Residual strength of panels with multiple site damage

Journal of Aircraft

Volumn 33, Issue 5, 1996, Pages 1014-1021

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

^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

AIRCRAFT; CRACK PROPAGATION; CRACKS; FATIGUE OF MATERIALS; FATIGUE TESTING; FRACTURE; LOADS (FORCES); MATHEMATICAL MODELS; RESIDUAL STRESSES; STRENGTH OF MATERIALS; STRESS INTENSITY FACTORS; TENSILE STRENGTH;

ALUMINUM PANELS; CYCLIC TENSION; FRACTURE RESISTANCE; MULTIPLE SITE DAMAGE; PLASTIC ZONE; RESIDUAL STRENGTH; TENSILE LOAD;

STRUCTURAL PANELS;

EID: 0030247699     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/3.47048     Document Type: Article

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