| contributor author | R. B. Ginder | |
| contributor author | W. J. Calvert | |
| date accessioned | 2017-05-08T23:26:00Z | |
| date available | 2017-05-08T23:26:00Z | |
| date copyright | July, 1987 | |
| date issued | 1987 | |
| identifier issn | 0889-504X | |
| identifier other | JOTUEI-28585#340_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/103210 | |
| description abstract | A recent ASME paper by the authors described a quasi-three-dimensional calculation system for transonic compressor blade rows. The system predicts both the internal flow field and the overall performance of the blade row. It therefore enables the compressor engineer to optimize the blade shapes in order to improve the design point efficiency. This is explored in the present paper. A new type of blade profile has been developed to allow sufficient freedom for the optimization. Application to the design of a high-efficiency, transonic civil fan rotor is discussed. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | The Design of an Advanced Civil Fan Rotor | |
| type | Journal Paper | |
| journal volume | 109 | |
| journal issue | 3 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.3262111 | |
| journal fristpage | 340 | |
| journal lastpage | 345 | |
| identifier eissn | 1528-8900 | |
| keywords | Design | |
| keywords | Rotors | |
| keywords | Blades | |
| keywords | Compressors | |
| keywords | Internal flow | |
| keywords | Optimization | |
| keywords | Shapes AND Engineers | |
| tree | Journal of Turbomachinery:;1987:;volume( 109 ):;issue: 003 | |
| contenttype | Fulltext | |
