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Varvara68 [4.7K]
3 years ago
4

Steam enters an adiabatic nozzle at 2.5 MPa and 450oC with a velocity of 55 m/s and exits at 1 MPa and 390 m/s. If the nozzle ha

s an inlet area of 6 cm2 , determine (a) the exit temperature. (b) the rate of entropy generation for this process.
Engineering
1 answer:
Mariulka [41]3 years ago
6 0

Answer:

(a). The value of temperature at turbine exit = 687.64 K

(b). The rate of entropy generation for this process =  S_{gen} = 0.3157 \frac{KJ}{Kg k}

Explanation:

Pressure at inlet P_{1} = 2.5 M pa

Temperature T_{1} = 450 °c = 723 K

Velocity at inlet V_{1} = 55 \frac{m}{sec}

Pressure at exit P_{2} = 1 M pa

Velocity at exit V_{2} = 390 \frac{m}{sec}

Value of specific heat for steam = 2.108 \frac{KJ}{Kg k}

(a). Apply steady flow energy equation for adiabatic nozzle

⇒ h_{1} + \frac{V_{1} ^{2} }{2000} = h_{2} + \frac{V_{2} ^{2} }{2000}  ----------- ( 1 )

⇒ h_{2} - h_{1} = \frac{V_{1} ^{2} }{2000} - \frac{V_{2} ^{2} }{2000}

⇒ C_{p} ( T_{2} - T_{1} ) =  \frac{V_{1} ^{2} }{2000} - \frac{V_{2} ^{2} }{2000}

⇒ 2.108 ( T_{2} - 723 ) = \frac{55 ^{2} }{2000} - \frac{390 ^{2} }{2000}

⇒ 2.108 ( T_{2} - 723 ) = - 74.53

⇒ ( T_{2} - 723 ) = - 35.36

⇒ T_{2} = 687.64 K

This is the value of temperature at turbine exit.

(b). Rate of entropy generation for this process is given by

S_{gen} = C_{p} log_{e} \frac{T_{2} }{T_{1} } - R log_{e} \frac{P_{2} }{P_{1} }

Put all the values in above equation we get

⇒ S_{gen} = 2.108 log_{e} \frac{687.64}{723} - 0.46 log_{e} \frac{1}{2.5}

⇒ S_{gen} = - 0.1057 + 0.4214

⇒ S_{gen} = 0.3157 \frac{KJ}{Kg k}

This is the value of entropy generation for this process.

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