BUCKLING BEHAVIOR OF COMPOSITE LAMINATES (WITH AND WITHOUT CUTOUTS) SUBJECTED TO NONUNIFORM IN-PLANE LOADS

DOI10.1142/S0219455413500442zbMath1359.74105MaRDI QIDQ2972255

Mira Mitra, Ganesh Kumar Soni, Ramesh K. Singh

Publication date: 7 April 2017

Published in: International Journal of Structural Stability and Dynamics (Search for Journal in Brave)

zbMATH Keywords

critical buckling loadcomposite laminates with cutoutsnonuniform in-plane load

Mathematics Subject Classification ID

Composite and mixture properties (74E30) Bifurcation and buckling (74G60)

Related Items (2)

Analysis of laminated plates and shells using B-spline wavelet on interval finite element ⋮ Effect of reinforced cutouts and ply-orientations on buckling behavior of composite panels subjected to non-uniform edge loads

Cites Work

• Buckling analysis of shear deformable plates using the quadrature element method
• Elastic buckling of rectangular plates under linearly varying in-plane normal load with a circular cutout

This page was built for publication: BUCKLING BEHAVIOR OF COMPOSITE LAMINATES (WITH AND WITHOUT CUTOUTS) SUBJECTED TO NONUNIFORM IN-PLANE LOADS