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Transitional Flow in Thin Tubes for Space Station Freedom RadiatorA two dimensional finite volume method is used to predict the film coefficients in the transitional flow region (laminar or turbulent) for the radiator panel tubes. The code used to perform this analysis is CAST (Computer Aided Simulation of Turbulent Flows). The information gathered from this code is then used to augment a Sinda85 model that predicts overall performance of the radiator. A final comparison is drawn between the results generated with a Sinda85 model using the Sinda85 provided transition region heat transfer correlations and the Sinda85 model using the CAST generated data.
Document ID
19950020939
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Patrick Loney
(NYMA, Inc. Brook Park, OH, United States)
Mounir Ibrahim
(Cleveland State University Cleveland, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1995
Publication Information
Publication: The Sixth Annual Thermal and Fluids Analysis Workshop
Publisher: National Aeronautics and Space Administration
Subject Category
Fluid Mechanics and Thermodynamics
Report/Patent Number
CP-10161
Meeting Information
Meeting: The Sixth Annual Thermal and Fluids Analysis Workshop
Location: Brook Park, OH
Country: US
Start Date: August 15, 1994
End Date: August 19, 1994
Sponsors: National Aeronautics and Space Administration, Ohio Aerospace Institute
Accession Number
95N27360
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
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