Study of Internal Flows in a Mixed-Flow Pump Impeller at Various Tip Clearances Using Three-Dimensional Viscous Flow ComputationsSource: Journal of Turbomachinery:;1992:;volume( 114 ):;issue: 002::page 373Author:A. Goto
DOI: 10.1115/1.2929154Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The complex three-dimensional flow fields in a mixed-flow pump impeller are investigated by applying the incompressible version of Dawes’ Three-Dimensional Navier–Stokes code. The applicability of the code is confirmed by comparison of computations with a variety of experimentally measured jet-wake flow patterns and overall performances at four different tip clearances, including the shrouded case. Based on the computations, the interaction mechanism of secondary flows and the formation of jet-wake flow are discussed. In the case of large tip clearances, the reverse flow caused by tip leakage flow is considered to be the reason for the thickening of the casing boundary layer followed by the deterioration of the whole flow field.
keyword(s): Flow (Dynamics) , Viscous flow , Internal flow , Computation , Pump impellers , Wakes , Boundary layers , Mechanisms AND Leakage flows ,
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| contributor author | A. Goto | |
| date accessioned | 2017-05-08T23:39:56Z | |
| date available | 2017-05-08T23:39:56Z | |
| date copyright | April, 1992 | |
| date issued | 1992 | |
| identifier issn | 0889-504X | |
| identifier other | JOTUEI-28619#373_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/111099 | |
| description abstract | The complex three-dimensional flow fields in a mixed-flow pump impeller are investigated by applying the incompressible version of Dawes’ Three-Dimensional Navier–Stokes code. The applicability of the code is confirmed by comparison of computations with a variety of experimentally measured jet-wake flow patterns and overall performances at four different tip clearances, including the shrouded case. Based on the computations, the interaction mechanism of secondary flows and the formation of jet-wake flow are discussed. In the case of large tip clearances, the reverse flow caused by tip leakage flow is considered to be the reason for the thickening of the casing boundary layer followed by the deterioration of the whole flow field. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Study of Internal Flows in a Mixed-Flow Pump Impeller at Various Tip Clearances Using Three-Dimensional Viscous Flow Computations | |
| type | Journal Paper | |
| journal volume | 114 | |
| journal issue | 2 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.2929154 | |
| journal fristpage | 373 | |
| journal lastpage | 382 | |
| identifier eissn | 1528-8900 | |
| keywords | Flow (Dynamics) | |
| keywords | Viscous flow | |
| keywords | Internal flow | |
| keywords | Computation | |
| keywords | Pump impellers | |
| keywords | Wakes | |
| keywords | Boundary layers | |
| keywords | Mechanisms AND Leakage flows | |
| tree | Journal of Turbomachinery:;1992:;volume( 114 ):;issue: 002 | |
| contenttype | Fulltext |