| contributor author | R. L. McKnight | |
| date accessioned | 2017-05-08T23:30:00Z | |
| date available | 2017-05-08T23:30:00Z | |
| date copyright | April, 1989 | |
| date issued | 1989 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26665#271_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/105406 | |
| description abstract | The programs in the structural analysis area of the HOST program emphasized the generation of computer codes for performing three-dimensional inelastic analysis with more accuracy and less manpower. This paper presents the application of that technology to Aircraft Gas Turbine Engine (AGTE) components: combustors, turbine blades, and vanes. Previous limitations will be reviewed and the breakthrough technology highlighted. The synergism and spillover of the program will be demonstrated by reviewing applications to thermal barrier coatings analysis and the SSME HPFTP turbine blade. These applications show that this technology has increased the ability of the AGTE designer to be more innovative, productive, and accurate. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Structural Analysis Applications | |
| type | Journal Paper | |
| journal volume | 111 | |
| journal issue | 2 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3240248 | |
| journal fristpage | 271 | |
| journal lastpage | 278 | |
| identifier eissn | 0742-4795 | |
| keywords | Structural analysis | |
| keywords | Turbine blades | |
| keywords | Combustion chambers | |
| keywords | Gas turbines | |
| keywords | Inelastic analysis | |
| keywords | Computers | |
| keywords | Aircraft AND Thermal barrier coatings | |
| tree | Journal of Engineering for Gas Turbines and Power:;1989:;volume( 111 ):;issue: 002 | |
| contenttype | Fulltext | |
