Consider a gas turbine power plant operating at steady state
Solution
solution:
1)here for compressor work isgiven by
-Wc=mCp(T2-T1)
here 1 Hp=.7067 BTu/s,Cp=.24
1191.8549=38.165*.24*(T2-520)
T2=650.12 R
here work of compression is
wc=-1191.8549/m=-31.22 BTU/lb
where enthalphy are
h1=Cp*T1=.24*520=124.8 BTu/lb
h2=Cp*T2=.24*650.12=156 BTU/lb
3)for combustor heat supplied is given by
n=net work/heat supplied
heat supplied=Wt-Wc=14506-1686.3/.68=18852.5 Hp or 13323.7020 BTU/s
heat supplied per unit mass =13323.7020/38.165=349.13 BTu/lb
Qs=MCp(T3-T2)
T3=2104.72 R
here enthlpy are
h3=Cp*T3=.24*2104.72=505.13 BTU/lb
4)for turbine work is given by
Wt=m*Cp*(T3-T4)
T4=985.42 R
work done is given per pound is
Wt=Wt/m=10252.6523/38.165=268.64 BTU/lb
5)for rejected heat we have that
Qr=mCp(T4-T1)
Qr=4263.90 BTU/s or 6032.79 HP
per lb
qr=111.72 BTU/lb
7)in this way all underlined parameter are found


