| contributor author | Richard A. Layton | |
| contributor author | John J. Marra | |
| date accessioned | 2017-05-09T00:02:26Z | |
| date available | 2017-05-09T00:02:26Z | |
| date copyright | April, 2000 | |
| date issued | 2000 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26795#321_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/123697 | |
| description abstract | A central issue in gas turbine engine design today is the demand for higher performance, greater reliability, shorter lead times, and lower cost. The design of bladed disks (fans, compressors and turbines) is one area in which suitable design tools are sought to meet this demand. In this paper is presented the conceptual basis for a new, energy-based approach to design and an outline for future development of the approach as a software-based design tool. Technical tasks and risks associated with this development are summarized. It is hoped that this study will facilitate dialogue among practitioners of the various disciplines involved in bladed-disk design. [S0742-4795(00)00302-1] | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Conceptual Basis for a New Approach to Bladed-Disk Design | |
| type | Journal Paper | |
| journal volume | 122 | |
| journal issue | 2 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.483210 | |
| journal fristpage | 321 | |
| journal lastpage | 325 | |
| identifier eissn | 0742-4795 | |
| keywords | Design AND Disks | |
| tree | Journal of Engineering for Gas Turbines and Power:;2000:;volume( 122 ):;issue: 002 | |
| contenttype | Fulltext | |
