| contributor author | R. P. Dring | |
| contributor author | D. A. Spear | |
| date accessioned | 2017-05-08T23:36:54Z | |
| date available | 2017-05-08T23:36:54Z | |
| date copyright | October, 1991 | |
| date issued | 1991 | |
| identifier issn | 0889-504X | |
| identifier other | JOTUEI-28615#600_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/109353 | |
| description abstract | A methodology based on wake mixing has been developed that enables more accurate predictions of compressor airfoil pressure distributions when the airfoil is operating downstream of an airfoil row that has strong wakes. The methodology has an impact on throughflow analysis, on airfoil-to-airfoil flow analysis, and on the interpretation of experimental data. It is demonstrated that the flow in the endwall region is particularly sensitive to mixing due to the strong wakes caused by the secondary flow and corner separation that commonly occur in this region. It is also demonstrated that wake mixing can have a strong impact on both airfoil incidence and deviation as well as on loading. Differences of up to 13 deg and 30 percent in loading are demonstrated. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | The Effects of Wake Mixing on Compressor Aerodynamics | |
| type | Journal Paper | |
| journal volume | 113 | |
| journal issue | 4 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.2929121 | |
| journal fristpage | 600 | |
| journal lastpage | 607 | |
| identifier eissn | 1528-8900 | |
| keywords | Aerodynamics | |
| keywords | Compressors | |
| keywords | Wakes | |
| keywords | Airfoils | |
| keywords | Flow (Dynamics) | |
| keywords | Pressure | |
| keywords | Separation (Technology) AND Corners (Structural elements) | |
| tree | Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 004 | |
| contenttype | Fulltext | |
