| タイトル | An analytical study of reduced-gravity flow dynamics |
| 本文（外部サイト） | http://hdl.handle.net/2060/19760017416 |
| 著者（英） | Zich, J. L.; Bradshaw, R. D.; Kramer, J. L. |
| 著者所属（英） | General Dynamics/Convair |
| 発行日 | 1976-04-01 |
| 言語 | eng |
| 内容記述 | Addition of surface tension forces to a marker-and-cell code and the performance of four incompressible fluid simulations in reduced gravity, were studied. This marker-and-cell code has a variable grid capability with arbitrary curved boundaries and time dependent acceleration fields. The surface tension logic includes a spline fit of surface marker particles as well as contact angle logic for straight and curved wall boundaries. Three types of flow motion were simulated with the improved code: impulsive settling in a model Centaur LH2 tank, continuous settling in a model and full scale Centaur LO2 tank and mixing in a Centaur LH2 tank. The impulsive settling case confirmed a drop tower analysis which indicated more orderly fluid collection flow patterns with this method providing a potential savings in settling propellants. In the LO2 tank, fluid collection and flow simulation into the thrust barrel were achieved. The mixing simulation produced good results indicating both the development of the flow field and fluid interface behavior. |
| NASA分類 | FLUID MECHANICS AND HEAT TRANSFER |
| レポートNO | 76N24504
CASD-NAS-76-015
NASA-CR-135023 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/185740 |
