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.
- Publication:
-
AIAA, Aerospace Sciences Meeting
- Pub Date:
- January 1985
- Bibcode:
- 1985aiaa.meetR....P
- Keywords:
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- Computerized Simulation;
- Heat Pipes;
- Performance Prediction;
- Spacecraft Radiators;
- Thermal Analysis;
- Capillary Flow;
- Grooves;
- Heat Exchangers;
- Heat Transfer;
- Liquid-Vapor Interfaces;
- Mathematical Models;
- Pressure Drop;
- Thermal Simulation;
- Fluid Mechanics and Heat Transfer