Single-Stringer Compression Specimen for the Assessment of Damage Tolerance of Postbuckled Structures
Journal of Aircraft ; 48 , 2 ; 495-502
01.03.2011
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Fatigue Life of Postbuckled Structures with Indentation Damage (AIAA 2016-0982)
British Library Conference Proceedings | 2016
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