Influence of Large Amplitudes on Flexural Vibrations of a Thin Circular Cylindrical Shell
- 1 August 1961
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 28 (8) , 602-609
- https://doi.org/10.2514/8.9113
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Supersonic Panel Flutter of a Cylindrical Shell of Finite LengthJournal of the Aerospace Sciences, 1961
- Three-Dimensional Investigation of the Propagation of Waves in Hollow Circular Cylinders. I. Analytical FoundationThe Journal of the Acoustical Society of America, 1959
- Nonlinear Response of Aircraft Panels in Acoustic NoiseThe Journal of the Acoustical Society of America, 1957
- Influence of Large Amplitudes on Free Flexural Vibrations of Rectangular Elastic PlatesJournal of Applied Mechanics, 1956
- On the non-linear vibration problem of the elastic stringQuarterly of Applied Mathematics, 1945