| contributor author | H. Pfeil | |
| contributor author | M. Göing | |
| date accessioned | 2017-05-08T23:26:01Z | |
| date available | 2017-05-08T23:26:01Z | |
| date copyright | July, 1987 | |
| date issued | 1987 | |
| identifier issn | 0889-504X | |
| identifier other | JOTUEI-28585#405_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/103219 | |
| description abstract | This paper presents boundary layer measurements in a diffuser behind a one-stage axial compressor for the case of nearly axial outlet flow direction from the blades. According to the results, three-dimensional effects caused by the compressor blading have a great influence on the character and development of the turbulent boundary layer and must be included in methods to predict the diffuser flow. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Measurements of the Turbulent Boundary Layer in the Diffuser Behind an Axial Compressor | |
| type | Journal Paper | |
| journal volume | 109 | |
| journal issue | 3 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.3262120 | |
| journal fristpage | 405 | |
| journal lastpage | 412 | |
| identifier eissn | 1528-8900 | |
| keywords | Measurement | |
| keywords | Compressors | |
| keywords | Diffusers | |
| keywords | Boundary layer turbulence | |
| keywords | Flow (Dynamics) | |
| keywords | Boundary layers AND Blades | |
| tree | Journal of Turbomachinery:;1987:;volume( 109 ):;issue: 003 | |
| contenttype | Fulltext | |