| contributor author | R. V. Chima | |
| contributor author | A. J. Strazisar | |
| date accessioned | 2017-05-08T23:15:28Z | |
| date available | 2017-05-08T23:15:28Z | |
| date copyright | July, 1983 | |
| date issued | 1983 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26783#596_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/97073 | |
| description abstract | Two-and three-dimensional inviscid solutions for the flow within a transonic axial compressor rotor at design speed are compared to laser anemometer measurements at maximum flow and near stall operating points. Computational details of the two-dimensional axisymmetric stream function solution and the three-dimensional full Euler solution are described. Upstream of the rotor, the two and three-dimensional solutions for radial distribution of relative Mach number and total pressure agree well with the data. Within the bow wave system and the blade row, the axisymmetric two-dimensional solution shows only qualitative agreement with the data. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Comparison of Two- and Three-Dimensional Flow Computations With Laser Anemometer Measurements in a Transonic Compressor Rotor | |
| type | Journal Paper | |
| journal volume | 105 | |
| journal issue | 3 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3227459 | |
| journal fristpage | 596 | |
| journal lastpage | 605 | |
| identifier eissn | 0742-4795 | |
| keywords | Lasers | |
| keywords | Measurement | |
| keywords | Compressors | |
| keywords | Flow (Dynamics) | |
| keywords | Rotors | |
| keywords | Computation | |
| keywords | Pressure | |
| keywords | Blades | |
| keywords | Mach number | |
| keywords | Waves AND Design | |
| tree | Journal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 003 | |
| contenttype | Fulltext | |
