| contributor author | B. S. Seidel | |
| contributor author | J. J. Adamczyk | |
| contributor author | M. D. Matwey | |
| date accessioned | 2017-05-08T23:08:33Z | |
| date available | 2017-05-08T23:08:33Z | |
| date copyright | October, 1980 | |
| date issued | 1980 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26762#924_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/93195 | |
| description abstract | A single stage axial compressor with distorted inflow is studied. The inflow distortion occurs far upstream and may be a distortion in stagnation temperature, stagnation pressure or both. The blade rows are modelled as semi-actuator disks. Losses, quasi-steady deviation angles, and reference incidence correlations are included in the analysis. Both subsonic and transonic relative Mach Numbers are considered. A parameter study is made to determine the influence of such variables as Mach Number and swirl angle on the attenuation of the distortion. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Inlet Flow Distortion in Turbomachinery | |
| type | Journal Paper | |
| journal volume | 102 | |
| journal issue | 4 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3230362 | |
| journal fristpage | 924 | |
| journal lastpage | 929 | |
| identifier eissn | 0742-4795 | |
| keywords | Pressure | |
| keywords | Flow (Dynamics) | |
| keywords | Mach number | |
| keywords | Temperature | |
| keywords | Compressors | |
| keywords | Actuators | |
| keywords | Disks | |
| keywords | Blades | |
| keywords | Turbomachinery AND Inflow | |
| tree | Journal of Engineering for Gas Turbines and Power:;1980:;volume( 102 ):;issue: 004 | |
| contenttype | Fulltext | |