This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
Some Aspects of Thermal Modeling Theory and Analysis as Applied to Spacecraft Temperature Control
Annotation ability available
Sector:
Language:
English
Abstract
A description of digital computer methods and numerical techniques which are used in evaluating temperature distributions in spacecraft structures is presented.
The theory and application of thermal modeling from the point of view of comparing the accuracy of simplified analytical models with zonal and nodal methods are discussed, and an example is given to illustrate the general theory.
Authors
Citation
Karam, R. and Eby, R., "Some Aspects of Thermal Modeling Theory and Analysis as Applied to Spacecraft Temperature Control," SAE Technical Paper 690199, 1969, https://doi.org/10.4271/690199.Also In
References
- Richtmyer R. D. “Difference Methods for Initial-Value Problems.” New York Interscience Publishers, Inc. 1956
- Anderson J. T. “A Review of Digital-Computer Heat Transfer Programs.” ASME Paper 65-WA/HT-48 1965
- Koffel W. K. “Transient Heat Transfer Program -- Experience and Extensions.” Oct. 29 1959