As per the given question,
Temperature of the space "(T)=298K"
Power of heat engine "(P)=1600 J\/s"
Flow of vapor=3.9kg/min
Inlet temperature "(T_i)=333K"
Outlet temperature "(T_o)=40^\\circ C=(273+40)=313K"
Entering temperature of evaporate = 285K
Quality =15%
Specific heat of saturated vapor is represented by "h_1" and specific heat of compressed vapor is represented by "h_2"
a)"\\dfrac{dW}{dt}=\\frac{dm}{dt}(h_2-h_1)\\times 0.15"
Now, substituting the values in the above equation,
"\\dfrac{dm}{dt}=\\frac{1600}{0.15(423.9-392.7)}=341.88 kg\/s"
b)"\\frac{dQ}{dt}= \\frac{3.9kg}{60s}(392.7-241.7)=9.81J\/s"
c)"E_f=1-\\frac{T_c}{T_h}"
"E_f=1-\\frac{313}{333}=\\frac{20}{333}"
"\\Rightarrow COP= \\frac{1}{E_f}"
"\\Rightarrow COP = \\frac{333}{20}=16.65"
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