| contributor author | J. H. Griffin | |
| date accessioned | 2017-05-08T23:27:10Z | |
| date available | 2017-05-08T23:27:10Z | |
| date copyright | January, 1988 | |
| date issued | 1988 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26651#45_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/103915 | |
| description abstract | The vibratory responses of blades in gas turbine engines vary because of mistuning. An approach is developed for calculating the statistical distribution of peak resonant stresses in engine blading. It is used to predict the vibratory response of an un-shrouded fan stage. The results of the calculation compare favorably with test data for the lower frequency modes. The procedure can be used to predict fleet durability and offers a practical engineering approach for dealing with stage mistuning. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | On Predicting the Resonant Response of Bladed Disk Assemblies | |
| type | Journal Paper | |
| journal volume | 110 | |
| journal issue | 1 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3240085 | |
| journal fristpage | 45 | |
| journal lastpage | 50 | |
| identifier eissn | 0742-4795 | |
| keywords | Engines | |
| keywords | Stress | |
| keywords | Durability | |
| keywords | Gas turbines | |
| keywords | Disks | |
| keywords | Blades AND Statistical distributions | |
| tree | Journal of Engineering for Gas Turbines and Power:;1988:;volume( 110 ):;issue: 001 | |
| contenttype | Fulltext | |
