P. Linde
- Influence of modelling and solution methods on the FE-simulation of the post-buckling behaviour of stiffened aircraft fuselage panels. In: Composite Structures, v. 73, n. 2 (May 2006). (2006):
- Mitigating the weak impact response of thin-ply based thin laminates through an unsymmetrical laminate design incorporating intermediate grade plies. In: Composite Structures, v. 220 (July 2019). (2019):
- A strategy to improve the structural performance of non-crimp fabric thin-ply laminates. In: Composite Structures, v. 188 (March 2018). (2018):
- Effect of tow thickness on the structural response of aerospace-grade spread-tow fabrics. In: Composite Structures, v. 179 (November 2017). (2017):
- An experimental study on matrix crack induced delamination in composite laminates. In: Composite Structures, v. 127 (September 2015). (2015):
- Micro-mechanical analysis of the in situ effect in polymer composite laminates. In: Composite Structures, v. 116 (September 2014). (2014):
- An energy based failure criterion for matrix crack induced delamination in laminated composite structures. In: Composite Structures, v. 112 (June 2014). (2014):
- Size effects on the tensile and compressive failure of notched composite laminates. In: Composite Structures, v. 96 (February 2013). (2013):
- Impact and compression after impact response in thin laminates of spread-tow woven and non-crimp fabrics. In: Composite Structures, v. 215 (May 2019). (2019):