| contributor author | S. H. Moustapha | |
| contributor author | U. Okapuu | |
| contributor author | R. G. Williamson | |
| date accessioned | 2017-05-08T23:26:03Z | |
| date available | 2017-05-08T23:26:03Z | |
| date copyright | April, 1987 | |
| date issued | 1987 | |
| identifier issn | 0889-504X | |
| identifier other | JOTUEI-28583#155_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/103233 | |
| description abstract | This paper describes the performance of a highly loaded single-stage transonic turbine with a pressure ratio of 3.76 and a stage loading factor of 2.47. Tests were carried out with three rotors, covering a range of blade Zweifel coefficient of 0.77 to 1.18. Detailed traversing at rotor inlet and exit allowed an assessment of rotor and stage performance as a function of blade loading under realistic operating conditions. The effect of stator endwall contouring on overall stage performance was also investigated using two different contours with the same vane design. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Influence of Rotor Blade Aerodynamic Loading on the Performance of a Highly Loaded Turbine Stage | |
| type | Journal Paper | |
| journal volume | 109 | |
| journal issue | 2 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.3262078 | |
| journal fristpage | 155 | |
| journal lastpage | 161 | |
| identifier eissn | 1528-8900 | |
| tree | Journal of Turbomachinery:;1987:;volume( 109 ):;issue: 002 | |
| contenttype | Fulltext | |
