Determination of Fracture Parameters for Multiple Edge Cracks of a Finite Plate
Author:
Affiliation:
1. Department of Mechanical Engineering, S. V. National Institute of Technology, Surat 395 007, India
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C032036
Reference20 articles.
1. Calculation of stress intensity factors by the force method
2. Progressive crack growth analysis using interface element based on the virtual crack closure technique
3. Finite element analysis of postbuckling and delamination of composite laminates using virtual crack closure technique
4. A closed form solution about stress intensity factors of shear modes for 3-D finite bodies with eccentric cracks by the energy release rate method
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