Brittle Matrix Composites, Год журнала: 1986, Номер unknown, С. 227 - 240
Опубликована: Янв. 1, 1986
Язык: Английский
Brittle Matrix Composites, Год журнала: 1986, Номер unknown, С. 227 - 240
Опубликована: Янв. 1, 1986
Язык: Английский
Composites, Год журнала: 1994, Номер 25(9), С. 863 - 868
Опубликована: Окт. 1, 1994
Язык: Английский
Процитировано
104European Journal of Mechanics - A/Solids, Год журнала: 2018, Номер 73, С. 224 - 234
Опубликована: Сен. 16, 2018
Язык: Английский
Процитировано
37International Journal of Mechanical Sciences, Год журнала: 2024, Номер 274, С. 109222 - 109222
Опубликована: Март 30, 2024
Язык: Английский
Процитировано
3Journal of Composite Materials, Год журнала: 1992, Номер 26(3), С. 405 - 431
Опубликована: Март 1, 1992
Solidification, under nonisothermal conditions and pressure gradients present during processing, is shown to be a major contributor the generation of internal stresses in advanced composite materials. These may amplified materials with significant anisotropic characteristics. Using process simulated lami nate (PSL) technique, methodology was developed for evaluation residual stress distributions induced processing. The PSL contained separation films placed between certain layers laminate, enabling laminate after ing. strain gage attached distribution over calculated. detached laminates served as specimens through-thickness morphological property distributions. direct relationship tween investigation releasing phenomena such voids, microcracks and/or fiber buckling important complete pro cess effects. Different techniques were presented compared pressformed 40-ply unidirectional composites cooled at rate 20-50°C/s. A pronounced skin-core profile observed PEEK/AS4 compos ites demonstrating compressive surface tensile center laminate.
Язык: Английский
Процитировано
57Solid mechanics and its applications, Год журнала: 1992, Номер unknown, С. 75 - 167
Опубликована: Янв. 1, 1992
Язык: Английский
Процитировано
47Composite Structures, Год журнала: 2011, Номер 94(3), С. 1155 - 1164
Опубликована: Окт. 24, 2011
Язык: Английский
Процитировано
33Composite Structures, Год журнала: 1993, Номер 25(1-4), С. 305 - 312
Опубликована: Янв. 1, 1993
Язык: Английский
Процитировано
44Journal of Composite Materials, Год журнала: 2014, Номер 49(12), С. 1513 - 1524
Опубликована: Май 22, 2014
Three-dimensional fabric composites have evolved as an attractive structural material for multi-directional load bearing and impact application. However, research on prediction of their behavior before being fabricated is inadequate. This article reports a two-step modeling approach predicting the effective mechanical properties three-dimensional carbon fiber-reinforced composites. In step one, micro-heterostructural were represented by microscale cylindrical, square, or hexagonal prismatic representative volume elements, containing long fiber surrounded polymer matrix, taking into account transversely isotropic fibers. The each element extracted from results uniaxial tensile, lateral expansion, transverse shear tests, using appropriately derived formulae, averaged equivalent micro-heterostructures. two, composite unit cell was finite model, orientations architecture. A orthogonal epoxy selected case study material. overall orthotropic predicted conducting tensile tests cell. show that Young’s moduli in oriented directions are significantly higher than those matrix. shearing cross-sections even much along longitudinal direction. Carbon can improve stability lowering Poisson’s ratios compared with validated experimental tests.
Язык: Английский
Процитировано
24Progress in Organic Coatings, Год журнала: 2014, Номер 78, С. 73 - 82
Опубликована: Ноя. 4, 2014
Язык: Английский
Процитировано
22Polymer Composites, Год журнала: 2009, Номер 31(5), С. 847 - 857
Опубликована: Апрель 20, 2009
Abstract The through‐thickness thermal conductivity of polymer composite molds has a strong effect on out‐of‐autoclave manufacturing operations. Limited and variability data is available for composites made from carbon fibers that are widely used in mold aircraft construction. This article presents in‐plane structural fiber three types reinforcements. Variability quantified all cases. Techniques the predictive modeling transverse assessed. Effects variations model geometry quantified. Conclusive observations recommendations techniques appropriate different reinforcements made. POLYM. COMPOS., 2010. © 2009 Society Plastics Engineers
Язык: Английский
Процитировано
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