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A reheat-regenerative engine receives steam at 207 bar and 59.3 °C, expanding it to 38.6 bar, 343°C. At this point the steam passes through a reheater and reenters the turbine at 34.5 bar. 593°C, hence expands to 9 bar, 492°C, at which point the steam is bled for feedwater heating. Exhaust occurs at 0.07 bar. Beginning at the throttle (point 1) enthalpies are known (in kJ/kg). 


An ideal reheat turbine with one-stage of reheat receives steam at 8.0 MPa, 480 °C. Reheat pressure is 0.83 MPa and exhaust pressure is 0.007 MPa. The work is 1559 kJ/kg and the thermal efficiency is 41.05%. Find the temperature of the steam leaving the reheater. 


Expand 2 kg of steam at 15 bar, 320°C, into the wet region to 100°C in a polytropic process where pv1.21 = C. Determine (a) y2, (b) ΔH, (c) ΔS, (d) nonflow and steady flow work, and (e) Q.


If a load of 100kg is to be lifted with a lever inclined at 35 degrees to horizontal with a force of 750N. Calculate the coefficient of friction.

A rigid tank contains air at 1.5 bar and 600C. The pressure of air is raised

to 2.5 bar by transfer if heat from a constant temperature reservoir at

4000C. The temperature of the surroundings is 270C. Determine per kg of

air, the loss of available energy due to heat transfer.


A reheat cycle with one stage of reheating is executed with steam initially from 90 bar and

530 C. The reheater pressure is 10 bar and the steam leaves the reheater at 480 C.

Condensation occurs at 0.03 bar. find a) W and Wp, b) Heat added, c) Heat rate of the engine


The diameter of an open-topped tank 1.5 m high increases uniformly from 4.2 m at the [20] base to 6 m at the top. Discharge from the base of the tank takes place through a

75 mm diameter pipe which is 3 m in length. The pipe discharges the water to the atmosphere 1.5 m below the base of the tank. Initially, the tank is fully filled with water.

Take ƒ = 0.01. Find the time to empty the tank.


In a steady flow apparatus, 250 k} of work is done by each kg of the fluid. The specific volume of the fluid, pressure and speed at the inlet are 0.37m*/kg, 600 kPa and 16 m/s. The inlet is 32 m above the floor under the discharge pipe is at lour level. The discharge conditions arc 0.62 m*/kg, 100 kPa and 270 m/s. The internal energy decreases from 100 k/kg to S0 k/kg. How much heat in kJ kg is added to the system? (15 points)


3. For a certain ideal gus R = 25.8 d k = 1.09 What is the value of c, in points) You sent b.What rass (in lb) of this gas would occupy a volume of 15 eu ft at 75 psia and 80 degrees Fahrenheit? points) f 30 BTU are transferred to thais gas at constant volume in (bj, what is the resulting temperature in degrees Fahrenheit? (1 BTU-778 ft h An adiabatic expansion of air occurs through a nozzle from 828 kPa and 71 degrees Celsius to 138 kPa. The initial kinetic energy is negligible. Far an isentropic expansion compile the speed the (5 points) exit section (1S peints)


One kilogram of gas at an initial pressure of 0.11 MN/m2 and a temperature of 150C.


It is compressed isothermally until the volume becomes 0.1 m3. Determine


a) the final pressure


b) the final temperature


c) the heat transfer


If the compression had been adiabatic, determine


d) the final pressure


e) the final temperature


f) the work transfer


For the gas, take cp = 0.92 KJ/kg K cv = 0.66 KJ/kg K


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