| contributor author | B. Lakshminarayana | |
| contributor author | N. Sitaram | |
| contributor author | J. Zhang | |
| 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#22_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/101154 | |
| description abstract | The blade-to-blade variation of relative stagnation pressure losses in the tip region inside the rotor of a single-stage, axial-flow compressor is presented and interpreted in this paper. The losses are measured at two flow coefficients (one at the design point and the other at the near peak pressure rise point) to discern the effect of blade loading on the end-wall losses. The tip clearance losses are found to increase with an increase in the pressure rise coefficient. The losses away from the tip region and near the hub regions are measured downstream. The losses are integrated and interpreted in this paper. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | End-Wall and Profile Losses in a Low-Speed Axial Flow Compressor Rotor | |
| type | Journal Paper | |
| journal volume | 108 | |
| journal issue | 1 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3239880 | |
| journal fristpage | 22 | |
| journal lastpage | 31 | |
| identifier eissn | 0742-4795 | |
| keywords | Rotors | |
| keywords | Axial flow | |
| keywords | Blades | |
| keywords | Pressure | |
| keywords | Flow (Dynamics) | |
| keywords | Compressors | |
| keywords | Clearances (Engineering) AND Design | |
| tree | Journal of Engineering for Gas Turbines and Power:;1986:;volume( 108 ):;issue: 001 | |
| contenttype | Fulltext | |
