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Abstract
In this study, exergetic and exergoeconomic analysis methods are applied to a four-cylinder, spark ignition (SI), naturally aspirated and air-cooled piston-prop aircraft engine in the cruise phase of flight operations. The duration of cruise is selected to be 1 h. Three parameters, altitude, rated power setting (PS), and air-to-fuel ratio (AF), are varied by the calculation of the max–min values of exergy analysis. Based on the results of energy analysis, the values for the maximum energy efficiency and fuel consumption flow rate are calculated to be 21.73% and 28.02 kg/h, respectively, at 1000-m altitude and 75% PS. The results of exergy analysis indicate that all exergetic values vary from 65% to 75% PS, while this increase is not seen in exergoeconomic analysis. While the maximum exergy input rate is obtained to be 405.60 kW, exergy efficiency has the minimum value with 14.43% and exergy destruction rate has the maximum value with 168.48 kW. These values are achieved at 3000-m altitude and 18 AFs. The maximum average exergy cost of the fuel is calculated to be 130.77 $/GJ at 1000-m altitude, 13 AF ratios, and 65% PS. At this point, while the minimum cost rate associated with the exergy destruction is obtained to be 40.29 $/h, the maximum exergoeconomic factor is found to be 19.98%.