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Air is compressed from an inlet condition of 100 kPa, 300 K to an exit pressure of 1000 kPa by an internally reversible compressor. Determine the compressor power per unit mass flow rate if the device is (a) isentropic, (b) polytropic with n =1.3, (c) isothermal

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Answer:

(a)
W_(isoentropic)=8.125(kJ)/(mol)

(b)
W_(polytropic)=7.579(kJ)/(mol)

(c)
W_(isothermal)=5.743(kJ)/(mol)

Step-by-step explanation:

Hello,

(a) In this case, since entropy remains unchanged, the constant
k should be computed for air as an ideal gas by:


(R)/(Cp_(air))=1-(1)/(k) \\\\(8.314)/(29.11) =1-(1)/(k)\\


0.2856=1-(1)/(k)\\\\k=1.4

Next, we compute the final temperature:


T_2=T_1((p_2)/(p_1) )^(1-1/k)=300K((1000kPa)/(100kPa) )^(1-1/1.4)=579.21K

Thus, the work is computed by:


W_(isoentropic)=(kR(T_2-T_1))/(k-1) =(1.4*8.314(J)/(mol*K)(579.21K-300K))/(1.4-1)\\\\W_(isoentropic)=8.125(kJ)/(mol)

(b) In this case, since
n is given, we compute the final temperature as well:


T_2=T_1((p_2)/(p_1) )^(1-1/n)=300K((1000kPa)/(100kPa) )^(1-1/1.3)=510.38K

And the isentropic work:


W_(polytropic)=(nR(T_2-T_1))/(n-1) =(1.3*8.314(J)/(mol*K)(510.38-300K))/(1.3-1)\\\\W_(polytropic)=7.579(kJ)/(mol)

(c) Finally, for isothermal, final temperature is not required as it could be computed as:


W_(isothermal)=RTln((p_2)/(p_1) )=8.314(J)/(mol*K)*300K*ln((1000kPa)/(100kPa) ) \\\\W_(isothermal)=5.743(kJ)/(mol)

Regards.

User OysterD
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