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The failure characteristic of graphite polyetheretherketone (Gr/PEEK) under compression with a centrally located circular discontinuity was investigated through experimentation and a nonlinear ply-by-ply finite element technique. The stacking sequence of the laminates investigated were: [0 °16], [90 °16], [±45 °]4S [0 °/90 °]4S, and [0 °/ ± 45 0°/90 °]2S. In the experimentation, [90 °]16, [0 °/90 °]4S, and [0 °/ ±45 °/90 °]2S laminates, as well as three of the [0 °]16, failed due to a crack that was normal to the loading direction and initiated from the edge of the hole progressing to the outer edges of the specimen. The [±45 °]4S specimens failed to support the load due to an internal crack that originated from the hole's edge and then traveled at an angle of about 42% to the direction of loading. The finite element method used to analytically model the failure of Gr/PEEK accurately modeled the response of the specimens tested experimentally. 相似文献
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Fire Technology - Wildland urban interface (WUI) communities in the Western United States have recently dealt with historic and devastating wildfires year after year. The fires have cost tens of... 相似文献
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