Comparison of damage path predictions for composite laminates by explicit and standard finite element analysis tools

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

Volumn 3, Issue , 2006, Pages 1919-1941

  Bogert, Philip B ^a,d   Satyanarayana, Arunkumar ^b,e   Chunchu, Prasad B ^c,e  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b NORTHROP GRUMMAN CORPORATION   (United States)

^c Eagle Aeronautics Inc   (United States)

^d Mechanics of Structures and Materials Branch   (United States)

^e AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DAMAGE PATH; INTRA LAMINAR FIBER; SPLITTING; TENSION LOADING;

COMPOSITE MATERIALS; COMPUTER AIDED SOFTWARE ENGINEERING; DAMAGE DETECTION; FINITE ELEMENT METHOD; LAMINATES; LOADING; TENSILE TESTING;

FAILURE ANALYSIS;

EID: 34147206891     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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