Boundary element analysis for damage tolerance assessment of aircraft panels-Reference-Cited by-同舟云学术

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Boundary element analysis for damage tolerance assessment of aircraft panels

Published:2002 Issue:4/5 Volume:15 Page:147
ISSN:0952-8091
Container-title:International Journal of Computer Applications in Technology
language:en
Short-container-title:IJCAT

Author:

Aliabadi M.H.,Wen P.H.,Salgado N.

Publisher

Inderscience Publishers

Subject

Electrical and Electronic Engineering,Industrial and Manufacturing Engineering,Computer Networks and Communications,Computer Science Applications,Information Systems,Software

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. Analysis of Fatigue Crack Growth Rate Data in an Aircraft 7175-T7351 Al-Alloy Generated at Different Accredited Laboratories with Probability Life Assessment Example;Journal of Multiscale Modelling;2018-12

2. Crack propagation in flat panels stiffened by bonded pads;International Journal of Fatigue;2014-11

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