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////Chapter No 14 Air Standard Cycles
////Example No 14.3 Page No 303
///Find pressure at intermediate salient points
//Input data
clc;
clear;
//Refer figure
T1=300; //Carnot engine work in minimum temperature in kelvin
T2=750; //Carnot engine work in maximum temperature kelvin
P2=50; //pressure of carnot engine N/m^2
P4=1; //pressure of carnot engine N/m^2
//Considering air as the working fluid therefore
R=0.287; //Air as the working fluid in KJ/Kg K
Cp=1.005; //KJ/Kg K
Cv=0.718; //KJ/Kg K
K=1.4;
gamma1=1.4;
//Calculation
//T2/T1=(P2/P1)**(gamma1-1)/gamma1;
P1=P2*(T1/T2)^(gamma1/(gamma1-1)); //Pressure at intermediate salient points(1-2) in bar
P3=P4*(T2/T1)**(gamma1/(gamma1-1)); //Pressure at intermediate salient points(3-4) in bar
QS=R*T2*log(P2/P3 ); //Heat supplied and rejected per Kg of air in KJ/Kg
QR=R*T1*log(P1/P4 ); //Heat supplied and rejected per Kg of air in KJ/Kg
W=QS-QR; //Work done in KJ/Kg
eta=(1-(T1/T2)); //Thermal of the carnot cycle
//Output
printf('pressure at intermediate salient points(1-2)= %f bar \n',P1);
printf('pressure at intermediate salient points(3-4)= %f bar \n',P3);
printf('heat supplied and rejected per Kg of air(2-3)= %f KJ/Kg \n',QS);
printf('heat supplied and rejected per Kg of air(4-1)= %f KJ/Kg \n',QR);
printf('work done= %f KJ/Kg \n',W);
printf('thermal of the carnot cycle= %f percent \n',100*eta);
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