Application of the temperature equivalence principle for design of heat engineering systems with variable composition

Aircraft Engineering


Аuthors

Avkhimovich B. M.

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.

mai.ru — informational site of MAI

Copyright © 1994-2024 by MAI