| contributor author | J. P. Ayers | |
| contributor author | D. M. Feiner | |
| contributor author | J. H. Griffin | |
| date accessioned | 2017-05-09T00:21:56Z | |
| date available | 2017-05-09T00:21:56Z | |
| date copyright | July, 2006 | |
| date issued | 2006 | |
| identifier issn | 0889-504X | |
| identifier other | JOTUEI-28730#466_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/134821 | |
| description abstract | A method for predicting the vibratory response of bladed disks under high engine acceleration rates is developed. The method is based on the Fundamental Mistuning Model, an existing reduced order model for predicting the steady-state vibratory response. In addition, a criterion is developed for a critical engine acceleration rate, above which transient effects play a large role in the response. It is shown that military engines operate at acceleration rates above this critical value and therefore transient effects are important in practice. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | A Reduced-Order Model for Transient Analysis of Bladed Disk Forced Response | |
| type | Journal Paper | |
| journal volume | 128 | |
| journal issue | 3 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.2185675 | |
| journal fristpage | 466 | |
| journal lastpage | 473 | |
| identifier eissn | 1528-8900 | |
| keywords | Engines | |
| keywords | Disks | |
| keywords | Blades | |
| keywords | Steady state | |
| keywords | Frequency | |
| keywords | Transient analysis AND Transients (Dynamics) | |
| tree | Journal of Turbomachinery:;2006:;volume( 128 ):;issue: 003 | |
| contenttype | Fulltext | |