Fatigue Crack Growth in D357-T6 and 2024-T3 under Variable Amplitude Loading and Validation of Fatigue Crack Growth Models
22nd, Symposium of the International Committee on Aeronautical Fatigue; ICAF 2003 ; 2003 ; Lucerne, Switzerland
2004-01-01
14 pages
Includes bibliographic references
Aufsatz (Konferenz)
Englisch
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