The response of a thin cylindrical shell to transient surface loading
- 1 April 1965
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 3 (4) , 701-709
- https://doi.org/10.2514/3.2950
Abstract
No abstract availableThis publication has 12 references indexed in Scilit:
- The response of a thin cylindrical shell to transient surface loadingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1964
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- The Flexural Vibrations of Thin CylindersProceedings of the Institution of Mechanical Engineers, 1953
- Displacements of a Linear Elastic System Under a Given Transient LoadAeronautical Quarterly, 1949
- Flexural vibrations of the walls of thin cylindrical shells having freely supported endsProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1949
- Transient vibration in an airplane wing obtained by several methodsJournal of Research of the National Bureau of Standards, 1949
- IV. Note on the free vibrations of an infinitely long cylindrical shellProceedings of the Royal Society of London, 1889