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Experimental, Numerical and Analytical Characterization of Slosh Dynamics Applied to In-Space Propellant Storage, Management and TransferExperimental 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.
Document ID
20160001427
Acquisition Source
Kennedy Space Center
Document Type
Conference Paper
Authors
Storey, Jedediah M.
(Florida Inst. of Tech. Melbourne, FL, United States)
Kirk, Daniel
(Florida Inst. of Tech. Melbourne, FL, United States)
Gutierrez, Hector
(Florida Inst. of Tech. Melbourne, FL, United States)
Marsell, Brandon
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Schallhorn, Paul
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Lapilli, Gabriel D.
(Florida Inst. of Tech. Melbourne, FL, United States)
Date Acquired
February 2, 2016
Publication Date
July 27, 2015
Subject Category
Fluid Mechanics And Thermodynamics
Propellants And Fuels
Report/Patent Number
KSC-E-DAA-TN24557
Report Number: KSC-E-DAA-TN24557
Meeting Information
Meeting: AIAA/SAE/ASEE Joint Propulsion Conference
Location: Orlando, FL
Country: United States
Start Date: July 27, 2015
End Date: July 29, 2015
Sponsors: American Society for Electrical Engineers, Society of Automotive Engineers, Inc., American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNX14AM08H
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
slosh mode frequencies
slosh
cryogenics
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