What is it about?
The cracking simulation between two holes in the fuselage of an aircraft. A finite element-based simulator has been used to investigate the cracking behavior of the notches around the fuselage. A comparison with a case study has been presented. Hence, a validation with the FE model was shown.
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Photo by Kevin Hackert on Unsplash
Why is it important?
The using of Fracture analysis code-Franc2D to verify this issue
Perspectives
The maintenance and repairing around the rivets and notches have to emphasize.
Dr. Ahmed Almukhtar
Read the Original
This page is a summary of: Aircraft Fuselage Cracking and Simulation, Procedia Structural Integrity, January 2020, Elsevier,
DOI: 10.1016/j.prostr.2020.10.016.
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