| contributor author | W. C. Swan | |
| date accessioned | 2017-05-08T23:19:41Z | |
| date available | 2017-05-08T23:19:41Z | |
| date copyright | July, 1964 | |
| date issued | 1964 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26635#243_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/99513 | |
| description abstract | An experiment in unstalled range of a transonic axial flow compressor stage is discussed. Two rotors of identical design, but of differing aspect ratio, are compared. The study suggests that some criteria other than blade chord Reynolds number be used to define chord lengths of transonic stages. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | An Experiment With Aspect Ratio as a Means of Extending the Useful Range of a Transonic Inlet Stage of an Axial Flow Compressor | |
| type | Journal Paper | |
| journal volume | 86 | |
| journal issue | 3 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3677586 | |
| journal fristpage | 243 | |
| journal lastpage | 246 | |
| identifier eissn | 0742-4795 | |
| keywords | Axial flow | |
| keywords | Chords (Trusses) | |
| keywords | Design | |
| keywords | Rotors | |
| keywords | Blades AND Reynolds number | |
| tree | Journal of Engineering for Gas Turbines and Power:;1964:;volume( 086 ):;issue: 003 | |
| contenttype | Fulltext | |
