Mathematical model for calculating the mass of a heat exchanger in problems of optimizing the parameters of the working process of aircraft gas turbine engines

Despite the fact that aviation gas turbine engines (GTE) have reached a high degree of sophistication, requirements for the improvement of their efficiency are constantly increasing. Reduction of specific fuel consumption and specific weight of the engine unit makes it possible to improve aircraft p...

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Bibliographic Details
Main Authors: V. S. Kuz'michev, H. Omar, A. Yu. Tkachenko, A. A. Bobrik
Format: Article
Language:English
Published: Samara National Research University 2019-10-01
Series:Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение
Subjects:
Online Access:https://journals.ssau.ru/index.php/vestnik/article/view/7455