Research Project code：9800000252
Update date：Dec. 15, 2003
Non-steady flow properties of wings and cascades
1975 - 2002
Investigating Researcher (1)：
The purpose of this study is to elucidate the performance of a cascade into which pulsation flow comes from an engine like an exhaust turbine. So far based on a thin airfoil theory we have made a performance estimation of the flow around a single airfoil placed at a flow site where the speed of the flow periodically changes and have confirmed the estimation by an experiment. We are now making a research on cascade performance.
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