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Modeling of Thermal Performance of Multiphase Nuclear Fuel Cell Under Variable Gravity ConditionsA unique numerical method has been developed to model the dynamic processes of bulk evaporation and condensation processes, associated with internal heat generation and natural convection under different gravity levels. The internal energy formulation, for the bulk liquid-vapor phase change problems in an encapsulated container, was employed. The equations, governing the conservation of mass, momentum and energy for both phases involved in phase change, were solved. The thermal performance of a multiphase uranium tetra-fluoride fuel element under zero gravity, micro-gravity and normal gravity conditions has been investigated. The modeling yielded results including the evolution of the bulk liquid-vapor phase change process, the evolution of the liquid-vapor interface, the formation and development of the liquid film covering the side wall surface, the temperature distribution and the convection flow field in the fuel element. The strong dependence of the thermal performance of such multiphase nuclear fuel cell on the gravity condition has been revealed. Under all three gravity conditions, 0-g, 10(exp -3)-g, and 1-g, the liquid film is formed and covers the entire side wall. The liquid film covering the side wall is more isothermalized at the wall surface, which can prevent the side wall from being over-heated. As the gravity increases, the liquid film is thinner, the temperature gradient is larger across the liquid film and smaller across the vapor phase. This investigation provides valuable information about the thermal performance of multi-phase nuclear fuel element for the potential space and ground applications.
Document ID
19960047487
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ding, Z.
(Florida Univ. Gainesville, FL United States)
Anghaie, S.
(Florida Univ. Gainesville, FL United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1996
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
E-9884
NASA-CR-198391
NAS 1.26:198391
Report Number: E-9884
Report Number: NASA-CR-198391
Report Number: NAS 1.26:198391
Accession Number
96N33153
Funding Number(s)
CONTRACT_GRANT: NAS3-26314
PROJECT: RTOP 233-01-0N
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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