| contributor author | N. A. Cumpsty | |
| contributor author | Y. Dong | |
| date accessioned | 2017-05-08T23:34:07Z | |
| date available | 2017-05-08T23:34:07Z | |
| date copyright | April, 1990 | |
| date issued | 1990 | |
| identifier issn | 0889-504X | |
| identifier other | JOTUEI-28601#255_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/107750 | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Discussion: “The Measurement of Boundary Layers on a Compressor Blade in Cascade: Part 4—Flow Fields for Incidence Angles of −1.5 and −8.5 Degrees” (Zierke, W. C., and Deutsch, S., 1990, ASME J. Turbomach., 112, pp. 241–255) | |
| type | Journal Paper | |
| journal volume | 112 | |
| journal issue | 2 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.2927639 | |
| journal fristpage | 255 | |
| identifier eissn | 1528-8900 | |
| keywords | Flow (Dynamics) | |
| keywords | Compressors | |
| keywords | Cascades (Fluid dynamics) | |
| keywords | Boundary layers AND Blades | |
| tree | Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 002 | |
| contenttype | Fulltext | |