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Computer modeling of heat pipe performanceA parametric study of the defining equations which govern the steady state operational characteristics of the Grumman monogroove dual passage heat pipe is presented. These defining equations are combined to develop a mathematical model which describes and predicts the operational and performance capabilities of a specific heat pipe given the necessary physical characteristics and working fluid. Included is a brief review of the current literature, a discussion of the governing equations, and a description of both the mathematical and computer model. Final results of preliminary test runs of the model are presented and compared with experimental tests on actual prototypes.
Document ID
19830016535
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Peterson, G. P.
(Texas A&M Univ. College Station, TX, United States)
Date Acquired
September 4, 2013
Publication Date
January 13, 1983
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-171641
NAS 1.26:171641
Report Number: NASA-CR-171641
Report Number: NAS 1.26:171641
Accession Number
83N24806
Funding Number(s)
CONTRACT_GRANT: NAS9-16606
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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