Approach to Critical Crack Opening Displacement Modeling of Damage in Metal Sheets after Composite Patch Bonded Repair

The paper proposes a method of calculating the maximum displacement in the aircraft metal structure repaired by CPBR (bonded composite patch repair).

Bibliographic Details
Main Authors:	Sałacinski Michał, Leski Andrzej, Stefaniuk Michał
Format:	Article
Language:	English
Published:	Sciendo 2016-06-01
Series:	Fatigue of Aircraft Structures
Subjects:	composites aerospace composite patch bonded repair
Online Access:	https://doi.org/10.1515/fas-2016-0009

Internet

https://doi.org/10.1515/fas-2016-0009