首页> 外文会议>Conference of the International Committee on Aeronautical Fatigue and Structural Integrity >Creation and Verification of World's largest K_I-Databases for Multiple Cracks at a Countersunk and Straight-Shank Hole in a Plate subject to Tension, Bending and Pin-Loading
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Creation and Verification of World's largest K_I-Databases for Multiple Cracks at a Countersunk and Straight-Shank Hole in a Plate subject to Tension, Bending and Pin-Loading

机译:在电阻,弯曲和针脚装载的板中埋头和直柄孔的多个裂缝的创建和验证世界上最大的K_I数据库

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The paper describes the results and mathematical-numerical methods used in one multi-year collaboration between the U.S. Air Force's Academy Centre for Aircraft Structural Life Extension, CAStLE and Swedish organisations FOI and BARE developing novel numerical methods for reliable large-scale structural analysis and application of these methods for derivation of the world's largest high-accuracy databases, containing over 180 million K_i(Φ) -graphs all with a relative point wise error less than 10~(-3). The databases will be provided to the engineering community for fatigue crack growth analysis using AFGROW crack growth software or similar. Parts of the methods used in the present paper have earlier been reported at ICAF, ICAS, ASIP and ASTM-meetings [1-6] and in scientific journals [7-11].
机译:本文介绍了美国空军航空器结构寿命延伸,城堡和瑞典组织的一家多年合作中的结果和数学 - 数值方法,CASTLE和瑞典组织FOI和裸露于可靠的大规模结构分析和应用的新型数值方法这些方法的推导方法最大的高精度数据库,其中包含超过180万K_I(φ)-Graphy,其均具有小于10〜(3)的相对点明智误差。使用Afgrow裂缝增长软件或类似,将向工程界提供数据库以进行疲劳裂纹增长分析。本文中使用的部分方法已经在ICAF,ICAS,ASIP和ASTM-overings [1-6]和科学期刊上报告了本文的方法及其在科学期刊[7-11]。

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