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Mathematics 2020, 8, x FOR PEER REVIEW 26 of 34 Mathematics 2020, 8, x FOR PEER REVIEW 26 of 34 thermal efficiency is a function of cycle net power divided by heat input. The heat input increases thermal efficiency is a function of cycle net power divided by heat input. The heat input increases with increasing the inlet temperature. For 30,000 rpm, the rate of increase of heat input is greater than Mathematics 2020, 9, 50 with increasing the inlet temperature. For 30,000 rpm, the rate of increase of heat input is greater than 24 of 30 that of cycle net power for all operating temperatures. For 40,000 rpm, on the other hand, the rate of that of cycle net power for all operating temperatures. For 40,000 rpm, on the other hand, the rate of increase of heat input from 430 to 450 K is 8.60% compared 4.17% of net power. From 450 to 471.55 increase of heat input from 430 to 450 K is 8.60% compared 4.17% of net power. From 450 to 471.55 K, the rate of increase in heat input is 4.07% compared to 5.80% of net power. This clarifies the trend K, the rate of increase in heat input is 4.07% compared to 5.80% of net power. This clarifies the trend of cycle thermal efficiency operating with 40,000 rpm. ratio equal to 9.5 while the latter results at a pressure ratio equal to 6.9. Cycle efficiency is a of cycle thermal efficiency operating with 40,000 rpm. function of cycle net power that increases with increasing turbine pressure ratio. Figure 26. Cycle thermal efficiency and net power at various pressure ratios. Figure 26. Cycle thermal efficiency and net power at various pressure ratios. Figure 26. Cycle thermal efficiency and net power at various pressure ratios. Figure 27. Cycle thermal efficiency and net power at various turbine inlet temperatures. Figure 27. Cycle thermal efficiency and net power at various turbine inlet temperatures. Figure27.CycletFhiegrumrael2e7ffischieonwcysathndatnceytcploewnertaptovwareioruisncturerbaisneesilnilneetatermlypweriatthurinesc.reasingturbineinlet 6.4. Results of Finite EtlemepnetrAatnuarleybsesca(FuEseAo) f the increased turbine power, Figure 25. The cycle thermal efficiency, 6.4. Results ofFinite Eloenmethnet Aonthaelyrshesa(nFdE,Ash)ows different trends. For 40,000 rpm, it decreases with increasing For safe operation, the maximum von Mises stress and stress and total displacement should not inlet temperature then increases, reaching the design point. For 30,000 rpm, the cycle For safe operation, the maximum von Mises stress and stress and total displacement should not exceed be the material tensile strength and the tip clearance gap between the rotor and casing. Figure efficiency decreases with increasing temperature. The different trend in both speeds is exceed be the material tensile strength and the tip clearance gap between the rotor and casing. Figure related to the definition of the cycle thermal efficiency. Cycle thermal efficiency is a function of cycle net power divided by heat input. The heat input increases with increasing the inlet temperature. For 30,000 rpm, the rate of increase of heat input is greater than that of cyclePDF Image | Generation of 3D Turbine Blades for Automotive ORC
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