| contributor author | R. A. Miller | |
| date accessioned | 2017-05-08T23:30:01Z | |
| date available | 2017-05-08T23:30:01Z | |
| date copyright | April, 1989 | |
| date issued | 1989 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26665#301_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/105409 | |
| description abstract | Thermal barrier coating life models developed under the NASA Lewis Research Center’s Hot Section Technology (HOST) program are summarized. An initial laboratory model and three design-capable models are discussed. Current understanding of coating failure mechanisms is also summarized. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Life Modeling of Thermal Barrier Coatings for Aircraft Gas Turbine Engines | |
| type | Journal Paper | |
| journal volume | 111 | |
| journal issue | 2 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3240251 | |
| journal fristpage | 301 | |
| journal lastpage | 305 | |
| identifier eissn | 0742-4795 | |
| keywords | Gas turbines | |
| keywords | Modeling | |
| keywords | Aircraft | |
| keywords | Thermal barrier coatings | |
| keywords | Coating processes | |
| keywords | Coatings | |
| keywords | Design AND Failure mechanisms | |
| tree | Journal of Engineering for Gas Turbines and Power:;1989:;volume( 111 ):;issue: 002 | |
| contenttype | Fulltext | |
