Abstract
The elastodynamic response of a four-layered composite with an interface crack under anti-plane shear impact load is considered in this paper. Laplace and Fourier transforms are applied to reduce this mixed boundary value problem to a Cauchy-type singular integral equation of the first kind in Laplace transform plane, which is solved numerically. A Laplace inversion technique developed by Miller and Guy is then used to get the solution in the physical plane. Finally, the elastodynamic stress intensity factors are obtained as function of time, geometrical parameters and material properties.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
