Computation of energy release rates for cracked composite panels with nonlinear deformation

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

Volumn 4, Issue , 1995, Pages 2713-2727

  Wang, John T ^a   Xue, David Y ^a   Sleight, David W ^a   Housner, Jerrold M ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPOSITE PANELS; ENERGY RELEASE RATE; GRADIENT METHOD; NONLINEAR DEFORMATION; VIRTUAL CRACK CLOSURE TECHNIQUE;

BUCKLING; COMPUTATIONAL METHODS; DEFORMATION; FRACTURE MECHANICS; FUSELAGES; PRESSURE EFFECTS; STIFFNESS; STRESS ANALYSIS; STRUCTURAL ANALYSIS; STRUCTURAL LOADS; STRUCTURAL PANELS; TENSILE TESTING;

COMPOSITE STRUCTURES;

EID: 0029227129     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (26)