| contributor author | J. H. Horlock | |
| date accessioned | 2017-05-08T23:34:09Z | |
| date available | 2017-05-08T23:34:09Z | |
| date copyright | April, 1990 | |
| date issued | 1990 | |
| identifier issn | 0889-504X | |
| identifier other | JOTUEI-28601#294_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/107770 | |
| description abstract | An actuator disk analysis is given of the flow through a guide vane and rotor combination. It is shown that changes in total pressure across the rotor are in general related to circumferential variations in guide vane outlet angle. In particular known variations in inlet total pressure may be eliminated by suitable circumferential changes in guide vane stagger. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | The Use of Circumferentially Varying Stagger Guide Vanes in an Axial Flow Pump or Compressor | |
| type | Journal Paper | |
| journal volume | 112 | |
| journal issue | 2 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.2927652 | |
| journal fristpage | 294 | |
| journal lastpage | 297 | |
| identifier eissn | 1528-8900 | |
| keywords | Pressure | |
| keywords | Flow (Dynamics) | |
| keywords | Compressors | |
| keywords | Actuators | |
| keywords | Pumps | |
| keywords | Rotors | |
| keywords | Disks AND Axial flow | |
| tree | Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 002 | |
| contenttype | Fulltext | |
