找回密码
 To register

QQ登录

只需一步,快速开始

扫一扫,访问微社区

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

[复制链接]
查看: 27353|回复: 46
发表于 2025-3-21 18:11:46 | 显示全部楼层 |阅读模式
书目名称Riveted Lap Joints in Aircraft Fuselage
副标题Design, Analysis and
编辑Andrzej Skorupa,Malgorzata Skorupa
视频video
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
丛书名称Solid Mechanics and Its Applications
图书封面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
关键词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

书目名称Riveted Lap Joints in Aircraft Fuselage影响因子(影响力)




书目名称Riveted Lap Joints in Aircraft Fuselage影响因子(影响力)学科排名




书目名称Riveted Lap Joints in Aircraft Fuselage网络公开度




书目名称Riveted Lap Joints in Aircraft Fuselage网络公开度学科排名




书目名称Riveted Lap Joints in Aircraft Fuselage被引频次




书目名称Riveted Lap Joints in Aircraft Fuselage被引频次学科排名




书目名称Riveted Lap Joints in Aircraft Fuselage年度引用




书目名称Riveted Lap Joints in Aircraft Fuselage年度引用学科排名




书目名称Riveted Lap Joints in Aircraft Fuselage读者反馈




书目名称Riveted Lap Joints in Aircraft Fuselage读者反馈学科排名




单选投票, 共有 1 人参与投票
 

1票 100.00%

Perfect with Aesthetics

 

0票 0.00%

Better Implies Difficulty

 

0票 0.00%

Good and Satisfactory

 

0票 0.00%

Adverse Performance

 

0票 0.00%

Disdainful Garbage

您所在的用户组没有投票权限
发表于 2025-3-22 00:19:18 | 显示全部楼层
发表于 2025-3-22 02:07:58 | 显示全部楼层
发表于 2025-3-22 06:16:30 | 显示全部楼层
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
发表于 2025-3-22 09:39:30 | 显示全部楼层
发表于 2025-3-22 15:51:02 | 显示全部楼层
https://doi.org/10.1007/978-94-007-4282-6aircraft engineering; aluminium alloys; fatigue; fuselage systems; riveted joints; riveting process; safet
发表于 2025-3-22 18:48:30 | 显示全部楼层
978-94-007-9267-8Springer Science+Business Media Dordrecht 2012
发表于 2025-3-22 23:40:14 | 显示全部楼层
Riveted Lap Joints in Aircraft Fuselage978-94-007-4282-6Series ISSN 0925-0042 Series E-ISSN 2214-7764
发表于 2025-3-23 01:38:51 | 显示全部楼层
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
发表于 2025-3-23 09:27:42 | 显示全部楼层
 关于派博传思  派博传思旗下网站  友情链接
派博传思介绍 公司地理位置 论文服务流程 影响因子官网 SITEMAP 大讲堂 北京大学 Oxford Uni. Harvard Uni.
发展历史沿革 期刊点评 投稿经验总结 SCIENCEGARD IMPACTFACTOR 派博系数 清华大学 Yale Uni. Stanford Uni.
|Archiver|手机版|小黑屋| 派博传思国际 ( 京公网安备110108008328) GMT+8, 2025-6-17 00:28
Copyright © 2001-2015 派博传思   京公网安备110108008328 版权所有 All rights reserved
快速回复 返回顶部 返回列表