| contributor author | O. E. Baljé | |
| date accessioned | 2017-05-09T00:35:57Z | |
| date available | 2017-05-09T00:35:57Z | |
| date copyright | July, 1970 | |
| date issued | 1970 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26687#287_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/142244 | |
| description abstract | The flow conditions in a mixed flow rotor are investigated for a “pressure balanced” flow path design. Boundary layer arguments are applied to calculate the losses in the rotor as well as in the subsequent diffuser section. The resulting efficiency data imply a comparatively high efficiency potential for mixed flow compressors with multiple cascaded components, designed on the premise of a “pressure balanced” rotor flow path. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Loss and Flow Path Studies on Centrifugal Compressors—Part II | |
| type | Journal Paper | |
| journal volume | 92 | |
| journal issue | 3 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3445353 | |
| journal fristpage | 287 | |
| journal lastpage | 300 | |
| identifier eissn | 0742-4795 | |
| keywords | Flow (Dynamics) | |
| keywords | Compressors | |
| keywords | Rotors | |
| keywords | Pressure | |
| keywords | Diffusers | |
| keywords | Boundary layers AND Design | |
| tree | Journal of Engineering for Gas Turbines and Power:;1970:;volume( 092 ):;issue: 003 | |
| contenttype | Fulltext | |
