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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


What is the difference between bending stress and pitting resistance? And why is it important to verify the bending stress of the standard selected gears.

The center rod CD of the assembly shown in the figure is heated from T1 = 30oC to T2 = 180oC using electrical resistance heating. The two end rods AB and EF are heated from T1 = 30oC to  T2 = 50oC. At the lower temperature T1, the gap between C and the rigid bar is 0.7 mm. Rods AB and EF are made of steel and each have a cross-sectional area of 125 mm2. CD is made of aluminum and has a cross-sectional area of 375 mm2. ESteel = 200 GPa, EAluminum = 70 GPa,    αsteel = 12x10-6/oC, αAluminum = 23 x10-6 /oC.

Calculate the force and the stress in rods AB, EF and CD caused by the increase in temperature.  


CEO of a well-known television show wants to build a new rectangular shaped acting stage. The width, thickness and length of the stage are 3 m, 0.2 m and 5 m, respectively. Both ends of the stage must be fixed. The stage should carry a musical instrument, and air conditioner of a total mass of 1500 kg and 800 kg at 1 m, and 2 m from the left end support. Such equipment acts as a concentrated loads on the stage that has a distributed load of 500 kg/m. The Young’s modulus of the material is 200 GPa. 1.1. Use the engineering sketch to illustrate the structure of the stage and calculate the transverse vibration frequency of the stage. (18) 1.2. Determine the amount of rection forces on the stage supports.
1.2 For the purpose of turbine design, there is a need for aerodynamics test of the nose corn design in a wind tunnel. Suppose that the fluid enters the test section of a circular tunnel with a uniform speed of 50 m/s and it flows over a nose corn placed at the centreline of the tunnel, as shown in Fig. 1, the nose corn rotates at a constant speed w=10 rad/s about the centreline of the tunnel. Assume that the flow is laminar and fully developed before exits from the tailpipe, with the information given above, provide a set of governing equations and boundary conditions in its simplest form that can be used to determine the unique flow through the tunnel, in terms of fluid velocity and pressure distributions.
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