Composite skin/stringer disbond analysis using a shell/3D modeling technique

American Society for Composites - 21st Technical Conference of the American Society for Composites 2006

Volumn 1, Issue , 2006, Pages 14-32

  Krueger, R ^a   Minguet, P J ^b  

^a NATIONAL INSTITUTE OF AEROSPACE   (United States)

^b BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

3D SOLID MODEL; CERTIFICATION AUTHORITIES; COMPOSITE SKINS; DISBOND; EMBEDDED DEFECTS; FAILURE CRITERIA; FAILURE INDEX; INTERLAMINAR FRACTURE; LOCAL REFINEMENT; MIXED MODE; MODELING TECHNIQUE; OUT-OF-PLANE; REDUCED MODEL; SHEAR LOADINGS; SHELL ELEMENT; SHELL MODELS; SOLID ELEMENTS;

DEFECTS; DELAMINATION; FINITE ELEMENT METHOD; FRACTURE MECHANICS; LOADING;

STRINGERS;

EID: 84867640589     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (27)

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