Analysis of frame-to-skin joint pull-off tests and prediction of the delamination failure

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

Volumn 3, Issue , 2001, Pages 2258-2264

  Li, J ^a   Sen, J K ^a  

^a BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFRAMES; BENDING MOMENTS; COMPUTER SIMULATION; CRACKS; DEFECTS; DELAMINATION; FAILURE ANALYSIS; FINITE ELEMENT METHOD; FLANGES; MATERIALS TESTING; RESINS; STRAIN;

CLIP ANGLE; DELAMINATION FAILURE; FRAME TO SKIN JOINT PULL OFF TESTS; STRAIN ENERGY RELEASE RATE; STRUCTURAL INTEGRITY;

JOINTS (STRUCTURAL COMPONENTS);

EID: 0035006592     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)