Fatigue Life Time Prediction of Poaf Epsilon Tb-30 Aircraft - Implementation of Automatic Crack Growth Based on 3D Finite Element Method

AuthID
 P-006-739
3
Author(s)
Marado, B
Document Type
Article
Year published
2013
Published
in ENGINEERING FAILURE ANALYSIS, ISSN: 1350-6307
Volume: 33, Pages: 17-28 (12)
Indexing
Wos®
Scopus®
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Google Scholar®
Publication Identifiers
Scopus: 2-s2.0-84877890979
Wos: WOS:000324082700002
Source Identifiers
ISSN: 1350-6307
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