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Titlebook: Structural Connections for Lightweight Metallic Structures; Pedro M.G.P. Moreira,Lucas F. M. Silva,Paulo M.S.T Book 2012 Springer-Verlag B

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发表于 2025-3-21 19:49:30 | 显示全部楼层 |阅读模式
书目名称Structural Connections for Lightweight Metallic Structures
编辑Pedro M.G.P. Moreira,Lucas F. M. Silva,Paulo M.S.T
视频video
概述Presents state-of-the-art discussions of aspects and processes for connections in lightweight structures.Dedicates a great interest to welding.Appeals to researchers as well as to engineers involved i
丛书名称Advanced Structured Materials
图书封面Titlebook: Structural Connections for Lightweight Metallic Structures;  Pedro M.G.P. Moreira,Lucas F. M. Silva,Paulo M.S.T Book 2012 Springer-Verlag B
描述Increasing concern with fuel consumption leads to widespread interest in lightweight structures for transportation vehicles. Several competing technologies are available for the structural connections of these structures, namely welding, mechanical fastening / riveting, and adhesive technologies. Arranged in a single volume, this work is to presents state-of-the-art discussions of those aspects and processes presenting greater novelty whilst simultaneously keeping wide applicability potential and interest. The topics chosen have the common feature of being of currently applied in lightweight structures, and one of the characteristics of this work is bringing together relevant state-of-the-art information usually presented in separate publications specializing in a single technology. The book provides discussions and examples of concrete applications, so that it appeals to researchers and designers and engineers involved in the design and fabrication of lightweight structures.
出版日期Book 2012
版次1
doihttps://doi.org/10.1007/978-3-642-18187-0
isbn_softcover978-3-642-42675-9
isbn_ebook978-3-642-18187-0Series ISSN 1869-8433 Series E-ISSN 1869-8441
issn_series 1869-8433
copyrightSpringer-Verlag Berlin Heidelberg 2012
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发表于 2025-3-21 20:47:45 | 显示全部楼层
Damage Tolerance of Aircraft Panels Taking into Account Residual Stress,The present chapter seeks to summarize the ideas of damage tolerance of aircraft panels, keeping in mind the effect of residual stresses. First concepts and techniques are briefly reviewed, and afterwards their application to experimental work is discussed.
发表于 2025-3-22 04:13:32 | 显示全部楼层
Pedro M.G.P. Moreira,Lucas F. M. Silva,Paulo M.S.TPresents state-of-the-art discussions of aspects and processes for connections in lightweight structures.Dedicates a great interest to welding.Appeals to researchers as well as to engineers involved i
发表于 2025-3-22 05:04:50 | 显示全部楼层
978-3-642-42675-9Springer-Verlag Berlin Heidelberg 2012
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发表于 2025-3-22 19:39:36 | 显示全部楼层
FSW of Lap and T-Joints,cess mechanics and the effectiveness of the final part. Furthermore, in the FSW of T-parts a proper clamping fixture is needed in order to fix the stringer during the process; such fixture is characterized by two radii, one for each side of the joints, corresponding to the radii between skin and str
发表于 2025-3-22 23:39:51 | 显示全部楼层
Lightweight Stiffened Panels Fabricated Using Emerging Fabrication Technologies: Fatigue Behaviour,s (.) of 0.1 and 0.5. It was found that welded panels presented longer lives up to rupture. This result is associated to the residual stress fields existing in the welded panels, and also to the location of the initial artificial defect, placed in the skin midway the specimen’s two stiffeners.
发表于 2025-3-23 04:12:25 | 显示全部楼层
Materials Selection for Airframes: Assessment Based on the Specific Fatigue Behavior,toughness and better damage tolerance in the presence of defects. In order to improve the material selection and the comparison of airframe materials, this chapter presents an weight assessment based on the specific weight for different damage scenarios taking into account their damage tolerant prop
发表于 2025-3-23 09:00:56 | 显示全部楼层
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