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Titlebook: Riveted Lap Joints in Aircraft Fuselage; Design, Analysis and Andrzej Skorupa,Malgorzata Skorupa Book 2012 Springer Science+Business Media

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發(fā)表于 2025-3-21 18:11:46 | 只看該作者 |倒序瀏覽 |閱讀模式
書目名稱Riveted Lap Joints in Aircraft Fuselage
副標題Design, Analysis and
編輯Andrzej Skorupa,Malgorzata Skorupa
視頻videohttp://file.papertrans.cn/831/830899/830899.mp4
概述Provides help in rational planning of experiments on riveted lap joints in aircraft fuselage.Provides essential information for safe in-service operation of aircrafts.Includes 200 figures
叢書名稱Solid Mechanics and Its Applications
圖書封面Titlebook: Riveted Lap Joints in Aircraft Fuselage; Design, Analysis and Andrzej Skorupa,Malgorzata Skorupa Book 2012 Springer Science+Business Media
描述.Fatigue of the pressurized fuselages of transport aircraft is a significant problem all builders and users of aircraft have to cope with for reasons associated with assuring a sufficient lifetime and safety, and formulating adequate inspection procedures. These aspects are all addressed in various formal protocols for creating and maintaining airworthiness, including damage tolerance considerations. In most transport aircraft, fatigue occurs in lap joints, sometimes leading to circumstances that threaten safety in critical ways. The problem of fatigue of lap joints has been considerably enlarged by the goal of extending aircraft lifetimes. .??????????? .Fatigue of riveted lap joints between aluminium alloy sheets, typical of the pressurized aircraft fuselage, is the major topic of the present book. The richly illustrated and well-structured chapters treat subjects such as: structural design solutions and loading conditions for fuselage skin joints; relevance of laboratory test results for simple lap joint specimens to riveted joints in a real structure; effect of various production and design related variables on the riveted joint fatigue behaviour; analytical and experimental res
出版日期Book 2012
關鍵詞aircraft engineering; aluminium alloys; fatigue; fuselage systems; riveted joints; riveting process; safet
版次1
doihttps://doi.org/10.1007/978-94-007-4282-6
isbn_softcover978-94-007-9267-8
isbn_ebook978-94-007-4282-6Series ISSN 0925-0042 Series E-ISSN 2214-7764
issn_series 0925-0042
copyrightSpringer Science+Business Media Dordrecht 2012
The information of publication is updating

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Andrzej Skorupa,Malgorzata SkorupaProvides help in rational planning of experiments on riveted lap joints in aircraft fuselage.Provides essential information for safe in-service operation of aircrafts.Includes 200 figures
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發(fā)表于 2025-3-22 09:39:30 | 只看該作者
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https://doi.org/10.1007/978-94-007-4282-6aircraft engineering; aluminium alloys; fatigue; fuselage systems; riveted joints; riveting process; safet
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發(fā)表于 2025-3-22 18:48:30 | 只看該作者
978-94-007-9267-8Springer Science+Business Media Dordrecht 2012
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Riveted Lap Joints in Aircraft Fuselage978-94-007-4282-6Series ISSN 0925-0042 Series E-ISSN 2214-7764
9#
發(fā)表于 2025-3-23 01:38:51 | 只看該作者
Riveted Lap Joints in a Pressurized Aircraft Fuselage,this situation takes place between the tear straps, a segment of the skin bends back creating an opening. This phenomenon, described as “flapping”, is a safe failure mode that limits the failure to the affected bay only (Kosai et al. 1992). A thin skin will flap more easily than a thick one (Maclin
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發(fā)表于 2025-3-23 09:27:42 | 只看該作者
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