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Thermal-Hydraulic-Analysis ProgramELM computer program is simple computational tool for modeling steady-state thermal hydraulics of flows of propellants through fuel-element-coolant channels in nuclear thermal rockets. Evaluates various heat-transfer-coefficient and friction-factor correlations available for turbulent pipe flow with addition of heat. Comparisons possible within one program. Machine-independent program written in FORTRAN 77.
Document ID
19930000786
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Walton, J. T. (NASA Lewis Research Center, Cleveland, OH.)
Date Acquired
August 16, 2013
Publication Date
December 1, 1993
Publication Information
Publication: NASA Tech Briefs
Volume: 17
Issue: 12
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LEW-15423
Accession Number
93B10786
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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