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Validation of Slosh Model Parameters and Anti-Slosh Baffle Designs of Propellant Tanks by Using Lateral Slosh Testing
本文(外部サイト)http://hdl.handle.net/2060/20120015663
著者(英)Lazor, Daniel R.; Perez, Jose G.; Parks, Russel A.
著者所属(英)NASA Marshall Space Flight Center
発行日2012-08-12
言語eng
内容記述The slosh dynamics of propellant tanks can be represented by an equivalent pendulum-mass mechanical model. The parameters of this equivalent model, identified as slosh model parameters, are slosh mass, slosh mass center of gravity, slosh frequency, and smooth-wall damping. They can be obtained by both analysis and testing for discrete fill heights. Anti-slosh baffles are usually needed in propellant tanks to control the movement of the fluid inside the tank. Lateral slosh testing, involving both random testing and free-decay testing, are performed to validate the slosh model parameters and the damping added to the fluid by the anti-slosh baffles. Traditional modal analysis procedures are used to extract the parameters from the experimental data. Test setup of sub-scale test articles of cylindrical and spherical shapes will be described. A comparison between experimental results and analysis will be presented.
NASA分類Mechanical Engineering
レポートNOM12-1537
M12-1538
権利No 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。