Methodology and algorithm determining the temperature dependence of thermal and physical characteristics for anisotropic materials basing on an inverse problem solution

Spacecraft and Rockets


Аuthors

Alifanov O. M.*, Ivanov N. A.**, Kolesnikov V. A.***

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

*e-mail: o.alifanov@yandex.ru
**e-mail: tdm1@mail.ru
***e-mail: v.kolesnikov@mail.ru

Abstract

Developed a methodical approach, algorithm and computer program for determining thermal characteristics are widely used in aviation and space technology anisotropic materials. Methodical approach is based on a solution of inverse heat conductivity problem stated as an extremal one. The effectiveness of the use of the recommended approach is illustrated by the example of recovery of the thermal conductivity tensor and volumetric heat capacity of the composite perspective on the results of physical experiments with a sample of this material.

Keywords:

the inverse problem, thermal conductivity tensor, anisotropic materials, volumetric heat capacity, space technology

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