| contributor author | C. Hah | |
| date accessioned | 2017-05-08T23:22:30Z | |
| date available | 2017-05-08T23:22:30Z | |
| date copyright | January, 1986 | |
| date issued | 1986 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26630#15_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/101153 | |
| description abstract | The current study is aimed at developing and appraising a numerical method for the development of endwall boundary layers through tip-clearances and their effect on the performance of an isolated compressor rotor. The Reynolds-averaged Navier-Stokes equation is solved for the entire flow field in elliptic form. The relative flow is computed on the generalized coordinates fixed on the rotor. Comparison between the numerical results and experimental data indicates that the complex three-dimensional viscous flow phenomena inside the tip region are properly predicted. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | A Numerical Modeling of Endwall and Tip-Clearance Flow of an Isolated Compressor Rotor | |
| type | Journal Paper | |
| journal volume | 108 | |
| journal issue | 1 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3239863 | |
| journal fristpage | 15 | |
| journal lastpage | 21 | |
| identifier eissn | 0742-4795 | |
| keywords | Flow (Dynamics) | |
| keywords | Computer simulation | |
| keywords | Compressors | |
| keywords | Clearances (Engineering) | |
| keywords | Rotors | |
| keywords | Navier-Stokes equations | |
| keywords | Boundary layers | |
| keywords | Numerical analysis AND Viscous flow | |
| tree | Journal of Engineering for Gas Turbines and Power:;1986:;volume( 108 ):;issue: 001 | |
| contenttype | Fulltext | |
