ASSESSMENT METHOD OF THE REPAIRED AIRCRAFT COMPOSITE WING PANEL WITH DISCRETE-SOURCE DAMAGE

ASSESSMENT METHOD OF THE REPAIRED AIRCRAFT COMPOSITE WING PANEL WITH DISCRETE-SOURCE DAMAGE

The progressive damage analysis technique was studied by using finite element method and test validation of the repaired aircraft wing composite panel with discrete-source damage. Firstly,an analysis model adopting the two dimensional LaRC05 and B-K failure criteria was established to indentify the...

Full description

Bibliographic Details
Main Authors: CHEN XiangMing, ZHANG AYing, CHAI YaNan, LIU HongWu, WANG LiLi, YU Fei
Format: Article
Language:zho
Published: Editorial Office of Journal of Mechanical Strength 2017-01-01
Series:Jixie qiangdu
Subjects:
Composite wing;Stiffened panel;Discrete-source damage;Repair;Assessment method
Online Access:http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2017.02.036

Internet

http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2017.02.036

Similar Items