| contributor author | J. J. Liu | |
| contributor author | T. P. Hynes | |
| date accessioned | 2017-05-09T00:11:46Z | |
| date available | 2017-05-09T00:11:46Z | |
| date copyright | January, 2003 | |
| date issued | 2003 | |
| identifier issn | 0889-504X | |
| identifier other | JOTUEI-28700#121_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/129300 | |
| description abstract | This paper describes the blade-row models applied to the asymmetric flow-field coupling between turbine and exhaust system. Numerical actuator disk is applied to represent a turbine blade row around the whole annulus and flow properties across the disk can jump to achieve required flow turning and entropy rise. The derivation of disk boundary conditions and the implementation in CFD solvers are described in detail. Validation of the actuator disk model and sample application of the present numerical approach are presented. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | The Investigation of Turbine and Exhaust Interactions in Asymmetric Flows— Blade-Row Models Applied | |
| type | Journal Paper | |
| journal volume | 125 | |
| journal issue | 1 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.1516812 | |
| journal fristpage | 121 | |
| journal lastpage | 127 | |
| identifier eissn | 1528-8900 | |
| keywords | Flow (Dynamics) | |
| keywords | Actuators | |
| keywords | Turbines | |
| keywords | Disks | |
| keywords | Blades | |
| keywords | Boundary-value problems AND Exhaust systems | |
| tree | Journal of Turbomachinery:;2003:;volume( 125 ):;issue: 001 | |
| contenttype | Fulltext | |