Finite strip dynamic instability analysis of perforated cylindrical shell panels
β Scribed by J. Fazilati; H.R. Ovesy
- Book ID
- 113552289
- Publisher
- Elsevier Science
- Year
- 2012
- Tongue
- English
- Weight
- 995 KB
- Volume
- 94
- Category
- Article
- ISSN
- 0263-8223
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π SIMILAR VOLUMES
The dynamic instability of laminated composite circular cylindrical shells subjected to periodic load is studied using a C o shear Β―exible two-noded axisymmetric shell element. The formulation includes the eects of inplane and rotary terms. The boundaries of the principal instability regions are con
It is proved that cylindrical shells and two dimensional flat panels constrained to zero displacement at their leading and trailing edges, and exposed to subsonic flow, can lose their stability by divergence (buckling) while in supersonic flow two-dimensional panels can only flutter. Moreover, it i