Vibration analysis of laminated plates and shells by a hybrid stresselement.
- 1 October 1973
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 11 (10), 1450-1452
- https://doi.org/10.2514/3.6943
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Bending and vibration of multilayer sandwich beams and platesInternational Journal for Numerical Methods in Engineering, 1973
- Three-dimensional finite-element analysis of laminated compositesComputers & Structures, 1972
- Finite Element Solutions for Laminated Thick PlatesJournal of Composite Materials, 1972
- A finite-element analysis including transverse shear effects for applications to laminated platesAIAA Journal, 1971
- Triangular finite elements of variable thickness and their application to plate and shell problemsJournal of Strain Analysis, 1969
- Basis of finite element methods for solid continuaInternational Journal for Numerical Methods in Engineering, 1969
- Vibration of plate and shell structures using triangular finite elementsJournal of Strain Analysis, 1967