Influence of Simplifying a Geometrical Model of the Gas Turbine Engine Combustion Chamber on the Results of Numerical Modeling


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We studied the geometric models of combustion chambers depending on their simplification. It is shown that the error in calculating the parameters does not exceed 8 % under the constraint of the geometrical model of the gas turbine engine (GTE) combustion chamber by an angular sector with a burner device.

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Yu. Aleksandrov

Tupolev Kazan National Research Technical University

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Email: alexwischen@rambler.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, 420111 Tatarstan

A. Sabirzyanov

Tupolev Kazan National Research Technical University

Email: alexwischen@rambler.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, 420111 Tatarstan

V. Yavkin

Tupolev Kazan National Research Technical University

Email: alexwischen@rambler.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, 420111 Tatarstan

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