| contributor author | T. Wright | |
| contributor author | S. Madhavan | |
| contributor author | J. DiRe | |
| date accessioned | 2017-05-08T23:17:43Z | |
| date available | 2017-05-08T23:17:43Z | |
| date copyright | October, 1984 | |
| date issued | 1984 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26610#895_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/98381 | |
| description abstract | Efforts to quantify degradation of the performance of a centrifugal fan subjected to distorted inflows are presented. The study centered on examination of pressure rise, efficiency, and onset of stall for a backwardly-inclined, airfoil-bladed fan. Nonuniform flow patterns were generated in an adjustable countervane damper assembly installed upstream of the inlet box, and systematic families of performance curves were generated. Results of these tests show that significant degradation in efficiency and pressure rise—as much as 10 to 15 percent—may result from moderately to severely distorted inflow patterns. Onset of stall was significantly influenced by severely distorted inflows. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Centrifugal Fan Performance With Distorted Inflows | |
| type | Journal Paper | |
| journal volume | 106 | |
| journal issue | 4 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3239654 | |
| journal fristpage | 895 | |
| journal lastpage | 900 | |
| identifier eissn | 0742-4795 | |
| keywords | Inflow | |
| keywords | Pressure | |
| keywords | Flow (Dynamics) | |
| keywords | Manufacturing | |
| keywords | Dampers AND Airfoils | |
| tree | Journal of Engineering for Gas Turbines and Power:;1984:;volume( 106 ):;issue: 004 | |
| contenttype | Fulltext | |
