Flutter Mechanisms in Low Pressure Turbine Blades
نویسندگان
چکیده
منابع مشابه
Aiaa 2001-0447 Experimental Investigation of Separation on Low Pressure Turbine Blades
Measurements of the flow field around a low pressure turbine blade are presented. The purpose of the experimental study is to investigate the detailed transition and separation characteristics on low pressure turbine blades. The present study focuses on the effect of Reynolds number on the formation of separation bubbles on the turbine blade surface. Specific attention is paid to the flow withi...
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ژورنال
عنوان ژورنال: Journal of Engineering for Gas Turbines and Power
سال: 1999
ISSN: 0742-4795,1528-8919
DOI: 10.1115/1.483179