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The compressor and turbine of a simple gas turbine engine each have isentropic efficiencies of 95%. The compressor pressure ratio is 12. The minimum and maximum temperatures in the engine are 290 K and 1400 K, respectively. On the basis of an air standard analysis, assuming Brayton cycle for the operation of the engine, determine:
(a) the net work per unit mass of air flowing, in kJ/kg,
(b) the heat rejected per unit mass of air flowing, in kJ/kg, and
(c) the thermal efficiencies for the actual cycle and an ideal cycle (i.e. if the compressor and turbine operates isentropically).
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Steam enters a diffuser at and with a velocity of and exits as saturated vapor at 240 F and 100 ft/s. The exit area of the diffuser is 1 ft2. Determine the mass flow rate of steam and the rate of entropy generation.
Average pressure at end of stroke? Upsetting force required at the end of the stroke? If friction is neglected, what is the amount of upsetting force?
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