Original paper
Numerical Analysis of the Bonded Composite Shape Effects under Thermal Loading in Aircraft Structures
Abstract
The design of the optimal shape of patch with a good compromise between mechanical performances and manufacturing aspects can be sought in order to get the maximum structural safety-cost ratio. In this work an analysis has been conducted for development of a finite element methodology to circumvent the thermal effect problem in the bonded repair. Physical and geometrical parameters of the repair material were assumed to be variables, this method...
Paper Details
Title
Numerical Analysis of the Bonded Composite Shape Effects under Thermal Loading in Aircraft Structures
Published Date
Nov 9, 2021
Journal
Volume
1167
Pages
1 - 11
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Notes
History