Finite strip analysis of singly curved skin-stringer structures
Author:
Publisher
Elsevier BV
Subject
Mechanical Engineering,Mechanics of Materials,Acoustics and Ultrasonics,Condensed Matter Physics
Reference17 articles.
1. The response of a typical aircraft structure to jet noise;Clarkson;Journal of the Royal Aeronautical Society,1962
2. Finite strip analysis of flat skin-stringer structures;Petyt;Journal of Sound and Vibration,1977
3. Free vibrations of continous skin-stringer panels;Lin;Journal of Applied Mechanics,1960
4. A brief survey of transfer matrix techniques with special reference to the analysis of aircraft panels;Lin;Journal of Sound and Vibration,1969
5. The analysis of curved multi-span structures;Henderson;Journal of Sound and Vibration,1971
Cited by 9 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Use of the finite strip method in predicting the behaviour of composite laminated structures;Composite Structures;2002-07
2. FREE VIBRATION ANALYSIS OF AN ORTHOGONALLY SUPPORTED MULTI-SPAN CURVED PANEL;Journal of Sound and Vibration;2001-03
3. Free Vibration Analysis of Symmetrical Cylindrical Honeycomb Panels by Using the Finite Strip Method;Journal of Vibration and Control;1997-01
4. Finite Element Free Vibration Analysis of Stiffened Shells;Journal of Sound and Vibration;1994-04
5. The buckling performance of composite stiffened panel structures subjected to combined in-plane compression and shear loading;Composite Structures;1994-01
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