| contributor author | E. K. Armstrong | |
| date accessioned | 2017-05-08T23:53:05Z | |
| date available | 2017-05-08T23:53:05Z | |
| date copyright | July, 1967 | |
| date issued | 1967 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26661#437_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/118478 | |
| description abstract | The methods which have been used recently to predict the amplitudes of vibration of compressor blades are explained. Examples for resonances with maldistributions in the intake flow and downstream blockages are given. Two techniques of obtaining blade vibration data from the HP shaft of a two-shaft jet engine are described. By comparing the measured amplitudes with the fatigue properties of blading, a parameter has been established which is used in assessing the seriousness of a vibration when considering its service life. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Recent Blade Vibration Techniques | |
| type | Journal Paper | |
| journal volume | 89 | |
| journal issue | 3 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3616710 | |
| journal fristpage | 437 | |
| journal lastpage | 444 | |
| identifier eissn | 0742-4795 | |
| keywords | Vibration | |
| keywords | Blades | |
| keywords | Jet engines | |
| keywords | Fatigue properties | |
| keywords | Flow (Dynamics) | |
| keywords | Compressors AND Service life (Equipment) | |
| tree | Journal of Engineering for Gas Turbines and Power:;1967:;volume( 089 ):;issue: 003 | |
| contenttype | Fulltext | |
