An Experimental Investigation on Aerodynamic Interblade Interactions of a Vibrating Cascade in Transonic Flow
スポンサーリンク
概要
- 論文の詳細を見る
The characteristics of the aerodynamic interblade interaction of the vibrating cascade in transonic flow are examined by a "one-blade oscillation method" and some aspects of aerodynamic interblade interaction which are hidden in case of the conventional "all-blades vibration method" are clarified. In the report, the effects of the compressibility of the flow on the aerodynamic interactions are clarified and the reasons why the characteristics of the aerodynamic damping of the uniform cascade are varied with the Mach number, reduced frequency and interblade phase angle are elucidated.
- 一般社団法人日本機械学会の論文
- 1987-12-16
著者
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YAMAGUCHI Kazuo
Institute for Gene Research, Kanazawa University
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Hanamura Yoji
Institute Of Space And Aeronautical Science University Of Tokyo
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Hanamura Yoji
Institue Of Interdisciplinary Research Faculty Of Engineering University Of Tokyo
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Yamaguchi Kazuo
Institue Of Interdisciplinary Research Faculty Of Engineering University Of Tokyo
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