| contributor author | Hong Qilin | |
| contributor author | Zheng Qixuan | |
| contributor author | Wang Ping | |
| contributor author | Hou Guicang | |
| date accessioned | 2017-05-08T23:38:27Z | |
| date available | 2017-05-08T23:38:27Z | |
| date copyright | April, 1992 | |
| date issued | 1992 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26699#334_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/110247 | |
| description abstract | An approximate analytical large deformation method, based on the Nadai deformation theory, for calculating the burst speed of aeroengine disks, is presented in this paper. The basic equations are developed and the calculation procedures are illustrated. The burst speeds are calculated for some tested disks, and the calculation results are compared with the test results; the differences between two results are shown to be less than 8 percent. This shows that the new method is both simple and convenient. Therefore, it could be employed in the development of aeroengine disks. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | A New Method for Calculating Burst Speed of Aeroengine Disks | |
| type | Journal Paper | |
| journal volume | 114 | |
| journal issue | 2 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.2906593 | |
| journal fristpage | 334 | |
| journal lastpage | 337 | |
| identifier eissn | 0742-4795 | |
| keywords | Disks | |
| keywords | Deformation AND Equations | |
| tree | Journal of Engineering for Gas Turbines and Power:;1992:;volume( 114 ):;issue: 002 | |
| contenttype | Fulltext | |
