タイトル | Ring baffle pressure distribution and slosh damping in large cylindrical tanks |
本文(外部サイト) | http://hdl.handle.net/2060/19730003558 |
著者(英) | Scholl, H. F.; Stephens, D. G.; Davis, P. K. |
著者所属(英) | NASA Langley Research Center |
発行日 | 1972-12-01 |
言語 | eng |
内容記述 | An investigation was conducted to determine the pressure loads and damping associated with rigid ring baffles in relatively large cylindrical tanks. The radial and circumferential pressure distribution, as well as the damping, was measured on a ring baffle subjected to fundamental antisymmetric slosh in a 284-cm-diameter rigid tank. Experimental and analytical data are presented as a function of slosh velocity or amplitude, baffle spacing, and baffle locations both above and below the liquid surface. Results suggest that pressure distributions and damping values can be determined from available theories for the design of single and multiple baffle configurations. |
NASA分類 | FLUID MECHANICS |
レポートNO | 73N12285 L-8352 NASA-TN-D-6870 |
権利 | No Copyright |
URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/201624 |