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Experimental Results of Hydrogen Slosh in a 62 Cubic Foot (1750 Liter) TankExtensive slosh testing with liquid and slush hydrogen was conducted in a 62 cubic foot spherical tank to characterize the thermodynamic response of the system under normal gravity conditions. Slosh frequency and amplitude, pressurant type, ramp pressure, and ullage volume were parametrically varied to assess the effect of each of these parameters on the tank pressure and fluid/wall temperatures. A total of 91 liquid hydrogen and 62 slush hydrogen slosh tests were completed. Both closed tank tests and expulsions during sloshing were performed. This report presents and discusses highlights of the liquid hydrogen closed tank results in detail and introduces some general trends for the slush hydrogen tests. Summary comparisons between liquid and slush hydrogen slosh results are also presented.
Document ID
19940030744
Acquisition Source
Headquarters
Document Type
Conference Paper
Authors
Moran, Matthew E.
(NASA Lewis Research Center Cleveland, OH, United States)
Mcnelis, Nancy B.
(NASA Lewis Research Center Cleveland, OH, United States)
Kudlac, Maureen T.
(NASA Lewis Research Center Cleveland, OH, United States)
Haberbusch, Mark S.
(NASA Lewis Research Center Cleveland, OH, United States)
Satornino, George A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1994
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
E-8916
NASA-TM-106625
AIAA PAPER 94-3259
NAS 1.15:106625
Report Number: E-8916
Report Number: NASA-TM-106625
Report Number: AIAA PAPER 94-3259
Report Number: NAS 1.15:106625
Meeting Information
Meeting: Joint Propulsion Conference
Location: Indianapolis, IN
Country: United States
Start Date: June 27, 1994
End Date: June 29, 1994
Sponsors: AIAA, ASME, SAE, and ASEE
Accession Number
94N35250
Funding Number(s)
CONTRACT_GRANT: NAS3-25517
Distribution Limits
Public
Copyright
Public Use Permitted.
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