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Titlebook: Damage Growth in Aerospace Composites; Aniello Riccio Book 2015 Springer International Publishing Switzerland 2015 Aerospace Composite Mat

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發(fā)表于 2025-3-21 18:47:40 | 只看該作者 |倒序?yàn)g覽 |閱讀模式
書目名稱Damage Growth in Aerospace Composites
編輯Aniello Riccio
視頻videohttp://file.papertrans.cn/261/260298/260298.mp4
概述Introduces novel numerical approaches for simulation of damage evolution in aerospace composites.Provides a state-of-the-art evaluation of European research projects.Presents collaborative activities
叢書名稱Springer Aerospace Technology
圖書封面Titlebook: Damage Growth in Aerospace Composites;  Aniello Riccio Book 2015 Springer International Publishing Switzerland 2015 Aerospace Composite Mat
描述This book presents novel methods for the simulation of damage evolution in aerospace composites that will assist in predicting damage onset and growth and thus foster less conservative designs which realize the promised economic benefits of composite materials. The presented integrated numerical/experimental methodologies are capable of taking into account the presence of damage and its evolution in composite structures from the early phases of the design (conceptual design) through to the detailed finite element method analysis and verification phase. The book is based on the GARTEUR Research Project AG-32, which ran from 2007 to 2012, and documents the main results of that project. In addition, the state of the art in European projects on damage evolution in composites is reviewed. While the high specific strength and stiffness of composite materials make them suitable for aerospace structures, their sensitivity to damage means that designing with composites is a challenging task. The new approaches described here will prove invaluable in meeting that challenge.
出版日期Book 2015
關(guān)鍵詞Aerospace Composite Materials; Composites‘ Damage Mechanisms; Damage Tolerant Design; Delamination Grow
版次1
doihttps://doi.org/10.1007/978-3-319-04004-2
isbn_softcover978-3-319-38163-3
isbn_ebook978-3-319-04004-2Series ISSN 1869-1730 Series E-ISSN 1869-1749
issn_series 1869-1730
copyrightSpringer International Publishing Switzerland 2015
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Book 2015 and thus foster less conservative designs which realize the promised economic benefits of composite materials. The presented integrated numerical/experimental methodologies are capable of taking into account the presence of damage and its evolution in composite structures from the early phases of t
地板
發(fā)表于 2025-3-22 05:52:26 | 只看該作者
Dara Ramalingam,Raymond J. Adamsf delaminated area to fatigue cycles. The proposed algorithm adopts Paris Law formulation based propagation criterion which can take into account the local damage accumulation along the delamination front.
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Seda U?urlu,Ba?ar ?ztay?i,Cengiz Kahramanre composite structure. These interactions can have a relevant role in particular for delaminated composite plates under compression. In this chapter, integrated numerical methodologies, considering simultaneously the presence of different damage mechanisms in composites, are presented.
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