Analysis of Radial Stress Field around Riveted Holes of Single Rivet Panel and Two Way Rolling Re Shaping Strategy
Author:
Affiliation:
1. School of Mechanical Enginnering, Northwestern Polytechnical University,Xi'an,China
Funder
Aeronautical Science Foundation of China
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10193874/10193855/10194177.pdf?arnumber=10194177
Reference7 articles.
1. Numerical and Experimental Investigation of Aircraft Panel Deformations During Riveting Process
2. Modeling and predicting of aeronautical thin-walled sheet metal parts riveting deformation
3. Numerical simulation of residual stress distribution in cold extrusion of fastener holes of aircraft structures;lu;Aeronaut Manuf Technol Beijing,2018
4. Influence of initial fit tolerance and squeeze force on the residual stress in a riveted lap joint
5. Numerical study on predicting and correcting assembly deformation of a large fuselage panel during digital assembly
1.学者识别学者识别
2.学术分析学术分析
3.人才评估人才评估
"同舟云学术"是以全球学者为主线，采集、加工和组织学术论文而形成的新型学术文献查询和分析系统，可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容，当前同舟云学术共收录了国内外主流学术期刊6万余种，收集的期刊论文及会议论文总量共计约1.5亿篇，并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询！咨询电话：010-8811{复制后删除}0370
www.globalauthorid.com
TOP
Copyright © 2019-2024 北京同舟云网络信息技术有限公司 京公网安备11010802033243号 京ICP备18003416号-3