| contributor author | J. H. Griffin | |
| date accessioned | 2017-05-08T23:08:42Z | |
| date available | 2017-05-08T23:08:42Z | |
| date copyright | April, 1980 | |
| date issued | 1980 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26757#329_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/93273 | |
| description abstract | The resonant response of a turbine airfoil attenuated through use of a Coulomb damper is analyzed. Parameters that control the damper’s effectiveness are identified and characteristics of an optimized system are described. The results of the analysis are confirmed by laboratory tests. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Friction Damping of Resonant Stresses in Gas Turbine Engine Airfoils | |
| type | Journal Paper | |
| journal volume | 102 | |
| journal issue | 2 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3230256 | |
| journal fristpage | 329 | |
| journal lastpage | 333 | |
| identifier eissn | 0742-4795 | |
| keywords | Friction | |
| keywords | Stress | |
| keywords | Damping | |
| keywords | Gas turbines | |
| keywords | Airfoils | |
| keywords | Turbines | |
| keywords | Dampers AND Coulombs | |
| tree | Journal of Engineering for Gas Turbines and Power:;1980:;volume( 102 ):;issue: 002 | |
| contenttype | Fulltext | |
