Stiffness tailoring for improved compressive strength of composite plates with holes
- 1 January 1988
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 26 (1) , 72-77
- https://doi.org/10.2514/3.9853
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- 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
- Applications of a Quadratic Extended Interior for Structural Optimization Penalty FunctionAIAA Journal, 1976
- Stress Fracture Criteria for Laminated Composites Containing Stress ConcentrationsJournal of Composite Materials, 1974
- NEUTRAL IIOLES IN PLANE SHEET—REINFORCED IIOLES WHICH ARE ELASTICALLY EQUIVALENT TO THE UNCUT SHEETThe Quarterly Journal of Mechanics and Applied Mathematics, 1953