| contributor author | V. Cyrus | |
| date accessioned | 2017-05-08T23:28:30Z | |
| date available | 2017-05-08T23:28:30Z | |
| date copyright | October, 1988 | |
| date issued | 1988 | |
| identifier issn | 0889-504X | |
| identifier other | JOTUEI-28592#434_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/104619 | |
| description abstract | A detailed investigation of the three-dimensional flow was carried out in a low-speed rear axial compressor stage with an aspect ratio of 1. Experimental data were obtained for both an inlet velocity profile with thin endwall boundary layer thickness and a distorted inlet velocity profile with a high turbulence intensity level. The distortion was produced by a specially designed screen. The flow mechanism in the rotor and stator blade rows is analyzed for these two velocity profiles at the design flow coefficient. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Effect of the Inlet Velocity Profile in the Three-Dimensional Flow in a Rear Axial Compressor Stage | |
| type | Journal Paper | |
| journal volume | 110 | |
| journal issue | 4 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.3262216 | |
| journal fristpage | 434 | |
| journal lastpage | 440 | |
| identifier eissn | 1528-8900 | |
| tree | Journal of Turbomachinery:;1988:;volume( 110 ):;issue: 004 | |
| contenttype | Fulltext | |
