| contributor author | G. H. Henderson | |
| contributor author | S. Fleeter | |
| date accessioned | 2017-05-08T23:55:05Z | |
| date available | 2017-05-08T23:55:05Z | |
| date copyright | July, 1997 | |
| date issued | 1997 | |
| identifier issn | 0889-504X | |
| identifier other | JOTUEI-28661#482_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/119595 | |
| description abstract | The effects of high steady loading and separated flow on the unsteady aerodynamic response of turbomachine blade rows are experimentally investigated. This is accomplished utilizing a unique single-stage turbomachine research facility in which the flow is not generated by the blading but rather by an additional fan. Thus, for a particular stator incidence angle, the steady or mean stator aerodynamic performance were determined in a completely steady flow with no rotor and also with unsteady flow generated by a rotor composed of perforated plates at the same mean operating condition, thereby identifying the stator vane row dynamic stall conditions. The unsteady aerodynamic response of the very low-solidity stator vane row is then investigated over a range of incidence angle values, including attached and separated flows with dynamic stall. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Vortical Gust Response of a Low-Solidity Vane Row Including Steady Loading and Dynamic Stall Effects | |
| type | Journal Paper | |
| journal volume | 119 | |
| journal issue | 3 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.2841147 | |
| journal fristpage | 482 | |
| journal lastpage | 490 | |
| identifier eissn | 1528-8900 | |
| keywords | Flow (Dynamics) | |
| keywords | Plates (structures) | |
| keywords | Rotors | |
| keywords | Blades | |
| keywords | Stators | |
| keywords | Turbomachinery AND Unsteady flow | |
| tree | Journal of Turbomachinery:;1997:;volume( 119 ):;issue: 003 | |
| contenttype | Fulltext | |
