Aspects of Gas Turbine Thermal Efficiency
| contributor author | Langston, Lee S. | |
| date accessioned | 2022-02-04T22:15:07Z | |
| date available | 2022-02-04T22:15:07Z | |
| date copyright | 9/1/2020 12:00:00 AM | |
| date issued | 2020 | |
| identifier issn | 0025-6501 | |
| identifier other | me-2020-sep4.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4275189 | |
| description abstract | In the family of heat engines, the gas turbine is unique in that it is used to produce two different kinds of useful power. By converting combusted fuel heat into work, a gas turbine engine can produce external shaft power (e.g., to drive a connected electric generator) or jet power (e.g., as a jet engine, to produce thrust forces to propel an aircraft). This means that the gas turbine’s thermodynamic figure of merit, thermal efficiency, is multifaceted, and calls for a nuanced examination. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Aspects of Gas Turbine Thermal Efficiency | |
| type | Journal Paper | |
| journal volume | 142 | |
| journal issue | 9 | |
| journal title | Mechanical Engineering | |
| identifier doi | 10.1115/1.2020-SEP4 | |
| journal fristpage | 54 | |
| journal lastpage | 55 | |
| page | 2 | |
| tree | Mechanical Engineering:;2020:;volume( 142 ):;issue: 009 | |
| contenttype | Fulltext |
