Proj
J-GLOBAL ID:200904022454681714  Research Project code:9800000252 Update date:Dec. 15, 2003

Non-steady flow properties of wings and cascades

翼および翼列の非定常流特性
Study period:1975 - 2002
Organization (1):
Investigating Researcher (1):
Research overview:
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.
Keywords (6):
cascade ,  blade(machine) ,  unsteady ,  flow ,  hydrodynamic ,  steam
Research program: Ordinary Research
Research budget: 1996: \0

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