Derivation of axisymmetric flexural vibration equations of a cylindrically aeolotropic circular plate.
- 1 July 1969
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 7 (7) , 1386-1388
- https://doi.org/10.2514/3.5360
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- Forced Axisymmetric Motions of Circular Elastic PlatesJournal of Applied Mechanics, 1965
- COMBINED EFFECTS OF VISCOUS INTERACTION AND IDEAL SOURCE FLOW ON PRESSURE AND HEAT-TRANSFER DISTRIBUTIONS OVER HEMISPHERE CYLINDERS AT MACH 18Published by Defense Technical Information Center (DTIC) ,1965
- Vibration Frequencies of Tapered Bars and Circular PlatesJournal of Applied Mechanics, 1964
- Flexural Vibrations of Cylindrically Aeolotropic Circular PlatesThe Journal of the Acoustical Society of America, 1964
- Forced Vibrations of a Circular PlateJournal of Applied Mechanics, 1959
- Closed-Form Solutions for Plates of Variable ThicknessJournal of Applied Mechanics, 1953
- Axially Symmetrical Plates With Linearly Varying ThicknessJournal of Applied Mechanics, 1951
- Note on the Bending of Circular Plates of Variable ThicknessJournal of Applied Mechanics, 1949
- The Bending of the Cylindrically Aeolotropic PlateJournal of Applied Mechanics, 1944