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Abstract
Three-dimensional unsteady aerodynamic interaction in a turbine stage, which has a great effect on aerodynamic stage performance, has attracted attention from researchers. To elucidate this effect, we have investigated the flow field by using high-precision three-dimensional Navier-Stokes solver ; where blade-count ratio is almost the same as that of a real turbine. Axial spacing between rotor and stator is changed. We have compared experimental timeaveraged pneumatic pressure data measured by five-hole pitot probe with numerical results.
Journal
- 年次大会講演論文集 : JSME annual meeting [List of Volumes]
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年次大会講演論文集 : JSME annual meeting 2006(2), 155-156, 2006-09-15 [Table of Contents]
The Japan Society of Mechanical Engineers