EPJ Web of Conferences 6, 24001 (2010)
https://doi.org/10.1051/epjconf/20100624001
https://doi.org/10.1051/epjconf/20100624001
Enhancing Buckling Limits in Honeycombs for Composite Sandwich Panels.
1
Engineering Mathematics and Physical Sciences, University of
Exeter, EX4
4QF, Exeter, UK.
2
Department of Aerospace Engineering, University of
Bristol, BS8
1TR, Bristol, UK.
This article has no abstract.
© Owned by the authors, published by EDP Sciences, 2010
