| contributor author | R. G. Williamson | |
| contributor author | S. H. Moustapha | |
| date accessioned | 2017-05-08T23:22:45Z | |
| date available | 2017-05-08T23:22:45Z | |
| date copyright | September, 1986 | |
| date issued | 1986 | |
| identifier issn | 0098-2202 | |
| identifier other | JFEGA4-27022#313_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/101291 | |
| description abstract | This paper presents detailed information on the three-dimensional flow field in a realistic low aspect ratio, high turning nozzle vane design which incorporates end-wall contouring and which has been tested over a range of exit Mach number from subsonic up to the design value at mean section of 1.15. The experimental results, in the form of nozzle surface pressure distributions as well as surveys of pressure losses and flow angles at exit, are compared with those calculated by a three-dimensional flow analysis. The effects of exit Mach number on the measured nozzle performance are also presented. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Annular Cascade Testing of Turbine Nozzles at High Exit Mach Numbers | |
| type | Journal Paper | |
| journal volume | 108 | |
| journal issue | 3 | |
| journal title | Journal of Fluids Engineering | |
| identifier doi | 10.1115/1.3242579 | |
| journal fristpage | 313 | |
| journal lastpage | 320 | |
| identifier eissn | 1528-901X | |
| keywords | Mach number | |
| keywords | Cascades (Fluid dynamics) | |
| keywords | Nozzles | |
| keywords | Testing | |
| keywords | Turbines | |
| keywords | Flow (Dynamics) | |
| keywords | Pressure AND Design | |
| tree | Journal of Fluids Engineering:;1986:;volume( 108 ):;issue: 003 | |
| contenttype | Fulltext | |