| contributor author | D. L. Tweedt | |
| contributor author | M. D. Hathaway | |
| contributor author | T. H. Okiishi | |
| date accessioned | 2017-05-08T23:23:40Z | |
| date available | 2017-05-08T23:23:40Z | |
| date copyright | October, 1986 | |
| date issued | 1986 | |
| identifier issn | 0889-504X | |
| identifier other | JOTUEI-28578#224_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/101831 | |
| description abstract | The use of stator endwall leading-edge sweep to improve axial-flow compressor stator row performance was examined experimentally. The aerodynamics of three stator hub (inner diameter) conditions, namely, a running clearance, a stationary clearance, and a shroud, were also investigated. Leading-edge sweep in the endwall regions of a stator blade can be beneficial in terms of loss reduction on the casing (outer diameter) end of a stator blade. It can also help at the hub end of a stator blade when either a stationary hub clearance or a hub shroud is used. A leading-edge sweep is detrimental (local loss increase) on the hub end of a stator blade when a running hub clearance is used. A running clearance is aerodynamically preferable to a stationary clearance. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Stator Endwall Leading-Edge Sweep and Hub Shroud Influence on Compressor Performance | |
| type | Journal Paper | |
| journal volume | 108 | |
| journal issue | 2 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.3262041 | |
| journal fristpage | 224 | |
| journal lastpage | 232 | |
| identifier eissn | 1528-8900 | |
| tree | Journal of Turbomachinery:;1986:;volume( 108 ):;issue: 002 | |
| contenttype | Fulltext | |
