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http://hdl.handle.net/11375/20348
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DC Field | Value | Language |
---|---|---|
dc.contributor.advisor | Siddall, J. N. | - |
dc.contributor.author | Tiwari, Sanat | - |
dc.date.accessioned | 2016-09-08T17:53:58Z | - |
dc.date.available | 2016-09-08T17:53:58Z | - |
dc.date.issued | 1968-05 | - |
dc.identifier.uri | http://hdl.handle.net/11375/20348 | - |
dc.description.abstract | <p> An oblique four bar structural model with fixed member ends, being the most general building block for space frames, is analysed for establishing its influence coefficients, using the Finite Element Matrix Method. </p> <p> Experimental techniques for measurement of the flexibility influence coefficients of the model are described. </p> <p> Experimental results have been compared against analytical ones. </p> | en_US |
dc.language.iso | en | en_US |
dc.subject | Vibration Analysis | en_US |
dc.subject | Design Optimisation | en_US |
dc.subject | Space Frames | en_US |
dc.subject | Static Analysis | en_US |
dc.title | Vibration Analysis and Design Optimisation Studies of Space Frames - Static Analysis | en_US |
dc.contributor.department | Mechanical Engineering | en_US |
dc.description.degreetype | Thesis | en_US |
dc.description.degree | Master of Engineering (MEngr) | en_US |
Appears in Collections: | Open Access Dissertations and Theses |
Files in This Item:
File | Description | Size | Format | |
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Tiwari_S_K_1968May_Masters.pdf | 6.64 MB | Adobe PDF | View/Open |
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