|
Fuel combustion in combustion chambers of a gas-turbine engine with a rotating injector
I. A. Kholmyanskii Siberian State Automobile-Road Academy, Omsk, 644080
Abstract:
Specific features of combustion in combustion chambers of a gas-turbine engine with a rotating injector are considered. The region of the combustion site and the temperature field are found. A method for three-dimensional simulation of heat and mass transfer is described. The calculation results are compared with the temperature fields of real engines.
Keywords:
combustion, heat and mass transfer, combustion chamber, gas-turbine engine, rotating injector.
Received: 15.05.2001 Accepted: 20.08.2003
Citation:
I. A. Kholmyanskii, “Fuel combustion in combustion chambers of a gas-turbine engine with a rotating injector”, Fizika Goreniya i Vzryva, 40:4 (2004), 54–59; Combustion, Explosion and Shock Waves, 40:4 (2004), 419–424
Linking options:
https://www.mathnet.ru/eng/fgv1791 https://www.mathnet.ru/eng/fgv/v40/i4/p54
|
Statistics & downloads: |
Abstract page: | 21 |
|