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College of Engineering / 工學院
Civil Engineering / 土木工程學系
A methodology for fatigue crack growth and residual strength prediction with applications to aircraft fuselages
Details
A methodology for fatigue crack growth and residual strength prediction with applications to aircraft fuselages
Journal
Computational Mechanics
Journal Volume
19
Journal Issue
6
Pages
527-532
Date Issued
1997
Author(s)
Chen, C.-S.
Wawrzynek, P.A.
Ingraffea, A.R.
CHUIN-SHAN CHEN
DOI
10.1007/s004660050204
URI
https://scholars.lib.ntu.edu.tw/handle/123456789/435459
URL
https://www.scopus.com/inward/record.uri?eid=2-s2.0-0031145392&doi=10.1007%2fs004660050204&partnerID=40&md5=eea85eb6da3ed4dd4759a669dd94dd58
Type
journal article