By G. Boxer
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Additional info for Applications of Engineering Thermodynamics: A tutorial text to Final Honours degree standard
Heat transfer between the gas and the cylinder walls during the process is negligible. 0 bar and a temperature of 300 K. Assume that both the residual gas and the new charge are perfect gases for which 'Y = 1. 38 and cp = 1. 005 kJ I (kg K) . 84 ~2 13 1 I I v I ---+! 4 refers. 275 = 938 K = v1(1 ~~~)2. E. T1(~)k = 1000 Pl T2 V2 + P2 (V3 - V:L) X = 0. 2 77 1. 424 = 0 · 846 5. In the air standard cycle of a proposed internal combustion engine, heat transfer to the air takes place at constant temperature, while heat transfer from the air takes place at constant pressure.
65 = 1. 012 Further Examples 8. 335 kg/(kW h) when the calorific value of the fuel is 44 200 kJ/kg. The mechanical efficiency is 80%. Calculate the indicated thermal efficiency. Calculate the brake and indicated mean effective pressures of the engine at this load if the gravimetric air-fuel ratio is 18, the volumetric efficiency is 82% and the ambient conditions are 1 bar and 20 °C. The engine has a compression ratio of 6. Determine the efficiency of the comparable air standard Otto cycle and thence the indicated efficiency ratio for the engine.
34 bar. 645 mm 2 and 2967 mm 2 respectively. Determine (a) the steam mass flow rate, (b) the dryness fraction of the steam at exit, (c) the isentropic efficiency of the nozzle. 58. 6 refers. Pt = 7 4. 06 bar 0. 135 = 450 !!!. uA] [-v 450 = 106 1 x 406 s X X 645 = 0. 5 .!!!. 4 """"484 = 0. 854 (c) 7. A perfect gas flows steadily through an adiabatic convergentdivergent nozzle into a large vessel in which the pressure can be maintained at any desired value. At inlet to the nozzle the gas temperature is 540 °C, the pressure 7 bar and the velocity negligible.
Applications of Engineering Thermodynamics: A tutorial text to Final Honours degree standard by G. Boxer