Shimming effect on the mechanical behaviors of composite assembly structures of aircraft

Autor:	Xuande Yue, Ende Ge, Wei Zhang, Ning Han, Yishen Yun, Guoqiang Gao, Luling An
Rok vydání:	2017
Předmět:	020303 mechanical engineering & transports Materials science 0203 mechanical engineering Mechanical Engineering Composite number Aerospace Engineering Mechanical engineering Shim (magnetism) 02 engineering and technology 021001 nanoscience & nanotechnology 0210 nano-technology
Zdroj:	Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 233:851-860
ISSN:	2041-3025 0954-4100
Popis:	The mechanical behaviors of composite assembly structures of aircraft might change due to filling the fit-up gap between two components with liquid shim or laminated shim. In order to investigate the change qualitatively and quantitatively, a kind of implicit nonlinear finite element models are developed, and mixed failure criteria considering the nonlinear shear relationship between composite matrix and fiber, out-of-plane stresses, and buckling of fiber are incorporated into finite element models. And tensile experimental research is also performed to validate the finite element models. Good agreement between the numerical and experimental results builds confidence that the finite element models are effective in predicting the shimming effect. And it is also observed that the mechanical behaviors of composite assembly structures with different filling present obvious differences.
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::ef8959775f389899c3385a22c970cfa8 https://doi.org/10.1177/0954410017740919 Zobrazit plný text záznamu