. Air at a temperature of 20°C passes through a heat exchanger at a
velocity of 40 m/s where its temperature is raised to 820°C. It then enters a turbine with same
velocity of 40 m/s and expands till the temperature falls to 620°C. On leaving the turbine, the air
is taken at a velocity of 55 m/s to a nozzle where it expands until the temperature has fallen to
510°C. If the air flow rate is 2.5 kg/s, calculate :
(i) Rate of heat transfer to the air in the heat exchanger ;
(ii) The power output from the turbine assuming no heat loss ;
(iii) The velocity at exit from the nozzle, assuming no heat loss.
Take the enthalpy of air as h = cpt, where cp is the specific heat equal to 1.005 kJ/kg°C and
t th
Solution;
Given;
Temperature of air,
Velocity of air,
Temperature of air after passing the heat exchanger,
Velocity of air at entry to the turbine,
Temperature of air leaving the turbine,
Velocity of air at entry to nozzle,
Temperature of air after expansion through the nozzle,
Air flow rate,
(i) Heat exchanger;
To find the rate of heat transfer;
From Energy equation given by;
In which ;
Therefore ,the equation reduces to;
Answer;
2010kJ/s
(ii) Turbine;
Power output from Turbine;
Energy equation for turbine will be ;
Since;
Answer;
504.3kW
(iii) Nozzle
Velocity at exit from the nozzle;
Energy Equation for the nozzle will be ;
Since;
Answer;
473m/s
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