Increase the efficiency of multistage compressor by optimization the angles of blades installation
Автор: Matveev Valeriy, Egorov Igor, Kolmakova Dariya, Popov Grigoriy
Журнал: Известия Самарского научного центра Российской академии наук @izvestiya-ssc
Рубрика: Проблемы энергетического машиностроения
Статья в выпуске: 4-2 т.15, 2013 года.
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Bi-criteria optimization of high pressure multistage compressor at gas-turbine engine is performed. As optimized parameters the corners of blades installation were used, and as criteria of optimization – peak efficiencies on two rotation frequencies of the compressor was used.
Numerical model, optimization, multistage compressor
Короткий адрес: https://sciup.org/148202334
IDR: 148202334
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