S. F. M. de Almeida
- The effect of piezoelectrically induced stress stiffening on the aeroelastic stability of curved composite panels. In: Composite Structures, v. 94, n. 12 (December 2012). (2012):
- A numerical study on the impact resistance of composite shells using an energy based failure model. In: Composite Structures, v. 93, n. 1 (December 2010). (2010):
- A progressive failure model for composite laminates subjected to low velocity impact damage. In: Computers & Structures, v. 86, n. 11-12 (June 2008). (2008):