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Fracture strength of various lay-ups of carbon/epoxy laminates using the modified inherent flaw model
Authors:V Kamala Kannan  B Nageswara Rao
Affiliation:a Department of Aeronautical Engineering, Hindustan College of Engineering, Padur 603 103, India
b Department of Mechanical Engineering, College of Engineering, Anna University, Guindy, Chennai 600 025, India
c Structural Analysis and Testing Group, Vikram Sarabhai Space Centre, Trivandrum 695 022, India
Abstract:Modifications are made in the inherent flaw model of Waddoups, Eisenman and Kaminski (known as the WEK model) for accurate prediction of notched tensile strength of composite laminates containing a sharp notch. To examine the adequacy of the model, fracture data of center cracked carbon/epoxy composite laminates with various lay-ups are considered. The notched strength estimates are found to be close to the test results.
Keywords:Inherent flaw model  Notched strength  Carbon/epoxy  Center crack  Fracture parameters
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