| contributor author | Shaw, M. J. | |
| contributor author | Hield, P. | |
| contributor author | Tucker, P. G. | |
| date accessioned | 2017-05-09T01:13:21Z | |
| date available | 2017-05-09T01:13:21Z | |
| date issued | 2014 | |
| identifier issn | 0889-504X | |
| identifier other | turb_136_02_021015.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/156542 | |
| description abstract | An investigation was carried out into the effects of variable inlet guide vanes (VIGVs) on the performance and stability margin of a transonic fan in the presence of inlet flow distortion. The study was carried out using computational fluid dynamics (CFD) and validated with experimental data. The capability of CFD to predict the changes in performance with or without VIGVs in the presence of an inlet flow distortion is assessed. Results show that the VIGVs improve the performance and stability margin and do so by reducing the amount of swirl at inlet to the rotor component of the fan. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | The Effect of Inlet Guide Vanes on Inlet Flow Distortion Transfer and Transonic Fan Stability | |
| type | Journal Paper | |
| journal volume | 136 | |
| journal issue | 2 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.4024906 | |
| journal fristpage | 21015 | |
| journal lastpage | 21015 | |
| identifier eissn | 1528-8900 | |
| tree | Journal of Turbomachinery:;2014:;volume( 136 ):;issue: 002 | |
| contenttype | Fulltext | |