| contributor author | Yang, B. | |
| contributor author | Gu, Ch. G. | |
| date accessioned | 2017-05-09T01:03:26Z | |
| date available | 2017-05-09T01:03:26Z | |
| date issued | 2013 | |
| identifier issn | 0889-504X | |
| identifier other | turb_135_1_011039.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/153403 | |
| description abstract | In this study, experiments and numerical simulations were carried out to evaluate the effects of radially distorted incident flow on the performance of axialflow fans, which were equipped with three kinds of forwardskewed blades. Loss coefficient and velocity components at exit section as well as overall performance are discussed, both at the design point and the lower mass flow rate point. Furthermore, rotating stall was also observed by use of three dynamic pressure sensors. All results reveal that there are beneficial effects of forwardskewed blades on the fan performance, but the fan performance and its unsteady aerodynamic characteristics are quite affected by the radially distorted incident flow. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | The Effects of Radially Distorted Incident Flow on Performance of Axial Flow Fans With Forward Skewed Blades | |
| type | Journal Paper | |
| journal volume | 135 | |
| journal issue | 1 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.4006535 | |
| journal fristpage | 11039 | |
| journal lastpage | 11039 | |
| identifier eissn | 1528-8900 | |
| tree | Journal of Turbomachinery:;2013:;volume( 135 ):;issue: 001 | |
| contenttype | Fulltext | |