IDENTIFICATION OF СOMPLICATED MECHANICAL SYSTEM PARAMETERS AT THERMAL FORCE ACTION

Empirical dependences for calculating reliability and mass of an aviation engine are obtained with the help of a regression analysis method and test of the obtained expression adequacy has been carried as well.A model for degradation of the effective, elastic and heat-conducting material properties...

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Bibliographic Details
Main Authors: A. V. Chigarev, D. N. Mironov
Format: Article
Language:Russian
Published: Belarusian National Technical University 2009-02-01
Series:Наука и техника
Online Access:https://sat.bntu.by/jour/article/view/618
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