S.F.M. de Almeida

A numerical study on the impact resistance of composite shells using an energy based failure model

Maurício Vicente Donadon, N. O. Yokoyama, S.F.M. de Almeida, 2010 .

A progressive failure model for composite laminates subjected to low velocity impact damage

Brian Falzon, Lorenzo Iannucci, Maurício Vicente Donadon, 2008 .

The Flexible Wing Project: Advanced Tailoring Strategies for Laminated Composite Materials Final Report

Christopher York, S.F.M. de Almeida, 2017 .

Optimum design for buckling of arbitrary shaped ribs under uncertain loadings

A. R. de Faria, S.F.M. de Almeida, A. C. Conrado, 2005, The Aeronautical Journal (1968).