Inter-laminar Stresses In Composite Sandwich Panels Using Variational Asymptotic Method (VAM)

In aerospace applications, use of laminates made of composite materials as face sheets in sandwich panels are on the rise. These composite laminates have low transverse shear and transverse normal moduli compared to the in-plane moduli. It is also seen that the corresponding transverse strength valu...

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Bibliographic Details
Main Author: Rao, M V Peereswara
Other Authors: Harursampath, Dineshkumar
Language:en_US
Published: 2013
Subjects:
Online Access:http://etd.iisc.ernet.in/handle/2005/2103
http://etd.ncsi.iisc.ernet.in/abstracts/2706/G24899-Abs.pdf