A methodology for fatigue crack growth and residual strength prediction with applications to aircraft fuselages

Chen, C.-S.C.-S.ChenWawrzynek, P.A.P.A.WawrzynekIngraffea, A.R.A.R.IngraffeaCHUIN-SHAN CHEN2019-12-102019-12-101997https://scholars.lib.ntu.edu.tw/handle/123456789/435459A methodology for fatigue crack growth and residual strength prediction with applications to aircraft fuselagesjournal article10.1007/s0046600502042-s2.0-0031145392https://www.scopus.com/inward/record.uri?eid=2-s2.0-0031145392&doi=10.1007%2fs004660050204&partnerID=40&md5=eea85eb6da3ed4dd4759a669dd94dd58