the stringers of the stiffened panels in some parts may be declined instead parallel to the boundary. The paper deals with stability experiment investigation on the stiffened composite panels with
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::9d5d6a15a29ec37e106544169a0b14a3
https://research-information.bris.ac.uk/en/publications/6746d628-a9ea-45d3-b874-36047a58aafc
https://research-information.bris.ac.uk/en/publications/6746d628-a9ea-45d3-b874-36047a58aafc
Autor:
Jia, Senqing1 (AUTHOR), Wang, Fusheng1 (AUTHOR) fswang@nwpu.edu.cn, Yu, Lingjun2 (AUTHOR), Wei, Zheng1 (AUTHOR), Xu, Bin1 (AUTHOR)
Publikováno v:
Science Progress. 9/27/2019, Vol. 103 Issue 1, p1-18. 18p.
Publikováno v:
Transactions of the Indian Institute of Metals; Oct2022, Vol. 75 Issue 10, p2507-2516, 10p