Analysing thermally induced macro-scale residual stresses in tailored morphing composite laminates

Author:

Telford R.,Katnam K.B.,Young T.M.

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference24 articles.

1. Mechanics of composite materials;Jones,1998

2. Hertz, TJ, Shirk MH, Ricketts RH, Weisshaar TA. Aeroelastic tailoring with composites applied to forward swept wings. Air force wright aeronautical labs wright-patterson AFB OH; 1981.

3. Calculations of the room-temperature shapes of unsymmetric laminates;Hyer;J Compos Mater,1981

4. A concept for airfoil-like active bi-stable twisting structures;Schultz;J Intell Mater Syst Struct,2008

5. Falcão L, Gomes A, Suleman A. Morphing wingtip devices based on multistable composites. In: RTO-MP-AVT-168, NATO research and technology organisation applied vehicle technology panel symposium on morphing vehicles, Evora, Portugal; 2009. p. 1–12.

同舟云学术

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