Optimum design of composite honeycomb sandwich panels subjected to uniaxial compression
- 1 October 1986
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 24 (10), 1690-1696
- https://doi.org/10.2514/3.9502
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- The behavior of structures composed of composite materialsPublished by Springer Nature ,1985
- Optimum Design of Laminated Plates under Axial CompressionAIAA Journal, 1979