Failure Mechanisms inCompression-Loaded Composite Laminates Containing Open and Filled Holes

Adam J. Sawicki; Pierre J. Minguet

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Failure Mechanisms inCompression-Loaded Composite Laminates Containing Open and Filled Holes

机译：开孔和填孔的受压复合材料层合板的破坏机理

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Filled hole-based compression allowable strengths for carbon/epoxy laminates are not widely used in airframe design, due to a lack of understanding of geometry-related effects and failure mechanisms.

机译：由于缺乏对几何相关影响和破坏机理的了解，碳/环氧树脂层压板的基于填充孔的压缩容许强度并未广泛用于飞机机身设计中。

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《Journal of Reinforced Plastics and Composites》 |1999年第18期|共21页
作者
Adam J. Sawicki; Pierre J. Minguet;
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正文语种 eng
中图分类增强塑料、填充塑料;工程材料学;
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1. Failure Mechanisms inCompression-Loaded Composite Laminates Containing Open and Filled Holes [J] . Adam J. Sawicki, Pierre J. Minguet Journal of Reinforced Plastics and Composites . 1999,第18期

机译：开孔和填孔的受压复合材料层合板的破坏机理
2. Open hole and filled hole progressive damage and failure analysis of composite laminates with a countersunk hole [J] . Joseph Ashith P. K., Davidson Paul, Waas Anthony M. Composite Structures . 2018,第NOVa期

机译：带埋头孔的复合材料层压板的裸眼和实孔渐进式破坏和破坏分析
3. On failure mechanisms of composite laminates with an open hole subjected to compressive load [J] . H. Suemasu, H. Takahashi, T. Ishikawa Composites Science and Technology . 2006,第5期

机译：开孔复合材料层合板在压缩载荷作用下的破坏机理
4. Intra-Inter Crack Band Model (I2CBM) as a Prediction Tool for Open Hole and Filled Hole Failure Analysis of Composite [C] . ASHITH P. K. JOSEPH, PAUL DAVIDSON, ANTHONY M. WAAS American Society for Composites technical conference;American Society for Composites . 2017

机译：内部裂缝带模型（I2CBM）作为复合材料裸眼和实心孔破坏分析的预测工具
5. Failure mechanisms of notched laminated composites under compressive loading at room and elevated temperature. [D] . Ahn, Jung Hyun. 1999

机译：缺口层压复合材料在室温和高温下的压缩载荷下的破坏机理。
6. Elasto-Plastic Mechanical Properties and Failure Mechanism of Innovative Ti-(SiCf/Al3Ti) Laminated Composites for Sphere-Plane Contact at the Early Stage of Penetration Process [O] . Jingchuan Liu, Lan Zhang, Fengchun Jiang, 2018

机译：新型Ti-（SiCf / Al3Ti）层状复合材料在球-面接触早期的弹塑性力学性能和破坏机理
7. Experimental analysis of failures in filled hole compression tests of carbon/epoxy laminate [O] . B. Castanié, S. Crézé, J.J. Barrau, 2010

机译：碳/环氧树脂层压填充孔压缩试验中的故障试验分析
8. Compression strength failure mechanisms in unidirectional composite laminates containing a hole [R] . Johnson, Eric R. 1993

机译：含孔的单向复合材料层压板的压缩强度破坏机理

Failure Mechanisms inCompression-Loaded Composite Laminates Containing Open and Filled Holes

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