An ideal air-standard Brayton cycle operates at steady state with compressor inlet conditions of 300K
and 100kPa and a fixed turbine inlet temperature of 1700K. For the cycle, determine (a) the pressure
ratio for given thermal efficiency of 45% and (b) the net power developed
Answer:-
"T_1=300k \\\\\np_1=100k\\\\\nT_3=1700k\\\\"
"r_p=(\\frac{P_2}{P_1})=8"
assume air working medium
r=1.4 , "C_p=1.005 K\/kg , m=1kg\\\\"
"process \\ \\ 1-2\\\\\n\\frac{T_2}{T_1}=(\\frac{P_2}{P_1})^{1.4-1\\over 1.4}"
"T_2=300\\times (8)^{1.4-1\\over 1.4}"
"\\boxed{T_2=543.43K}"
process 3-4
with same formula
"T_4=938.5K"
net power=power in turbine-power in compression
Net Power (P)="mC_p(T_3-T_4)-mC_p(T_2-T_1)"
putting values we get
"P_{net}=1\\times1.005[(1700-938.5)]"
=520.66Kw m=1kg/sec
"\\eta=1-\\frac{1}{(r_p)^{\\frac{r-1}{r}}}"
"\\eta=1-\\frac{1}{(8)^{\\frac{1.4-1}{1.4}}}"
"\\boxed{\\eta_{th}=45 \\%}"
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