| contributor author | R. L. Evans | |
| date accessioned | 2017-05-08T22:58:38Z | |
| date available | 2017-05-08T22:58:38Z | |
| date copyright | January, 1975 | |
| date issued | 1975 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26714#131_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/87484 | |
| description abstract | Turbulence and unsteadiness levels downstream of an axial-flow compressor rotor have been measured using an ensemble-averaging technique. Free-stream turbulence levels are lowest near the compressor design-point, and increase with decreasing flow coefficient as the compressor nears the stalled condition. The unsteady stator incidence angles have been found to have a peak-to-peak variation of between 12 deg and 15 deg for all flow coefficients tested. These observations have been confirmed qualitatively by hot-wire-anemometer spectral measurements. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Turbulence and Unsteadiness Measurements Downstream of a Moving Blade Row | |
| type | Journal Paper | |
| journal volume | 97 | |
| journal issue | 1 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3445892 | |
| journal fristpage | 131 | |
| journal lastpage | 137 | |
| identifier eissn | 0742-4795 | |
| keywords | Measurement | |
| keywords | Turbulence | |
| keywords | Blades | |
| keywords | Compressors | |
| keywords | Flow (Dynamics) | |
| keywords | Stators | |
| keywords | Wire | |
| keywords | Design | |
| keywords | Rotors AND Axial flow | |
| tree | Journal of Engineering for Gas Turbines and Power:;1975:;volume( 097 ):;issue: 001 | |
| contenttype | Fulltext | |
