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合成材料:力学,计算和应用

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ISSN 打印: 2152-2057

ISSN 在线: 2152-2073

The Impact Factor measures the average number of citations received in a particular year by papers published in the journal during the two preceding years. 2017 Journal Citation Reports (Clarivate Analytics, 2018) IF: 0.2 To calculate the five year Impact Factor, citations are counted in 2017 to the previous five years and divided by the source items published in the previous five years. 2017 Journal Citation Reports (Clarivate Analytics, 2018) 5-Year IF: 0.3 The Eigenfactor score, developed by Jevin West and Carl Bergstrom at the University of Washington, is a rating of the total importance of a scientific journal. Journals are rated according to the number of incoming citations, with citations from highly ranked journals weighted to make a larger contribution to the eigenfactor than those from poorly ranked journals. Eigenfactor: 0.00004 The Journal Citation Indicator (JCI) is a single measurement of the field-normalized citation impact of journals in the Web of Science Core Collection across disciplines. The key words here are that the metric is normalized and cross-disciplinary. JCI: 0.08 SJR: 0.153 SNIP: 0.178 CiteScore™:: 1 H-Index: 12

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EFFECT OF HOLE-NOTCH ON THE TENSILE AND COMPRESSIVE BEHAVIOR OF CARBON−EPOXY COMPOSITE LAMINATES

卷 5, 册 4, 2014, pp. 305-317
DOI: 10.1615/CompMechComputApplIntJ.v5.i4.30
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摘要

The high-performance carbon fiber-reinforced epoxy composites are promising replacements for many conventional materials used in aerospace structures. The effect of hole-notch on the mechanical properties of composites is deleterious and thus vital to the study. The carbon-epoxy composite laminates were produced by stacking and soaking carbon fabric layers with epoxy resin and curing them in a hot press. To determine the effect of hole-notch, composite specimens with and without hole-notch were tested under tensile and compressive loads. Fracture surfaces obtained after tests were examined by a scanning electron microscope. Significant features were observed in the resin, fiber, and especially on their interface, which revealed the possible failure mechanisms of hole-notched composites under tensile and compressive loading.

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