Behavior of plain woven textile composites subjected to uniaxial tensile loading-Reference-Cited by-同舟云学术

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Behavior of plain woven textile composites subjected to uniaxial tensile loading

Published:2001-06-11 Issue: Volume: Page:
ISSN:
Container-title:19th AIAA Applied Aerodynamics Conference
language:
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Author:

Kelkar Ajit¹,Shenoy Sunil¹,Whitcomb John²,Tang Xiaodong²

Affiliation:

1. North Carolina A & T State Univ., Greensboro

2. Texas A & M Univ., College Station

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2001-1510

Reference5 articles.

1. Chapman, C.D.,1997, "Prediction ofModuli and Strength of Woven Carbon-Carbon Composites Using Object-Oriented Finite Element Analysis," Ph.D Dissertation,Department of Aerospace Engineering, TexasA&MUniversity,College Station,Texas.

2. 12-1

3. Load= 8.5-10.5Kips

Cited by 2 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. Performance evaluation of VARTM manufactured textile composites for the aerospace and defense applications;Materials Science and Engineering: B;2006-07

2. Finite element analyses and simulations of manufacturing processes of composites and their mechanical properties: a bibliography (1985–2003);Computational Materials Science;2004-11

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