JAXA Repository / AIREX 未来へ続く、宙(そら)への英知

このアイテムに関連するファイルはありません。

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NO73N12285
L-8352
NASA-TN-D-6870
権利No Copyright
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/201624


このリポジトリに保管されているアイテムは、他に指定されている場合を除き、著作権により保護されています。