NASA NTRS ยท 19850037401
Heat pipe modeling and simulation
Abstract
Presented herein is a parametric study of the defining equations which govern the steady state operational characteristics of the Grumman Monogroove Dual Passage Heat Pipe. 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 performed by Grumman on actual prototypes.
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Peterson, G. P.. 1985-01-01. Heat pipe modeling and simulation. https://ntrs.nasa.gov/citations/19850037401
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