B. Troclet
- Analysis of steady and unsteady aerodynamic loads on the Ariane 5 lauch vehicle rear part during flight ascent. Dans: La Houille Blanche, v. 86, n. 6 (octobre 2000). (2000):
- On global bending–shear core transition effects for the vibroacoustic of sandwich structures: Analytical and numerical investigations. Dans: Composite Structures, v. 154 (octobre 2016). (2016):
- Efficient prediction of the response of layered shells by a dynamic stiffness approach. Dans: Composite Structures, v. 97 (mars 2013). (2013):
- Modeling the response of composite panels by a dynamic stiffness approach. Dans: Composite Structures, v. 96 (février 2013). (2013):
- Assessments of shear core effects on sound transmission loss through sandwich panels using a two-scale approach. Dans: Computers & Structures, v. 182 (1 avril 2017). (2017):