Crack-growth analysis code for assessing fatigue life of 2219 T851 aluminium specimens under aircraft structure service spectra

Author: Pantelakis S.G.   Kermanidis A.T.   Daglaras P.G.  

Publisher: Elsevier

ISSN: 0167-8442

Source: Theoretical and Applied Fracture Mechanics, Vol.28, Iss.1, 1997-10, pp. : 1-12

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Abstract