| contributor author | Y. Kashiwabara | |
| contributor author | K. Tokunaga | |
| contributor author | Y. Matsuura | |
| contributor author | Y. Katoh | |
| contributor author | N. Hagiwara | |
| contributor author | T. Hattori | |
| 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#233_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/101832 | |
| description abstract | In this paper, the development of a model 17-stage axial compressor (pressure ratio 14.7) for a medium-size gas turbine is described. The aerodynamic and mechanical design features of the compressor are presented. In advance of the full 17-stage test, the first three and nine stages were tested. Measured results confirm the design performance in the first stages of the 17-stage compressor. The details of the construction of the facilities, instrumentation and data acquisition system for the full 17-stage test are described. Test results for the 17-stage compressor are presented. The measured results are in good agreement with the predicted values. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Development of a High-Pressure-Ratio Axial Flow Compressor for a Medium-Size Gas Turbine | |
| type | Journal Paper | |
| journal volume | 108 | |
| journal issue | 2 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.3262042 | |
| journal fristpage | 233 | |
| journal lastpage | 239 | |
| identifier eissn | 1528-8900 | |
| tree | Journal of Turbomachinery:;1986:;volume( 108 ):;issue: 002 | |
| contenttype | Fulltext | |