| タイトル | A computer program for anisotropic shallow-shell finite elements using symbolic integration |
| 本文（外部サイト） | http://hdl.handle.net/2060/19760017534 |
| 著者（英） | Andersen, C. M.; Bowen, J. T. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1976-06-01 |
| 言語 | eng |
| 内容記述 | A FORTRAN computer program for anisotropic shallow-shell finite elements with variable curvature is described. A listing of the program is presented together with printed output for a sample case. Computation times and central memory requirements are given for several different elements. The program is based on a stiffness (displacement) finite-element model in which the fundamental unknowns consist of both the displacement and the rotation components of the reference surface of the shell. Two triangular and four quadrilateral elements are implemented in the program. The triangular elements have 6 or 10 nodes, and the quadrilateral elements have 4 or 8 nodes. Two of the quadrilateral elements have internal degrees of freedom associated with displacement modes which vanish along the edges of the elements (bubble modes). The triangular elements and the remaining two quadrilateral elements do not have bubble modes. The output from the program consists of arrays corresponding to the stiffness, the geometric stiffness, the consistent mass, and the consistent load matrices for individual elements. The integrals required for the generation of these arrays are evaluated by using symbolic (or analytic) integration in conjunction with certain group-theoretic techniques. The analytic expressions for the integrals are exact and were developed using the symbolic and algebraic manipulation language. |
| NASA分類 | STRUCTURAL MECHANICS |
| レポートNO | 76N24622
NASA-TM-X-3325
L-10483 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/185732 |
