Comparison of Variational, Differential Quadrature, and Approximate Closed-Form Solution Methods for Buckling of Highly Flexurally Anisotropic Laminates (2013)
Attributed to:
Aerostructural Efficiency of Damage Tolerant Composites via Optimised Fibre Placement
funded by
EPSRC
Abstract
No abstract provided
Bibliographic Information
Digital Object Identifier: http://dx.doi.org/10.1061/(asce)em.1943-7889.0000468
Publication URI: http://dx.doi.org/10.1061/(asce)em.1943-7889.0000468
Type: Journal Article/Review
Parent Publication: Journal of Engineering Mechanics
Issue: 8