Simulation of subsonic flow in compressor blade cascade
DOI:
https://doi.org/10.15587/1729-4061.2012.3760Keywords:
Flow simulation, compressor blade cascade, boundary layerAbstract
The results of simulation of subsonic flow in compressor blade cascade are presented in the work. Comparison results of numerical and physical experiments are givenReferences
- Терещенко Ю.М. Аэродинамическое совершенствование лопаточных аппаратов компрессоров / Ю.М. Терещенко // – М.: Машиностроение, 1987. – 168с.
- Дейч М.Е. Техническая газодинамика / М.Е. Дейч // – М.-Л.: Госэнергоиздат, 1961. – 672с.
- Бунимович А.И., Святогоров А.А. Аэродинамические характеристики плоских компрессорных решеток при большой дозвуковой скорости //Лопаточные машины и струйные аппараты.– М.: Машиностроение. – 1967. – №2. – С.5-35.
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Copyright (c) 2014 Юрий Матвеевич Терещенко, Иван Алексеевич Ластивка, Екатерина Викторовна Дорошенко
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