Air Standard cycle

Objective: close allclear allclc %inputs gamma=1.2;t3=2000; %state variables p1=202650;t1=600; %Engine geometric parameters bore=0.2;stroke=0.3;con_rod=0.14;cr=10; %state variable1 v_s=pi/4*bore^2*stroke;v_c=v_s/(cr-1); v1=v_s+v_c;v2=v_c; %state variable 2%p2v2^gamma=p1v1^gamma|p2==p1*(v1/v2)^gamma|cr=v1/v2p2=p1*(v1/v2)^gamma;%p1v1/t1=p2v2/t2…