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Experimental, Numerical and Analytical Characterization of Slosh Dynamics Applied to In-Space Propellant Storage, Management and Transfer
本文(外部サイト)http://hdl.handle.net/2060/20150018438
著者(英)Gutierrez, Hector; Lapilli, Gabriel D.; Storey, Jed; Schallhorn, Paul; Kirk, Daniel; Marsell, Brandon
著者所属(英)NASA Kennedy Space Center
発行日2015-07-27
言語eng
内容記述Experimental and numerical results are presented from a new cryogenic fluid slosh program at the Florida Institute of Technology (FIT). Water and cryogenic liquid nitrogen are used in various ground-based tests with an approximately 30 cm diameter spherical tank to characterize damping, slosh mode frequencies, and slosh forces. The experimental results are compared to a computational fluid dynamics (CFD) model for validation. An analytical model is constructed from prior work for comparison. Good agreement is seen between experimental, numerical, and analytical results.
NASA分類Spacecraft Design, Testing and Performance; Propellants and Fuels
レポートNOKSC-E-DAA-TN25160
権利Copyright, Distribution as joint owner in the copyright


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。