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.
- Publication:
-
NASA STI/Recon Technical Report N
- Pub Date:
- January 1983
- Bibcode:
- 1983STIN...8324806P
- Keywords:
-
- Computerized Simulation;
- Heat Pipes;
- Mathematical Models;
- Performance Prediction;
- Spacecraft Radiators;
- Computer Programs;
- Grooves;
- Heat Transfer;
- Pressure Distribution;
- Fluid Mechanics and Heat Transfer