Fatigue crack growth modelling based on CTOD for the 7050-T6 alloy

Author:

Antunes F. V.1ORCID,Branco R.1,Prates P. A.1,Borrego L.12

Affiliation:

1. CEMUC, Department of Mechanical Engineering; University of Coimbra Pólo II; Rua Luis Reis Santos, Pinhal de Marrocos 3030-788 Coimbra Portugal

2. Department of Mechanical Engineering; Polytechnic Institute of Coimbra; Rua Pedro Nunes, Quinta da Nora 3030-129 Coimbra Portugal

Funder

FCT - Portuguese Foundation for Science and Technology

Federación Española de Enfermedades Raras

Publisher

Wiley

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference83 articles.

1. Progress in structural materials for aerospace systems;Williams;Acta Materialia,2003

2. Influence of grain structure and crystallographic orientation on fatigue crack propagation behavior of 7050 alloy thick plate;Wei;International Journal of Fatigue,2014

3. Critical analysis of crack growth propagation laws;Paris;J. Basic Engineering,1963

4. Mechanics of crack tip deformation and extension by fatigue. In: Fatigue crack propagation;Rice;Philadelphia: ASTM STP,1967

5. Fatigue crack closure under cyclic tension;Elber;Engineering Fracture Mechanics,1970

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