Energo-Mechanical Evaluation of Damage Growth and Fracture Initiation in Aviation Composite Structures

被引：7

作者：

Kersiene, Neringa ^{[1
]}

Raslavicius, Laurencas ^{[2
]}

Kersys, Arturas ^{[2
]}

Kazys, Rymantas ^{[3
]}

Zukauskas, Egidijus ^{[3
]}

机构：

[1] Kaunas Univ Technol, Dept Mech Engn, LT-51424 Kaunas, Lithuania

[2] Kaunas Univ Technol, Dept Transport Engn, Studentu Str 59, LT-51424 Kaunas, Lithuania

[3] Kaunas Univ Technol, Prof Kazimieras Barauskas Ultrasound Res Inst, LT-51424 Kaunas, Lithuania

来源：

POLYMER-PLASTICS TECHNOLOGY AND ENGINEERING | 2016年 / 55卷 / 11期

关键词：

Aviation composites; CFRP composites; GFRP composites; minimal visual detectability damage; CARBON-FIBER; GLASS; SPECIMENS; MATRIX;

D O I：

10.1080/03602559.2015.1132452

中图分类号：

O63 [高分子化学（高聚物）];

学科分类号：

070305 ; 080501 ; 081704 ;

摘要：

The aim of the present paper is to (1) highlight the results of laboratory damage detection and monitoring in the aviation composite materials, during a mechanical testing constituted of multiple loadings, and (2) obtain a detailed understanding of damage evolution of composite specimens with regard to impact energy. Woven 12-ply glass fiber and 16-ply carbon fiber-reinforced epoxy composites (GFRP 92 125/L285/287 and CFRP 98 131/L285/287) were used as less studied subjects in research. This study explored the resistance to cracking and delamination of glass and carbon fiber laminates with the same resin system under low-load conditions. [GRAPHICS]

引用

页码：1137 / 1144

页数：8

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