DEVELOPMENT OF SOFTWARE FOR CALCULATION AND MATHEMATICAL MODELING OF THE FLOW PARTS OF TURBOJET ENGINE


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Abstract

To date, the turbojet dual-circuit engine (turbojet) is the most common air-jet aircraft engine due to low fuel consumption and a number of other advantages. The purpose of this work is to develop a software package for calculating the parameters of the flow part of the turbojet with an intuitive and user-friendly modern interface that allows further expansion of the functionality due to the modular architecture. The developed software package is allowed to raise the process of designing the flow part of the turbojet to a higher level, thereby reducing not only the time of its development, but also the costs.

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About the authors

Sergey Alexandrovich Gusarov

Moscow Aviation Institute (National Research University)

Email: gus@mai.ru
candidate of technical Sciences, senior researcher; associate Professor of 201 "Theory of Air-Jet Engines" Moscow, Russian Federation

Vladimir Nikolaevich Karasev

Moscow Aviation Institute (National Research University)

Email: vkar69@yandex.ru
candidate of technical Sciences, associate professor; associate Professor of 201 "Theory of Air-Jet Engines" Moscow, Russian Federation

Yuri Alexandrovich Kostikov

Moscow Aviation Institute (National Research University)

Email: kostikov@mail.ru
candidate of physical and mathematical Sciences; head of the Department 812 "Mathematics" Moscow, Russian Federation

Yuri Alexandrovich Rzhavin

Moscow Aviation Institute (National Research University)

Email: gus@mai.ru
candidate of technical Sciences, professor; professor of the Department 201 "Theory of Air-Jet Engines" Moscow, Russian Federation

Aleksandr Mikhailovich Romanenkov

Moscow Aviation Institute (National Research University); Federal Research Center «Informaticsand Management» ofthe Russian Academyof Sciences

Email: romanaleks@gmail.com
candidate of technical Sciences; associate professor of 812 "Mathematics"; senior researcher Moscow, Russian Federation

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