Detail stress analysis and fatigue crack initiation life prediction of riveted joint

Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica

Volumn 28, Issue 2, 2007, Pages 336-339

  Wu, Jian Guo ^a   Wang, Qi Zhi ^a   Zhang, Xing ^a   Wang, Zan Ping ^b  

^a BEIHANG UNIVERSITY   (China)

^b Xi'an Aircraft Manufacture Co   (China)

Author keywords

Crack initiation life; Damage driving force; Damage mechanics; Finite element detail analysis; Riveted joint; Serviceable probability

Indexed keywords

COMPUTER SIMULATION; CRACK INITIATION; FATIGUE TESTING; FINITE ELEMENT METHOD; STRESS ANALYSIS;

CRACK INITIATION LIFE; DAMAGE DRIVING FORCE; DAMAGE MECHANICS; RIVETED JOINT; SERVICEABLE PROBABILITY;

AIRCRAFT;

EID: 34249849984     PISSN: 10006893     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

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