Modelling of the Behaviour of Aramid Folded Cores Up to Global Crushing, Strain, vol.45, p.no?no, 2010. ,
DOI : 10.1111/j.1475-1305.2010.00753.x
URL : https://hal.archives-ouvertes.fr/hal-00435880
Numerical modeling of the geometrical defects of an origami-like sandwich core, Composite Structures, vol.93, issue.10, pp.6-52, 2010. ,
DOI : 10.1016/j.compstruct.2011.04.011
URL : https://hal.archives-ouvertes.fr/hal-00640689
A continuous folding process for sheet materials, International Journal of Materials and Product technology, vol.21, pp.217-238, 2004. ,
Technology for continuous folding of sheet materials into a honeycomb-like configuration, 2007. ,
Dynamic axial crushing of multilayer core structures of folded Chevron patterns, International Journal of Materials and Product Technology, vol.21, issue.1/2/3, pp.169-185, 2004. ,
DOI : 10.1504/IJMPT.2004.004750
The in-plane stiffnesses of a honeycomb core including the thickness effect, Archive of Applied Mechanics (Ingenieur Archiv), vol.68, issue.5, pp.334-341, 1998. ,
DOI : 10.1007/s004190050169
Closed-form analysis of the thickness effect of regular honeycomb core material, Composite Structures, vol.48, issue.1-3, pp.1-3, 2000. ,
DOI : 10.1016/S0263-8223(99)00074-4
Thin elastic and periodic plates, Mathematical Methods in the Applied Sciences, vol.2, issue.18, pp.159-191, 1984. ,
DOI : 10.1002/mma.1670060112
A homogenized Reissner???Mindlin model for orthotropic periodic plates: Application to brickwork panels, International Journal of Solids and Structures, vol.44, issue.18-19, pp.18-19, 2007. ,
DOI : 10.1016/j.ijsolstr.2007.02.009
A solution including skin effect for stiffness and stress field of sandwich honeycomb core, International Journal of Solids and Structures, vol.42, issue.9-10, pp.9-10, 2005. ,
DOI : 10.1016/j.ijsolstr.2004.09.042
Mechanical tests for foldcore base material properties, Composites Part A: Applied Science and Manufacturing, vol.40, issue.12, pp.1941-1952, 2009. ,
DOI : 10.1016/j.compositesa.2009.03.005
Asymptotic analysis of heterogeneous Cosserat media, International Journal of Solids and Structures, vol.38, issue.26-27, pp.26-27, 2001. ,
DOI : 10.1016/S0020-7683(00)00295-X
A finite element study of the transverse shear in honeycomb cores, International Journal of Solids and Structures, vol.30, issue.13, pp.1777-1788, 1993. ,
DOI : 10.1016/0020-7683(93)90233-W
Virtual testing of sandwich core structures using dynamic finite element simulations, Computational Materials Science, vol.45, issue.2, pp.205-216, 2009. ,
DOI : 10.1016/j.commatsci.2008.09.017
Sandwich structures with textile-reinforced composite foldcores under impact loads, Composite Structures, vol.92, issue.6, pp.1485-1497, 2010. ,
DOI : 10.1016/j.compstruct.2009.11.001
A direct homogenisation approach for determination of the stiffness matrix for microheterogeneous plates with application to sandwich panels, Composites Part B: Engineering, vol.34, issue.7, pp.615-626, 2003. ,
DOI : 10.1016/S1359-8368(03)00063-5
Method for the production of a sandwich structure for a sandwich composite, 2004. ,
The Shear Modulus of Foil Honeycomb Cores, Aircraft Engineering and Aerospace Technology, vol.30, issue.10, pp.294-302, 1958. ,
DOI : 10.1108/eb033026
Stiffness and failure behaviour of folded sandwich cores under combined transverse shear and compression, Composites Part A: Applied Science and Manufacturing, vol.38, issue.5, pp.1288-1295, 2007. ,
DOI : 10.1016/j.compositesa.2006.11.008
Doubly periodic flat surfaces in three-space, 1997. ,
Paterning technology for folded sheet structures, 2005. ,
A new model for thin plates with rapidly varying thickness, International Journal of Solids and Structures, vol.20, issue.4, pp.333-350, 1984. ,
DOI : 10.1016/0020-7683(84)90044-1
Thick periodic plates homogenization, application to sandwich panels including chevron folded core, 2010. ,
A Cosserat multiparticle model for periodically layered materials, Mechanics Research Communications, vol.37, issue.3, pp.293-297, 2010. ,
DOI : 10.1016/j.mechrescom.2010.01.007
Transverse shear stiffness of a chevron folded core used in sandwich construction, International Journal of Solids and Structures, vol.47, issue.18-19, pp.18-19, 2010. ,
DOI : 10.1016/j.ijsolstr.2010.05.024
A Bending-Gradient model for thick plates. Part I: Theory, International Journal of Solids and Structures, vol.48, issue.20, pp.2878-2888, 2011. ,
DOI : 10.1016/j.ijsolstr.2011.06.006
A Bending-Gradient model for thick plates, Part II: Closed-form solutions for cylindrical bending of laminates, International Journal of Solids and Structures, vol.48, issue.20, pp.2889-2901, 2011. ,
DOI : 10.1016/j.ijsolstr.2011.06.005
Homogenization of cellular sandwich panels, Comptes Rendus M??canique, vol.340, issue.4-5, 2011. ,
DOI : 10.1016/j.crme.2012.02.014
Zeta-core sandwich -its concept and realization, ISAS report, vol.37, issue.6, pp.137-164, 1972. ,
Simulation of impact on sandwich structures, Composite Structures, vol.67, issue.2, pp.217-227, 2005. ,
DOI : 10.1016/j.compstruct.2004.09.018
Evaluation of transverse shear stiffness of structural core sandwich plates, Composite Structures, vol.37, issue.2, pp.145-153, 1997. ,
DOI : 10.1016/S0263-8223(97)80007-4
Exact Solutions for Composite Laminates in Cylindrical Bending, Journal of Composite Materials, vol.1, issue.3, pp.398-411, 1969. ,
DOI : 10.1177/002199836900300304
Buckling of honeycomb sandwiches: Periodic finite element considerations, CMES-Computer Modeling In Engineering & Sciences, vol.12, issue.3, pp.229-241, 2006. ,
Failure mode maps for honeycomb sandwich panels, Composite Structures, vol.44, issue.4, pp.237-252, 1999. ,
DOI : 10.1016/S0263-8223(98)00123-8
Buckling in Thin Walled Micro and Meso Structures of Lightweight Materials and Material Compounds, Computational Mechanics, vol.37, issue.6, pp.470-478, 2006. ,
DOI : 10.1007/s00466-005-0731-0
Sandwich-type structural element, 1960. ,
Equivalent transverse shear stiffness of honeycomb cores, International Journal of Solids and Structures, vol.32, issue.10, pp.1383-1393, 1995. ,
DOI : 10.1016/0020-7683(94)00202-8
A technique for designing highly-stiffened chevron folded cores, Russian Aeronautics, vol.49, issue.4, pp.1-7, 2006. ,