Fracture mechanics analyses of composite skin-stiffener debond configurations with shell elements

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 2, Issue , 1994, Pages 676-693

  Wang, J T ^a   Raju, I S ^a   Sleight, D W ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DEGREES OF FREEDOM (MECHANICS); ENERGY DISSIPATION; FINITE ELEMENT METHOD; LAMINATED COMPOSITES; MATHEMATICAL MODELS; SKIN; STRAIN; THREE DIMENSIONAL;

COMPOSITE SKIN STIFFENER DEBOND CONFIGURATION; STIFFENER; VIRTUAL CRACK CLOSURE TECHNIQUE;

FRACTURE MECHANICS;

EID: 0028725880     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1994-1389     Document Type: Conference Paper

References (21)