Free vibration behavior of laminated composite stiffened elliptic parabolic shell panel with cutout
Abstract: In this paper free vibration behavior of laminated composite stiffened elliptic parabolic shell has been analyzed in terms of natural frequency and mode shape. Finite element method has been applied using an eight-noded curved quadratic isoparametric element for shell with a three noded curved beam element for stiffener. Cross and angle ply shells with different edge conditions have been studied varying the size and position of the cutouts to arrive at a set of inferences of practical engineering significances.
- Location
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Deutsche Nationalbibliothek Frankfurt am Main
- Extent
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Online-Ressource
- Language
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Englisch
- Bibliographic citation
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Free vibration behavior of laminated composite stiffened elliptic parabolic shell panel with cutout ; volume:2 ; number:1 ; year:2015 ; extent:21
Curved and layered structures ; 2, Heft 1 (2015) (gesamt 21)
- Creator
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Sahoo, Sarmila
- DOI
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10.1515/cls-2015-0009
- URN
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urn:nbn:de:101:1-2410251617017.134495168421
- Rights
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Open Access; Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Last update
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15.08.2025, 7:30 AM CEST
Data provider
Deutsche Nationalbibliothek. If you have any questions about the object, please contact the data provider.
Associated
- Sahoo, Sarmila