| タイトル | Conceptual design for spacelab two-phase flow experiments |
| 本文（外部サイト） | http://hdl.handle.net/2060/19780006120 |
| 著者（英） | Bradshaw, R. D.; King, C. D. |
| 著者所属（英） | General Dynamics/Convair |
| 発行日 | 1977-12-01 |
| 言語 | eng |
| 内容記述 | KC-135 aircraft tests confirmed the gravity sensitivity of two phase flow correlations. The prime component of the apparatus is a 1.5 cm dia by 90 cm fused quartz tube test section selected for visual observation. The water-cabin air system with water recycle was a clear choice for a flow regime-pressure drop test since it was used satisfactorily on KC-135 tests. Freon-11 with either overboard dump or with liquid-recycle will be used for the heat transfer test. The two experiments use common hardware. The experimental plan covers 120 data points in six hours with mass velocities from 10 to 640 kg/sec-sq m and qualities 0.01 to 0.64. The apparatus with pump, separator, storage tank and controls is mounted in a double spacelab rack. Supporting hardware, procedures, measured variables and program costs are defined. |
| NASA分類 | ASTRONAUTICS (GENERAL) |
| レポートNO | 78N14063
CASD-NAS-77-025
NASA-CR-135327 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/180329 |
