ATTENTION: The works hosted here are being migrated to a new repository that will consolidate resources, improve discoverability, and better show UTA's research impact on the global community. We will update authors as the migration progresses. Please see MavMatrix for more information.
Show simple item record
dc.contributor.advisor | Wang, Bo Ping | |
dc.creator | Wang, Xingzhi | |
dc.date.accessioned | 2018-06-05T16:35:59Z | |
dc.date.available | 2018-06-05T16:35:59Z | |
dc.date.created | 2018-05 | |
dc.date.issued | 2018-04-25 | |
dc.date.submitted | May 2018 | |
dc.identifier.uri | | |
dc.identifier.uri | http://hdl.handle.net/10106/27380 | |
dc.description.abstract | Finite Element Method (FEM) is widely used in structural analysis, and the standard approach to increase the accuracy of analysis is increasing the total degrees of freedom (DOFs), namely, refine the mesh. By introducing the rotational DOFs, better accuracy can be achieved without change the mesh. The objective of this study was to investigate the performance of elements with rotational DOFs in statics and dynamics analysis and applying these elements to optimization. The implementation of three representative elements with rotational DOFs for statics analysis is reproduced. Also, this work implements these elements to dynamics analysis and optimization. The results show the performance of elements with rotational DOFs is better than the regular element in both statics and dynamics analysis. | |
dc.format.mimetype | application/pdf | |
dc.language.iso | en_US | |
dc.subject | FEM | |
dc.subject | Rotational DOF | |
dc.subject | Quadrilateral element | |
dc.subject | Dynamics | |
dc.title | THE PERFORMANCE OF QUADRILATERAL ELEMENT WITH ROTATIONAL DEGREES OF FREEDOM IN STATICS AND DYNAMICS ANALYSIS AND OPTIMIZATION | |
dc.type | Thesis | |
dc.degree.department | Mechanical and Aerospace Engineering | |
dc.degree.name | Master of Science in Aerospace Engineering | |
dc.date.updated | 2018-06-05T16:37:03Z | |
thesis.degree.department | Mechanical and Aerospace Engineering | |
thesis.degree.grantor | The University of Texas at Arlington | |
thesis.degree.level | Masters | |
thesis.degree.name | Master of Science in Aerospace Engineering | |
dc.type.material | text | |
dc.creator.orcid | 0000-0003-4829-3968 | |
Files in this item
- Name:
- WANG-THESIS-2018.pdf
- Size:
- 1.498Mb
- Format:
- PDF
This item appears in the following Collection(s)
Show simple item record