Aircraft Engineering
Аuthors
Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
Abstract
Design algorithms are obtained for heat engineering systems and heat-loaded vehicle structures. These algorithms based on the temperature equivalence principle allow to develop a set of heat engineering system versions which are equivalent according to non-stationary temperatures of their elements. A special case of the temperature equivalence principle named as instant temperature equivalence is used for this purpose. Besides, a controlled temperature equivalence principle is proposed, which is a generalization of the temperature equivalence principle and provides a generation of a broader set of design versions for heat-loaded vehicle structures.
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