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.
Some Aspects of Thermal Modeling Theory and Analysis as Applied to Spacecraft Temperature Control
Sae Technical Papers
1969 International Automotive Engineering Congress and Exposition ; 1969
1969-02-01
Conference paper
English
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