Fatigue life of panels with multiple site damage

Journal of Aircraft

Volumn 33, Issue 5, 1996, Pages 1003-1013

  Moukawsher, E J ^a,c   Grandt Jr , A F ^b,c,d   Neussl, M A ^a,b  

^a U S COAST GUARD   (United States)

^b PURDUE UNIVERSITY   (United States)

^c Dept of Aeronautical Engineering ^*

^d Aeronautical and Astronautical Engineering

Author keywords

[No Author keywords available]

Indexed keywords

CRACK INITIATION; CRACK PROPAGATION; CRACKS; FATIGUE OF MATERIALS; FATIGUE TESTING; FRACTURE MECHANICS; LOADS (FORCES); NONDESTRUCTIVE EXAMINATION; NUMERICAL METHODS; RESIDUAL STRESSES; STRAIN; TENSILE STRENGTH;

ALUMINUM PANELS; CRACKS INTERACTION EFFECTS; MINER RULE; MULTIPLE SITE DAMAGE; NEUBER RULE; RESIDUAL STRENGTH; STRAIN LIFE ANALYSIS;

STRUCTURAL PANELS;

EID: 0030245369     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/3.47047     Document Type: Article

References (16)

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