| タイトル | Development of a solid hexahedron finite dynamic element |
| 著者（英） | Gupta, K. K. |
| 著者所属（英） | NASA Flight Research Center |
| 発行日 | 1984-11-01 |
| 言語 | eng |
| 内容記述 | This paper presents the pertinent details of a newly developed solid rectangular hexahedron finite dynamic element, involving the derivation of the higher order stiffness and inertia dynamic correction matrices. Numerical results of a test case are also presented which indicate that adoption of the dynamic elements significantly improves the solution convergence, when compared with the related performance of the corresponding finite elements. |
| NASA分類 | STRUCTURAL MECHANICS |
| レポートNO | 85A16262 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/394042 |
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