Question #230098

. 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


1
Expert's answer
2021-08-30T17:54:51-0400

Solution;

Given;

Temperature of air,t1=20°ct_1=20°c

Velocity of air, C1=40m/sC_1=40m/s

Temperature of air after passing the heat exchanger,t2=820°ct_2=820°c

Velocity of air at entry to the turbine,C2=40m/sC_2=40m/s

Temperature of air leaving the turbine,t3=620°ct_3=620°c

Velocity of air at entry to nozzle,C3=55m/sC_3=55m/s

Temperature of air after expansion through the nozzle,t4=510°ct_4=510°c

Air flow rate, m˙=2.5kg/s\dot{m}=2.5kg/s

(i) Heat exchanger;

To find the rate of heat transfer;

From Energy equation given by;

m(h1+C122+z1g)+Q12=m(h2+C222+z2g)+W12m(h_1+\frac{C_1^2}{2}+z_1g)+Q_{1-2}=m(h_2+\frac{C_2^2}{2}+z_2g)+W_{1-2}

In which ;

z1=z2z_1=z_2

C1,C2C_1,C_2 =0=0

W12=0W_{1-2}=0

Therefore ,the equation reduces to;

mh1+Q12=mh2mh_1+Q_{1-2}=mh_2

Q12=m(h2h1)Q_{1-2}=m(h_2-h_1)

Q12=mcp(t2t1)Q_{1-2}=mc_p(t_2-t_1)

Q12=2.5×1.005×(82020)Q_{1-2}=2.5×1.005×(820-20)

Q12=2010kJ/sQ_{1-2}=2010kJ/s

Answer;

2010kJ/s

(ii) Turbine;

Power output from Turbine;

Energy equation for turbine will be ;

m(h2+C222)=m(h3+C322)+W23m(h_2+\frac{C_2^2}{2})=m(h_3+\frac{C_3^2}{2})+W_{2-3}

Since;

Q23=0Q_{2-3}=0

z1=z2=z3z_1=z_2=z_3

W23=m[(h2h3)+(C22C322)]W_{2-3}=m[(h_2-h_3)+(\frac{C_2^2-C_3^2}{2})]

W23=m[cp(t2t3)+C22C322]W_{2-3}=m[c_p(t_2-t_3)+\frac{C_2^2-C_3^2}{2}]

W23=2.5[1.005(820620)+(4025522×1000)]W_{2-3}=2.5[1.005(820-620)+(\frac{40^2-55^2}{2×1000})]

W23=2.5[201+0.7125]W_{2-3}=2.5[201+0.7125]

W23=504.3kJ/sW_{2-3}=504.3kJ/s

Answer;

504.3kW

(iii) Nozzle

Velocity at exit from the nozzle;

Energy Equation for the nozzle will be ;

h3+C322=h4+C422h_3+\frac{C_3^2}{2}=h_4+\frac{C_4^2}{2}

Since;

z1=z2z_1=z_2

W34=0W_{3-4}=0

Q23=0Q_{2-3}=0

C422=cp(t3t4)+C322\frac{C_4^2}{2}=c_p(t_3-t_4)+\frac{C_3^2}{2}

C422=1.005(620510)+5522×1000\frac{C_4^2}{2}=1.005(620-510)+\frac{55^2}{2×1000}

C4=473m/sC_4=473m/s

Answer;

473m/s



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