INVESTIGATION OF REPAIR TECHNIQUE FOR AIRCRAFT COMPOSITE WING PANEL WITH DISCRETE-SOURCE DAMAGE

INVESTIGATION OF REPAIR TECHNIQUE FOR AIRCRAFT COMPOSITE WING PANEL WITH DISCRETE-SOURCE DAMAGE

Since the wing is the principle bearing structure of aircraft,wing skin is repaired by using mechanically fastened joints. In this paper,scheme design,experimental verification,finite element analysis and design improvement investigation of aircraft composite wing panel with discrete-source damage w...

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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 design;Scheme Improvement
Online Access:http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2017.03.010

Internet

http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2017.03.010

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