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Validation of Slosh Model Parameters and Anti-Slosh Baffle Designs of Propellant Tanks by Using Lateral Slosh TestingThe 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.
Document ID
20120015663
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Perez, Jose G.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Parks, Russel A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Lazor, Daniel R.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 26, 2013
Publication Date
August 12, 2012
Subject Category
Mechanical Engineering
Report/Patent Number
M12-1537
M12-1538
Meeting Information
Meeting: 27th Aerospace Testing Seminar
Location: Los Angeles, CA
Country: United States
Start Date: October 16, 2012
End Date: October 18, 2012
Sponsors: Aerospace Corp., American Society of Mechanical Engineers, Jet Propulsion Lab., California Inst. of Tech.
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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