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Titlebook: ICAF 2011 Structural Integrity: Influence of Efficiency and Green Imperatives; Proceedings of the 2 Jerzy Komorowski Conference proceedings

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发表于 2025-3-21 16:27:49 | 显示全部楼层 |阅读模式
书目名称ICAF 2011 Structural Integrity: Influence of Efficiency and Green Imperatives
副标题Proceedings of the 2
编辑Jerzy Komorowski
视频videohttp://file.papertrans.cn/461/460073/460073.mp4
概述ICAF Symposium has a history of being a location for presentation of significant papers on aeronautical fatigue design practices.Bi-annual update on the state of the art for aeronautical design and en
图书封面Titlebook: ICAF 2011 Structural Integrity: Influence of Efficiency and Green Imperatives; Proceedings of the 2 Jerzy Komorowski Conference proceedings
描述Proceedings of the 26th Symposium of the International Committee on Aeronautical Fatigue are a widely referenced summary of advances in aeronautical design against fatigue. This is a bi-annual event and the proceedings have been published in book form for over 35 years.
出版日期Conference proceedings 2011
关键词Aeronautical; Aircraft; Damage Tolerance; Durability; Fatigue; Engineering Economics; quality control, rel
版次1
doihttps://doi.org/10.1007/978-94-007-1664-3
isbn_softcover978-94-017-7882-4
isbn_ebook978-94-007-1664-3
copyrightSpringer Netherlands 2011
The information of publication is updating

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Fatigue Damage Behavior of Glass/Epoxy Composites Using Carbon Nanotubes as Sensorsred with the strain changes measured by strain gages. It is found that the changes in electrical resistance are more sensitive to the degradation in the composite laminate as compared to strain gauges. This technique may be used to provide in-situ monitoring of damages in composites.
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re a widely referenced summary of advances in aeronautical design against fatigue. This is a bi-annual event and the proceedings have been published in book form for over 35 years.978-94-017-7882-4978-94-007-1664-3
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pdate on the state of the art for aeronautical design and enProceedings of the 26th Symposium of the International Committee on Aeronautical Fatigue are a widely referenced summary of advances in aeronautical design against fatigue. This is a bi-annual event and the proceedings have been published i
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Potential of CFRP Used for Light Weight Structures: Some Experimental Resultslus, compressive strength and inter-fibre failure for tension are presented..The second topic is structural testing related to curved fuselage panel testing. A new approach to increase capabilities of that technology is presented.
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Formation of a Metal Coating by Means of Friction Stir Processing a Fe-Ni and Fe-Cu diffusion systems in a structural materials. Verification of the presented considerations was carried out for adhesive nickel or copper coatings on S235JR and S355JR low alloyed steels.
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Modelling of Continuing Damage for Damage Tolerance Analysismpared to the improved approach. For the tested cases, the continuing damage sizes calculated using the simplified approach were underestimated by up to 24 times and the fatigue lives were overestimated by up to 1.4 times.
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