| contributor author | W. Steinert | |
| contributor author | R. Fuchs | |
| contributor author | H. Starken | |
| date accessioned | 2017-05-08T23:39:51Z | |
| date available | 2017-05-08T23:39:51Z | |
| date copyright | July, 1992 | |
| date issued | 1992 | |
| identifier issn | 0889-504X | |
| identifier other | JOTUEI-28622#487_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/111060 | |
| description abstract | Tests of transonic compressor cascades require special measuring techniques to determine the inlet flow angle around sonic inlet flow conditions. One of the main requirements for these methods is the ability to adjust the inlet flow angle during the test to a prescribed value. A method has been successfully applied that relies on theoretically determined suction surface velocities. The described method was applied in testing cascades at inlet Mack numbers between M1 = 0.75−1.18. The test results confirmed the practicability of this method. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Inlet Flow Angle Determination of Transonic Compressor Cascades | |
| type | Journal Paper | |
| journal volume | 114 | |
| journal issue | 3 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.2929169 | |
| journal fristpage | 487 | |
| journal lastpage | 493 | |
| identifier eissn | 1528-8900 | |
| keywords | Flow (Dynamics) | |
| keywords | Compressors | |
| keywords | Testing AND Suction | |
| tree | Journal of Turbomachinery:;1992:;volume( 114 ):;issue: 003 | |
| contenttype | Fulltext | |