State Engineering Service Mains Exam-2016
Paper II
1. (A) Final the heat transferred to a gas of 2 kg when it is heated mom 20 °C to 100 °C . The specific heat of gas at constant volume is given lay C = (0.5 + 0.005 T) kJ kg °C also find out the mean value of specific heat.
(B) A
stone of mass 10 kg and tank containing 100 kg water are initially at same temperature.
A stone above 100 m falls into the water. Considering the stone and water as a
system, determine AU, APE, AKE $ and W, When
(i) the stone is about to enter the water
(ii) the stone has come to rest in the tank.
(C) In ii flow ink river a body is immersed at a depth of 3.5 in and the pressure on the upstream face of the body is found to be 35.30 kN/m² find the velocity of the river at that depth.
(D) If the velocity distribution in the boundary layer is given by determine the displacement thickness. the momentum thickness and the energy thickness.
(E) The temperature distribution across a wall 1 m thick at a certain instant of time is given by T(x)= a + bx + cx²
while a = 900 °C, b = -300 °C/m and C = -50 °C/m2.
A uniform heat generation q = 1000 W/m3 is present
in the wall area of 10 m2 having the property K = 40 W/m K. Determine the rate
of heat transfer entering the wall (x — 0) and leaving the wall (s — 1 m). Also
calculate the rate of change of energy storage in wall.
(F) A system for heating water from an inlet temperature of 20 °C to an outlet temperature of 60 °C involves passing the water through a thick walled tube having inner and outer diameters of 20 and 40 mm. The outer surface of the tube is well insulated and electrical heating within the wall provides for a uniform generation of heat of q = 10 W /m³. For a water mass flow rate of m = 0.1 kg/s, how long must the tube be to achieve the desired outlet temperature ?
Take Cp =
4179 J/kg- K.
(G) An engine working on otto-cycle has a volume of 0.5 m° pressure I bar and temperature of 27 °C at the beginning of the compression stroke. At the end of the compression stroke, the pressure is 10 bar, 210 kf of heat is added during constant volume heating process. Calculate the pressures, temperatures and volumes at salient points in the cycle.
(H) For a vapour compression refrigeration system, sketch p-h diagram on T-S diagram and express the coefficient of performance of the cycle in terms of enthalpies.
(I) Explain any three geometry statements and three motion statements in APT language.
(J) Explain the general application characteristics in an environment of material handling by robots.
2. (A) Three pipes of same length L, diameter D and friction factor f are connected in parallel. Determine the diameter of the pipe of length L and friction factor f which will carry the same discharge for’the same head
(ii) the temperature of shield and (iii) heat transfer per m2 with shield.
(B) A vapour compression cycle with ammonia as refrigerant works between the limits of saturated suction temp. of —20 °C and saturated condensing temp. of 30 °C. lt is a simple saturated cycle and compression is isentropic, determine the work of compression per kg of ammonia. Compare the same if ammonia vapours leaving the evaporator at —20 °C is absorbed by water so that the mass concentration in the solution reaches about 40% and its solution is pumped to the condenser pressure.
Assume specific volume of solution to be 0.001161 m3/kg. Assume
h2 — 1420 kJ/kg and h3 = 1668 kJ/kg. (p-h chart values)Diameter of the cylinder — 80 mm, stroke of the piston = 100 mm. Speed of the engine = 3000 rpm, Load on the hydraulic dynamometer = 160 N, Dynamometer constant - 20420 when speed is in rpm. Fuel consumption = 8 kg/hr. Cp of the fuel used - 43000 kJ/kg. The temperature and pressure of the charge at the end of suction stroke = 15 °C and 1 bar. A : F ratio = 13 : 1.
For the determination of the mechanical efficiency of the engine, a Morse test was carried out by shooting the spark plugs of each cylinder successively without change of speed. The corresponding BP’s of the engine are 16.5, 16, 1 5.6 and 17.6 kW respectively. Determine :
(i) The BP, Brake mean effective pressure and Brake thermal efficiency of the engine.(ii) Also find the mechanical efficiency and volumetric efficiency of the engine at suction condition.
(B) A gas turbine plant operates on Brayton cycle between temp. limit of 1100 °K and 310 °K. Calculate the maximum work done per kg of air (kJ/kg) and corresponding cycle efficiency.
6.(A) A Kaplan turbine develops 24647.6 kW power at an average head of 39 meters. Assuming a speed ratio of 2, flow ratio of 0.6, diameter of the boss equal to 0.35 times the diameter of the runner and an overall efficiency of 90%. Calculate the diameter, speed and specific speed of the turbine.
(B) A simple turbo-jet unit operates with a turbine inlet temperature of 1100 K, a pressure ratio is 4 : 1 and air man flow of 22.7 kg/sec under design conditions. The following component efficiencies may be assumed :
Isentropic compressor
efficiency |
— |
0.85 |
Isentropic turbine efficiency |
— |
0.90 |
Propelling nozzle efficiency |
— |
0.95 |
Transmission efficiency |
— |
0.99 |
Combustion chamber pressure
loss |
— |
0.21 |
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