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handle: 11421/18517 , 11454/41651
This study deals with an exergoeconomic analysis of an aircraft turbofan engine utilising the kerosene as fuel. A new parameter is developed to define the thrust cost rate. The cost of exergy destruction, the relative cost difference and the exergoeconomic factor are investigated. The variation of the relative cost difference and exergoeconomic factor according to the operating and maintenance costs and the annual operating hour are also studied. For a high by-pass and high thrust rated engine, the cost rate of thrust is obtained to be 304.35 $(hkN) −1 for the hot thrust and 138.96 $ (hkN)−1 for the cold thrust, respectively.
exergy, efficiency, aircraft turbofan engine, exergoeconomic analysis, Efficiency, Exergy, Aircraft Turbofan Engine, Exergoeconomic Analysis
exergy, efficiency, aircraft turbofan engine, exergoeconomic analysis, Efficiency, Exergy, Aircraft Turbofan Engine, Exergoeconomic Analysis
citations This is an alternative to the "Influence" indicator, which also reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically). | 40 | |
popularity This indicator reflects the "current" impact/attention (the "hype") of an article in the research community at large, based on the underlying citation network. | Top 10% | |
influence This indicator reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically). | Top 10% | |
impulse This indicator reflects the initial momentum of an article directly after its publication, based on the underlying citation network. | Top 10% |