Design of a blade-stiffened composite panel with a hole
- 31 December 1991
- journal article
- Published by Elsevier in Composite Structures
- Vol. 18 (3) , 195-219
- https://doi.org/10.1016/0263-8223(91)90033-u
Abstract
No abstract availableKeywords
This publication has 14 references indexed in Scilit:
- Buckling behavior of compression-loaded symmetrically laminated angle-ply plates with holesAIAA Journal, 1988
- Stiffness tailoring for improved compressive strength of composite plates with holesAIAA Journal, 1988
- Compressive failure model for anisotropic plates with a cutoutAIAA Journal, 1987
- Compression Behavior of A= 45 -Dominated Laminates with a Circular Hole or Impact DamageAIAA Journal, 1986
- Effects of orthotropy and width on the compression strength of graphite-epoxy panels with holesAIAA Journal, 1984
- Optimization of openings in plates under plane stressAIAA Journal, 1983
- Improvement of the First-Ply-Failure Strength in Laminates by Using Softening StripsJournal of Composites Technology and Research, 1981
- Optimization of a Stiffened Square Panel Subjected to Compressive Edge LoadsAIAA Journal, 1979
- Optimum laminate design for strength and stiffnessInternational Journal for Numerical Methods in Engineering, 1973
- A Unified Approach to the Initial Buckling of Stiffened Panels in CompressionAeronautical Quarterly, 1968