Author:
Coronado P.,Argüelles A.,Viña J.,Mollón V.,Viña I.
Funder
Spanish Ministry of Science and Innovation
Subject
Applied Mathematics,Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science,Modeling and Simulation
Reference18 articles.
1. Empirical model for stress ratio effect on fatigue delamination growth rate in composite laminates;Anderson;Int. J. Fatigue,2004
2. Interlaminar crack initiation and growth rate in a carbon–fibre epoxy composite under mode-I fatigue loading;Argüelles;Compos. Sci. Technol.,2008
3. The effects of moisture and temperature on the interlaminar delamination toughness of a carbon/epoxy composite;Asp;Compos. Sci. Technol.,1998
4. ASTM D5528-01, 2001. Standard test method for mode I interlaminar fracture toughness of unidirectional fiber–reinforced polymer matrix composites.
5. ASTM D6115-97, 1997. Standard test method for mode I fatigue delamination growth onset of unidirectional fiber–reinforced polymer matrix composites.
Cited by
68 articles.
订阅此论文施引文献
订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献