Case Study and Simulation of Fatigue Damages and DTE of Aging Aircraft — A Review of Researches in Japan
Part of the Springer Series in Computational Mechanics book series (SSCMECH)
This is a review paper on the study of aging aircraft structures conducted in Japan.
KeywordsFatigue Crack Laminate Plate Joint Specimen National Aerospace Laboratory Rivet Hole
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.
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© Springer-Verlag Berlin, Heidelberg 1991