A full-annulus multi-row coupled fluid-structure simulation on a certain high pressure compressor was conducted by an in-house program to analyze the influence of inlet guide vane( IGV) on rotor blade flutter stability in different operation conditions and geometry models. The effectiveness of the program in the field of turbomachinery flutter was verified by numerically simulating the aeroelastic standard configuration 4for the IGV-rotor model and isolated rotor model respectively,detailed fluid-structure ...
【更新日期】
2016-03-17
【分类号】
V232.4
【正文快照】
网络出版地址:www.cnki.net/kcms/detail/11.2625.V.20150401.1627.002.html引用格式:杨慧,李振鹏.转静干涉对转子叶片颤振特性的影响[J].北京航空航天大学学报,2016,42(2):258-264.YANG H,LI Z P.Influence of rotor-stator interaction on rotor blade flutter characteristi
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