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Appl. Sci. 2020, 10, 9060 18 of 25 Author Contributions: Conceptualization, S.-P.M. and L.-L.R.; data curation, T.-G.E.V.; formal analysis, L.-M.H. and V.-L.J.; investigation, T.-G.E.V.; methodology, L.-M.H., T.-G.E.V., C.-H.S., and L.-L.R.; project administration, L.-L.R.; software, L.-M.H. and T.-G.E.V.; supervision, S.-P.M. and L.-L.R.; validation, L.-M.H. and C.-H.S.; visualization, C.-H.S.; writing, original draft, L.-M.H.; writing, review and editing, S.-P.M., V.-L.J., and L.-L.R. All authors have read and agreed to the published version of the manuscript. Funding: This research received no external funding. Acknowledgments: Castro-Hernández S. gratefully acknowledges the scholarship from the Mexican National Council for Science and Technology (CONACyT) to pursue his postgraduate studies. Conflicts of Interest: The authors declare no conflict of interest. Abbreviations The following abbreviations are used in this manuscript: AC air compressor, ACC annual capital cost, CRF capital recovery factor, chS chemical-gas stack, cS cold-gas stack, CC combustion chamber, C compressor, D diffuser, ECT exergetic cost theory, F fan, FN fan nozzle, GT gas turbine, HPT high pressure turbine, LPT low pressure turbine, N nozzle, OMC overhaul and maintenance cost, PW present worth, PVF present value factor, PFR product-resource-residue, FPR resource-product-residue, SV salvage ratio, TOT total, TCI total capital investment. Nomenclature x actual conditions, x0 reference conditions, Z ̇ capital cost rate of a component (USD h−1), D dissipative components, z elevation (m), H enthalpy (kJ), H ̇ enthalpy flow rate (MW), S ̇ entropy generation (MW), c exergoeconomic cost per unit of exergy (USD GJ−1), P∗ exergetic cost of the product (MW), F∗ exergetic cost of the resource (MW), R∗ exergetic cost of the waste (MW), f exergoeconomic factor (%), E ̇ exergy flow rate (MW), w flight velocity (m s−1), far fuel/air ratio (kgf (kgair)−1), R gas constant (kJ (kgK)−1), g gravitational acceleration 9.81 m s−2,PDF Image | Residue Cost Formation of a High Bypass Turbofan Engine
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