Publication Date:
2019-07-13
Description:
The status of an effort to increase the efficiency of calculating transient temperature fields in complex aerospace vehicle structures is described. The advantages and disadvantages of explicit and implicit algorithms are discussed. A promising set of implicit algorithms with variable time steps, known as the GEAR package is described. Four test problems, used for evaluating and comparing various algorithms, have been selected and finite-element models of the configurations are described. These problems include a Space Shuttle frame component, an insulated cylinder, a metallic panel for a thermal protection system, and a model of the Space Shuttle Orbiter wing. Results generally indicate a preference for implicit over explicit algorithms for solution of transient structural heat transfer problems when the governing equations are 'stiff' (typical of many practical problems such as insulated metal structures).
Keywords:
SPACECRAFT DESIGN, TESTING AND PERFORMANCE
Type:
ASME PAPER 81-WA/HT-4
,
Winter Annual Meeting; Nov 15, 1981 - Nov 20, 1981; Washington, DC
Format:
text
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