Mechanical
Engineering Written Exam Questions (Part-1)
➤ Show
that, specific speed of pump is a
dimensionless number.
➤ Draw
P-V & T-S diagram of Otto & Diesel
cycle and write down the corresponding process name.
➤ Find
the absolute pressure in Pa of 100 mm
mercury vacuum pressure.
Absolute Pressure = atmospheric pressure – vacuum pressure
= 760 – 100 = 660 mm of mercury
We also know,
P = hρg
= 88054.56 Pa
P = Absolute pressure, Pa
h = Manometer height, m
ρ = Density of mercury = 13600 Kg/m3
➤ Draw block diagram & T-S diagram for gas-steam combine cycle power plant. (For more details, click here)
➤ A
4 cylinder petrol engine has developed MEP=650 KPa, its engine diameter is 80
mm, stroke length is 100 mm, speed 3000 rpm. Find engine power in KW?
➤ For
counter flow heat exchanger Th1=160oC, Th2=125oC,
Tc1=20oC, Tc2=80oC, Draw temperature distribution curve. Also find arithmetic mean temperature
difference & logarithmic mean temperature difference.
➤ A
wire has got diameter of 20 mm, if heat transfer co-efficient is 20 W/m2.K
and thermal conductivity is 0.5 W/m.k. Then
find the distance at which maximum heat dissipation will occur.
➤ A
1.5m x 1.5m x 2m tank is kept at 11 m above from the ground. If a pump
installed on ground having efficiency of 60% can fill the tank in 30 minutes, then
find the required pump power.
➤ Engine
power developed 40 KW, solid shafts rpm 200, if the shaft diameter 40 mm then, find maximum torsional stress developer in
the shaft.
➤ Find the deflection of a
solid circular steel bar
having load 500 Kg, length 2.5 meter, diameter 60 mm & E=200 GPa.
➤ A
60 mm metal ball at 220oC is being cooled by air jet of 20oC,
heat transfer co-efficient 200 W/m.k & 100 W/m2.K, if the
specific heat of the metal ball 400 J/Kg.K, density 9000 Kg/m3, Find the temperature of the ball after 90
sec.
➤ An
aeroplane makes a complete half circle of 50 meters radius, towards left, when
flying at 200 Km/hr. the rotary engine and the propeller of the plane has a
mass of 400 Kg and a radius of gyration of 0.3 meter. The engine rotates at
2400 rpm clockwise when viewed from the rear. Find the gyroscopic couple on the aircraft.
➤ In a vapor compression refrigeration cycle inlet condenser enthalpy is 283 KJ/Kg, exit condenser enthalpy is 116 KJ/Kg, and exit evaporator enthalpy is 232 KJ/Kg, Find COP.
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