Title: К вопросу о влиянии окружной неравномерности на динамическую прочность компрессорных лопаток
Other Titles: On the question of circumferential variation effects on dynamic strength of compressor blades
Authors: Попов, Г.М.
Шкловец, А.О.
Колмакова, Д.А.
Issue Date: 2012
Publisher: СГАУ
Citation: Попов, Г. М. К вопросу о влиянии окружной неравномерности на динамическую прочность компрессорных лопаток = On the question of circumferential variation effects on dynamic strength of compressor blades / Г. М. Попов, А. О. Шкловец, Д. А. Колмакова // Самолетостроение России. Проблемы и перспективы: материалы симпозиума с международным участием / Самар. гос. аэрокосм. ун-т. – Самара: СГАУ, 2012. – C. 324-325.
Abstract: The approaches to forced axial compressor blades oscillations calculation are described in present paper. The flow circumferential variation that results in forced blade oscillations was evaluated with CFD methods. A modal calculation and the calculation of forced blade oscillations were carried out with ANSYS software. Resonance frequencies and stresses were calculated. Recommendations for reducing lever of resonance stresses are given.
URI: http://repo.ssau.ru/jspui/handle/123456789/20406
Appears in Collections:Самолетостроение России. Проблемы и перспективы

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