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Cylindrical Shell Flutter—Theory and Experiment

Published online by Cambridge University Press:  04 July 2016

D. J. Johns
D. J. Johns*
Affiliation:
Reader in Aeronautical Engineering, Loughborough College of Technology
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Extract

Despite the fact that there have been few reported instances of the flutter of circular, cylindrical, iso-tropic shells, there still remains a challenge to the analyst to derive a theory which will correlate with the available experimental data.

Information

Type
Technical Notes
Information
The Aeronautical Journal , Volume 70 , Issue 664 , April 1966 , pp. 533
Copyright
Copyright © Royal Aeronautical Society 1966

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References

1.Stearman, R., Lock, M. H. and Fung, Y. C. Ames Tests on the Flutter of Cylindrical Shells. GALCIT Rep SM62-37, December 1962.Google Scholar
2.Fung, Y. C.Some Recent Contributions to Panel Flutter Research. AIAA Journal, Vol 1(4), p 898, April 1963.Google Scholar
3.Olsen, M. H. Supersonic Flutter of Circular Cylindrical Shells Subjected to Internal Pressure and Axial Compression. GALCIT Rep SM65-7 (AFOSR 65-0599), April 1965.Google Scholar
4.Johns, D. J. Supersonic Flutter of Cylindrical Shells. College of Aeronautics, Note No. 104, July 1960.Google Scholar
5.Johns, D. J. Some Panel Aeroelastic Instabilities. AGARD Rep 474, September 1963.Google Scholar
6.Voss, H. M.The Effect of an External Supersonic Flow on the Vibration Characteristics of Thin Cylindrical Shells. J Aerospace Sci, Vol 28(12), p 945, December 1961.Google Scholar
7.Johns, D. J. A Survey on Panel Flutter. AGARD Report. To be published.Google Scholar