| タイトル | Study of propellant dynamics in a shuttle type launch vehicle |
| 本文（外部サイト） | http://hdl.handle.net/2060/19730009074 |
| 著者（英） | Jones, C. E.; Feng, G. C. |
| 著者所属（英） | Lockheed Missiles and Space Co. |
| 発行日 | 1972-04-01 |
| 言語 | eng |
| 内容記述 | A method and an associated digital computer program for evaluating the vibrational characteristics of large liquid-filled rigid wall tanks of general shape are presented. A solution procedure was developed in which slosh modes and frequencies are computed for systems mathematically modeled as assemblages of liquid finite elements. To retain sparsity in the assembled system mass and stiffness matrices, a compressible liquid element formulation was incorporated in the program. The approach taken in the liquid finite element formulation is compatible with triangular and quadrilateral structural finite elements so that the analysis of liquid motion can be coupled with flexible tank wall motion at some future time. The liquid element repertoire developed during the course of this study consists of a two-dimensional triangular element and a three-dimensional tetrahedral element. |
| NASA分類 | PROPELLANTS |
| レポートNO | 73N17801
NASA-CR-124070
HREC-7012-1
LMSC/HREC-D225823 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/200559 |
