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Heat Transfer and Pressure Drop in Concentric Annular Flows of Binary Inert Gas MixturesStudies of heat transfer and pressure drop of binary inert gas mixtures flowing through smooth concentric circular annuli, tubes with fully developed velocity profiles, and constant heating rate are described. There is a general lack of agreement among the constant property heat transfer correlations for such mixtures. No inert gas mixture data exist for annular channels. The intent of this study was to develop highly accurate and benchmarked pressure drop and heat transfer correlations that can be used to size heat exchangers and cores for direct gas Brayton nuclear power plants. The inside surface of the annular channel is heated while the outer surface of the channel is insulated. Annulus ratios range 0.5 < r* < 0.83. These smooth tube data may serve as a reference to the heat transfer and pressure drop performance in annuli, tubes, and channels having helixes or spacer ribs, or other surfaces.
Document ID
20080006635
Acquisition Source
Marshall Space Flight Center
Document Type
Technical Memorandum (TM)
Authors
Reid, R. S.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Martin, J. J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Yocum, D. J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Stewart, E. T.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 24, 2013
Publication Date
November 1, 2007
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
NASA/TM-2007-215135
M-1210
Report Number: NASA/TM-2007-215135
Report Number: M-1210
Distribution Limits
Public
Copyright
Public Use Permitted.
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