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Full metadata record
DC Field | Value | Language |
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dc.contributor.author | SAHOO, Sarmila | - |
dc.date.accessioned | 2017-12-21T11:42:12Z | - |
dc.date.available | 2017-12-21T11:42:12Z | - |
dc.date.issued | 2012-12 | - |
dc.identifier.uri | http://hdl.handle.net/123456789/1482 | - |
dc.description.abstract | Abstract: An eight noded shell element combined with a three noded beam element is used to study the free vibration behaviour of laminated composite stiffened hypar shells. A variety of problems are solved taking simply supported boundary conditions. Free vibration response of stiffened composite hypar shells is studied with respect to fundamental frequency by varying the number and depth of stiffeners. The results are further analysed to suggest guidelines to select optimum stiffener arrangement. | en_US |
dc.language.iso | en | en_US |
dc.publisher | IJEUUHAM | en_US |
dc.relation.ispartofseries | Volume 4 ; No 2; | - |
dc.subject | Hypar shell | en_US |
dc.subject | Stiffened | en_US |
dc.subject | Free vibration | en_US |
dc.subject | Finite element analysis | en_US |
dc.subject | Laminated composite | en_US |
dc.title | Fundamental Frequency of Composite Hypar Shell with Stiffener: Optimization of Stiffener Arrangement | en_US |
Appears in Collections: | Civil Engineering (Publications) |
Files in This Item:
File | Description | Size | Format | |
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Fundamental Frequency of Composite Hypar Shell with Stiffener Optimization of Stiffener Arrangement.pdf | 161.41 kB | Adobe PDF | View/Open |
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