2021
DOI: 10.1007/s10973-020-10449-9
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Performing thermodynamic analysis by simulating the general characteristics of the two-spool turbojet engine suitable for drone and UAV propulsion

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Cited by 21 publications
(3 citation statements)
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“…As a result, CO2 emission values were calculated between 1.88 kg/s and 1.5 kg/s according to different altitude cruise conditions. Koruyucu et al [12] determined the performance parameters of a two-spool turbojet engine model using thermodynamic analysis. As a result of the study, it was stated that when the engine thrust is 516 daN, and the thrust specific fuel consumption (TSFC) rate is about 19.7 g/kN.s.…”
Section: Introductionmentioning
confidence: 99%
“…As a result, CO2 emission values were calculated between 1.88 kg/s and 1.5 kg/s according to different altitude cruise conditions. Koruyucu et al [12] determined the performance parameters of a two-spool turbojet engine model using thermodynamic analysis. As a result of the study, it was stated that when the engine thrust is 516 daN, and the thrust specific fuel consumption (TSFC) rate is about 19.7 g/kN.s.…”
Section: Introductionmentioning
confidence: 99%
“…According to this analysis, exergy efficiency and EEF of the TF33 engine were found as 34.86% and 1.86, respectively. Koruyucu et al 16 investigated general characteristics of turbojet engine by performing thermodynamic analysis. The authors stated that thrust of the engine was determined as 516 daN whereas its SFC was measured as 19.706 g/kNs.…”
Section: Introductionmentioning
confidence: 99%
“…Moreover, the causes leading to fuel inefficiency could be understood with exergetic parameters. Therefore, when considering the literature, there are many of studies on thermodynamic and environmental based analyses for aircraft engines (Dinc et al 2022 ; Ekici and Sohret 2021 ; Koruyucu et al 2021 ). There are two ways that deal with the environmental effect from aircraft engine.…”
Section: Introductionmentioning
confidence: 99%