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Volumn 11, Issue 4, 2004, Pages 191-203
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A standard analysis methodology for the stress analysis of repaired aircraft structures with the method of composite patch repair
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Author keywords
Cracked aircraft structures; FEM software; SIF
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Indexed keywords
ALGORITHMS;
COMPUTER SIMULATION;
COMPUTER SOFTWARE;
FINITE ELEMENT METHOD;
MICROCRACKS;
NUMERICAL METHODS;
STRESS ANALYSIS;
COMPOSITE PATCH REPAIR;
CRACKED AIRCRAFT STRUCTURES;
FEM SOFTWARE;
SIF;
AIRCRAFT MATERIALS;
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EID: 3242753498
PISSN: 0929189X
EISSN: None
Source Type: Journal
DOI: 10.1023/B:ACMA.0000035426.85626.01 Document Type: Article |
Times cited : (16)
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References (8)
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