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NASA NTRS ยท 19830016535

Computer modeling of heat pipe performance

Abstract

A 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.

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BibTeXRIS

Peterson, G. P.. 1983-01-13. Computer modeling of heat pipe performance. https://ntrs.nasa.gov/citations/19830016535

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