Numerical Simulation of Performance of Micro Gas Turbine Engine Combustion Chamber Taking into Account Oil Addition to Fuel

被引：0
|
作者：
Bulat, P.V. [1 ]
Vokin, L.O. [1 ]
Volkov, K.N. [1 ]
Nikitenko, A.B. [1 ]
Prodan, N.V. [1 ]
Renev, M.E. [1 ]
机构：
[1] Ustinov Baltic State Technical University VOENMEH, ul. Pervaya Krasnoarmeiskaya 1, St. Petersburg,190005, Russia
来源：
Russian Aeronautics | 2024年 / 67卷 / 03期
关键词：
Aircraft fuels - Combustion chambers - Fuel oils - Photodissociation - Turbine components - Unmanned aerial vehicles (UAV);
D O I：
10.3103/S1068799824030140
中图分类号：
学科分类号：
摘要：
Abstract: This paper presents a model of working processes in the combustion chambers of micro gas turbine engines, taking into account turbulence, combustion, the detailed mechanism of chemical reactions, radiation, swirling flow, and the presence of oil in the fuel mixture. The results of calculations and experiments with the combustion chamber of the JetCat P100-RX engine are presented. Estimates of the addition of oil to fuel for fuel consumption are given. © Allerton Press, Inc. 2024.
引用
收藏
页码：594 / 600
页数：6
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