Effects of transverse shearing on cylindrical bending, vibration, and buckling of laminated plates
- 1 January 1987
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 25 (1), 123-129
- https://doi.org/10.2514/3.9590
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- Nonlinear theory for plates and shells including the effects of transverse shearingAIAA Journal, 1986
- A Simple Higher-Order Theory for Laminated Composite PlatesJournal of Applied Mechanics, 1984
- A Higher Order Theory for Free Vibration of Orthotropic, Homogeneous, and Laminated Rectangular PlatesJournal of Applied Mechanics, 1984
- A theory for stress analysis of composite laminatesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- A Twelvth Order Theory of Transverse Bending of Transversely Isotropic PlatesZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik, 1983
- An accurate, simple theory of the statics and dynamics of elastic platesMechanics Research Communications, 1980
- A High-Order Theory of Plate Deformation—Part 2: Laminated PlatesJournal of Applied Mechanics, 1977
- Transverse shear in laminated plate theories.AIAA Journal, 1973
- Shear Deformation in Heterogeneous Anisotropic PlatesJournal of Applied Mechanics, 1970