Solution of stresses and strains for laminated monoclinic cylinders.
- 1 October 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 10 (10), 1364-1366
- https://doi.org/10.2514/3.6623
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Temperature distributions in anisotropic shells of revolution.AIAA Journal, 1972
- Static solution of monoclinic circular plates.AIAA Journal, 1971
- Frequency and buckling eigenvalues of anisotropic cylinders subjected to nonuniform lateral prestressInternational Journal of Solids and Structures, 1971
- Laminar Boundary LayersPhysics Today, 1964