Adhesive Characterization and Progressive Damage Analysis of Bonded Composite JointsThe results of an experimental/numerical campaign aimed to develop progressive damage analysis (PDA) tools for predicting the strength of a composite bonded joint under tensile loads are presented. The PDA is based on continuum damage mechanics (CDM) to account for intralaminar damage, and cohesive laws to account for interlaminar and adhesive damage. The adhesive response is characterized using standard fracture specimens and digital image correlation (DIC). The displacement fields measured by DIC are used to calculate the J-integrals, from which the associated cohesive laws of the structural adhesive can be derived. A finite element model of a sandwich conventional splice joint (CSJ) under tensile loads was developed. The simulations indicate that the model is capable of predicting the interactions of damage modes that lead to the failure of the joint.
Document ID
20140004578
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Girolamo, Donato (North Carolina State Univ. Raleigh, NC, United States)
Davila, Carlos G. (NASA Langley Research Center Hampton, VA, United States)
Leone, Frank A. (NASA Langley Research Center Hampton, VA, United States)
Lin, Shih-Yung (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
May 2, 2014
Publication Date
April 23, 2014
Subject Category
Composite Materials
Report/Patent Number
NF1676L-18657Report Number: NF1676L-18657
Meeting Information
Meeting: Pegasus-AIAA Student Conference
Location: Prague
Country: Czechoslovakia
Start Date: April 23, 2014
End Date: April 25, 2014
Sponsors: American Inst. of Aeronautics and Astronautics