Optimization of Sandwich Composites Fuselages Under Flight Loads
Open Access
- 24 November 2010
- journal article
- Published by Springer Science and Business Media LLC in Applied Composite Materials
- Vol. 19 (1), 47-64
- https://doi.org/10.1007/s10443-010-9180-9
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Symmetrical Facing Wrinkling of Composite Sandwich PanelsJournal of Sandwich Structures & Materials, 2008
- Torsional buckling behaviour of stiffened cylinders under combined loadingThin-Walled Structures, 2000
- Honeycomb TechnologyPublished by Springer Science and Business Media LLC ,1997
- Buckling of imperfect sandwich cylinders under axial compressionInternational Journal of Solids and Structures, 1990