| contributor author | J. A. Kenyon | |
| contributor author | J. H. Griffin | |
| contributor author | D. M. Feiner | |
| date accessioned | 2017-05-09T00:11:43Z | |
| date available | 2017-05-09T00:11:43Z | |
| date copyright | April, 2003 | |
| date issued | 2003 | |
| identifier issn | 0889-504X | |
| identifier other | JOTUEI-28702#352_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/129277 | |
| description abstract | A method is presented for obtaining maximum bladed disk forced response from distortion of a structural mode. It is shown that maximum response from mode distortion in a bladed disk occurs when the harmonic components of a distorted mode superimpose in a certain manner, causing localization of the mode and strong response in a particular blade. In addition, it is shown that the response of an intentionally mistuned system with maximum response does not change significantly when small random mistuning is added to the system. A method is described for calculating the structural mistuning necessary to obtain the distorted mode that gives maximum response. The theory is validated numerically. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Maximum Bladed Disk Forced Response From Distortion of a Structural Mode | |
| type | Journal Paper | |
| journal volume | 125 | |
| journal issue | 2 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.1540118 | |
| journal fristpage | 352 | |
| journal lastpage | 363 | |
| identifier eissn | 1528-8900 | |
| keywords | Damping | |
| keywords | Disks | |
| keywords | Blades AND Frequency | |
| tree | Journal of Turbomachinery:;2003:;volume( 125 ):;issue: 002 | |
| contenttype | Fulltext | |