| contributor author | G. R. Leverant | |
| contributor author | H. R. Millwater | |
| contributor author | R. C. McClung | |
| contributor author | M. P. Enright | |
| date accessioned | 2017-05-09T00:13:05Z | |
| date available | 2017-05-09T00:13:05Z | |
| date copyright | January, 2004 | |
| date issued | 2004 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26825#155_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/130079 | |
| description abstract | This paper summarizes recent enhancements to a probabilistic damage tolerance software code, DARWINTM, that can be used for design certification of aircraft jet engine titanium disks/rotors that may contain melt-related anomalies. Evaluations of DARWINTM by engine manufacturers are also discussed, including comparisons with existing codes for accuracy and time efficiency. In addition, relevant test results, including various fatigue tests on material containing melt-related anomalies, are summarized. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | A New Tool for Design and Certification of Aircraft Turbine Rotors | |
| type | Journal Paper | |
| journal volume | 126 | |
| journal issue | 1 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.1622409 | |
| journal fristpage | 155 | |
| journal lastpage | 159 | |
| identifier eissn | 0742-4795 | |
| keywords | Design | |
| keywords | Rotors | |
| keywords | Disks | |
| keywords | Aircraft | |
| keywords | Titanium | |
| keywords | Engines | |
| keywords | Turbines | |
| keywords | Stress | |
| keywords | Product quality AND Fracture (Materials) | |
| tree | Journal of Engineering for Gas Turbines and Power:;2004:;volume( 126 ):;issue: 001 | |
| contenttype | Fulltext | |
