Numerical Analysis of Fastener Delamination/Disbond Arrest Mechanism in Aircraft Composite Structures
Journal of Aircraft ; 49 , 2 ; 630-635
01.03.2012
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Reliability of Damage Tolerance Composite Structure Using Fasteners as Disbond Arrest Mechanism
British Library Conference Proceedings | 2009
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