Composite Laminate Design for Improved Open-Hole Compression Strength using Non-Standard Ply Angles and Customized Stacking Sequences Characterized by [D] Matrix
Author:
Funder
Boeing
Publisher
Elsevier BV
Subject
Materials Chemistry,Mechanics of Materials,General Materials Science
Reference41 articles.
1. Strength degradation and stress analysis of composite plates with circular, square and rectangular notches using digital image correlation;Khechai;Compos Struct,2018
2. Strength of Composite Laminates Containing Holes and Subjected to Complex Loading Conditions;Ireman;J Compos Mater - J Compos MATER,1997
3. Static Compression Failure of Carbon Fibre T800/924C Composite Plate with a Single Hole;Soutis;J Compos Mater - J Compos MATER,1990
4. Parametric modeling, higher order FEA and experimental investigation of hat-stiffened composite panels;Jin;Compos Struct,2015
5. Boeing 787 Dreamliner;Wagner,2009
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. Improved composite open-hole compression strength and trade-off with manufacturability controlled by stacking sequence effect and non-standard ply angles;Composites Part B: Engineering;2022-01
2. A compact open-hole compression test fixture for composite materials;Composites Part B: Engineering;2021-10
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