Why does this error read
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P1 = 101 %pressure in kpa
T1 = 298%temperature in kelvin
n = 1.4
Cp = 1.004
Cv = 0.717
R = 0.287 %gas constant in kJ/kg*k
v1 = R * T1/P1 %specific volume in m^3/kg
IsentConst1 = P1 * v1^n
P2 = 2828 %outlet compressor/inlet combuster pressure
T2 = ((P2 / P1)^((n-1)/n)) * (T1)
v2 = (R * T2) / P2
Wc = Cp * (T2 - T1)
P3 = P2
T3 = 2260
v3 = R * T3 / P3
IsentConst2 = P3 * v3^n
Wt = Wc
T4 = (Wt / Cp) + T3
v4 = ((P3 * v3^n)/(R * T4)^(1/n-1))
P4 = R * T4 /v4
IsentConst3 = P4 * v4^n
u4 = Cv * T4
h4 = u4 + P4 * v4
P5 = P1
v5 = (P4 *v4^n / P5)^(1/n)
T5 = P5 *v5 / R
u5 = Cv * T5
h5 = u5 + P5 * v5
dh = (h5 - h4)*1000 %performance parameter
P = P1:0.001:P2;
v = v1:-0.001:v2;
plot(v,P,'r','lineWidth',1.5)
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