2009
DOI: 10.1504/ijex.2009.025322
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Exergoeconomic analysis of an aircraft turbofan engine

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Cited by 41 publications
(16 citation statements)
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“…Using the data in Table 1 and Eqs. (11), (12), (14) and (15), energy and exergy loss rates are calculated for main components of the CFBG system and given in Table 2. As can be seen in Table 2, while the most energy losses belong to the gasifier and PSA equipments as 22.45 and 10.51 MW, respectively, the most exergy losses are due to the gasifier, combustion chamber and PSA components with 47.95, 15.36 and 13.14 MW, respectively.…”
Section: Resultsmentioning
confidence: 99%
See 1 more Smart Citation
“…Using the data in Table 1 and Eqs. (11), (12), (14) and (15), energy and exergy loss rates are calculated for main components of the CFBG system and given in Table 2. As can be seen in Table 2, while the most energy losses belong to the gasifier and PSA equipments as 22.45 and 10.51 MW, respectively, the most exergy losses are due to the gasifier, combustion chamber and PSA components with 47.95, 15.36 and 13.14 MW, respectively.…”
Section: Resultsmentioning
confidence: 99%
“…_ L ex ¼ X in Exergy flow rates À X P Exergy flow rates (15) where the summations are overall input streams and all product output streams. A parameter, _ R is defined as the ratio of thermodynamic loss rate _ L to capital cost K as follows:…”
Section: 4mentioning
confidence: 99%
“…The cost coefficient of fuel, , is the key consideration of this study. As the aircraft model under study is A320-200s, which has turbofan engines, the important relationship of altitude, Mach number and velocity of a turbofan is accounted for (Roth and Mavris, 2001;Turgut et al, 2009…”
Section: Study Of Flight Trajectory Optimizationmentioning
confidence: 99%
“…In the meantime, several studies have also been conducted using either Jet-A1 or JP8 as the fuel [1,[5][6][7][8][9]. Most of these studies cover not only the thermodynamic analysis part, but also the economic [5,7] and sustainability factors [1,9]. However, all of them take a turbofan engine with separate exhaust as the case study.…”
Section: Introductionmentioning
confidence: 99%