Thermal Buckling Characteristics of Composite Conical Shell Structures

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Thermal buckling and free vibration analyses of multi-laered composite conical shells based on a layerwise displacement theory are performed. The Donnells displacement-strain relationships of conical shell structure are applied. The natural frequencies are compared with the ones existing in the previous literature for laminated conical shells with several cone semi-vertex angles. Moreover, the thermal buckling behaviors of the laminated conical shell are investigated to consider the effect of the semi-vertex angle, subtended angle, and radius to thickness ratio on the structural stability.
Publisher
한국항공우주학회
Issue Date
2007-11
Language
English
Citation

KSAS INTERNATIONAL JOURNAL, v.8, no.2, pp.82 - 88

ISSN
1229-9627
URI
http://hdl.handle.net/10203/5722
Appears in Collection
AE-Journal Papers(저널논문)
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