The pressure loss of the serial produced and modernized gas turbine combustor with many burners
Автор: Markushin Andrey, Baklanov Andrey, Salimzyanova Guzel
Журнал: Известия Самарского научного центра Российской академии наук @izvestiya-ssc
Рубрика: Авиационная и ракетно-космическая техника
Статья в выпуске: 1-1 т.18, 2016 года.
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The article presents the research results of the pressure loss of the serial produced and modernized gas turbine combustor. Their design and test facility design and also experiment methods are described. The calculations of the effect of the pressure loss on the engine performance are made.
Combustion chamber, design, experimental research, hydraulic loss
Короткий адрес: https://sciup.org/148204349
IDR: 148204349
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