FATIGUE INITIATION AND CRACK GROWTH BEHAVIOUR IN GLARE FROM THE AIRBUS MEGALINER BARREL TEST

机译：空中客车巨木桶测试的眩光疲劳初始化和裂纹增长行为

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The MegaLiner Barrel (MLB) pressure cabin test was part of the Airbus 380 structural fatigue evaluation programme. The test was discontinued after 45,402 simulated flights. Samples were designated for teardown, and the NLR is carrying out teardowns of some GLARE (GLAss Reinforced aluminium laminate) panels. The teardowns include Non-Destructive Inspection (NDI), and some fractographic analyses of detected fatigue cracks. This paper presents fractographic results for a GLARE window area.

机译：MegaLiner机筒（MLB）压力舱测试是空中客车380结构疲劳评估计划的一部分。在进行了45,402次模拟飞行后，测试停止。指定样品进行拆解，并且NLR正在对某些GLARE（玻璃纤维增强铝层压板）面板进行拆解。拆解包括无损检查（NDI），以及对检测到的疲劳裂纹进行的一些分形分析。本文介绍了GLARE窗口区域的分形结果。

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来源
《Congress of the International Council of the Aeronautical Sciences; 20060903-08; Hamburg(DE)》|2006年|P.2440-2445|共6页
会议地点 Hamburg(DE)
作者
R.J.H. Wanhill; T. Hattenberg; P.H. de Haan;
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作者单位

National Aerospace Laboratory NLR, Amsterdam, The Netherlands;

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会议组织
原文格式 PDF
正文语种 eng
中图分类航空;
关键词
fatigue; crack growth; fractography; GLARE;

机译：疲劳;裂纹增长;断口扫描; GLARE;

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1. Fatigue Crack Initiation and Early Growth in GLARE 3 Fiber-metal Laminate Subjected to Mixed Tensile and Bending Loading [J] . A. Chlupová, A. Va?ek, J. Heger Acta polytechnica . 2001,第4a5期

机译：混合拉伸和弯曲载荷作用下GLARE 3纤维金属层压板的疲劳裂纹萌生和早期生长
2. Crack initiation and propagation in air plasma sprayed thermal barrier coatings, testing and mathematical modelling of low cycle fatigue behaviour [J] . Magnus Jinnestrand, Hakan Brodin Materials Science and Engineering. A, Structural Materials . 2004,第1a2期

机译：空气等离子喷涂热障涂层的裂纹萌生和扩展，低循环疲劳行为的测试和数学建模
3. In situ synchrotron ultrasonic fatigue testing device for 3D characterisation of internal crack initiation and growth [J] . Alexandre Messager, Arnaud Junet, Thierry Palin-Luc, Fatigue & Fracture of Engineering Materials & Structures . 2020,第3期

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4. FATIGUE INITIATION AND CRACK GROWTH BEHAVIOUR IN GLARE FROM THE AIRBUS MEGALINER BARREL TEST [C] . R.J.H. Wanhill, T. Hattenberg, P.H. de Haan Congress of the International Council of the Aeronautical Sciences . 2006

机译：空中客车Megaliner桶试验中眩光的疲劳启动和裂纹增长行为
5. A crystal plasticity based methodology for modeling fatigue crack initiation and estimating material coefficients to predict fatigue crack initiation life at micro, nano and macro scales. [D] . Voothaluru, Rohit. 2014

机译：一种基于晶体可塑性的方法，用于建模疲劳裂纹萌生和估算材料系数，以预测微观，纳米和宏观尺度的疲劳裂纹萌生寿命。
6. Fatigue Growth Behaviour of Two Interacting Cracks with Different Crack Offset [O] . Huijin Jin, Bing Cui, Ling Mao 2019

机译：具有不同裂纹偏移量的两个相互作用裂纹的疲劳生长行为
7. Fatigue initiation and crack growth behaviour in GLARE from the Airbus MegaLiner Barrel test [O] . Wanhill R.J.H., Hattenberg T., Haan P.H. de 2006

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8. Open Hole Multilayer Fatigue Crack Growth in Glare Under Combined Tension Bending [R] . Randell, C. E. , Schijve, J. , van der Zwaag, S. 2005

机译：复合拉伸弯曲下眩光中裸眼多层疲劳裂纹扩展

FATIGUE INITIATION AND CRACK GROWTH BEHAVIOUR IN GLARE FROM THE AIRBUS MEGALINER BARREL TEST

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