| contributor author | Jardine, Lachlan J. | |
| contributor author | Miller, Robert J. | |
| date accessioned | 2022-02-04T22:15:09Z | |
| date available | 2022-02-04T22:15:09Z | |
| date copyright | 9/1/2020 12:00:00 AM | |
| date issued | 2020 | |
| identifier issn | 0025-6501 | |
| identifier other | me-2020-sep5.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4275190 | |
| description abstract | For over 50 years, high-pressure gas turbine blades have been cooled using air bled from the compressor. This cooling results in very high rates of heat transfer, both within the fluid and within the blade, shown in figure 1. The heat transfer often occurs across large temperature differences and is thus highly irreversible. It is therefore surprising that little is understood about the effect of this heat transfer on turbine performance. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | The Effect of Heat Transfer on Turbine Performance | |
| type | Journal Paper | |
| journal volume | 142 | |
| journal issue | 9 | |
| journal title | Mechanical Engineering | |
| identifier doi | 10.1115/1.2020-SEP5 | |
| journal fristpage | 56 | |
| journal lastpage | 57 | |
| page | 2 | |
| tree | Mechanical Engineering:;2020:;volume( 142 ):;issue: 009 | |
| contenttype | Fulltext | |
