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diff --git a/2223/CH2/EX2.6/Ex2_6.sav b/2223/CH2/EX2.6/Ex2_6.sav
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diff --git a/2223/CH2/EX2.6/Ex2_6.sce b/2223/CH2/EX2.6/Ex2_6.sce
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+// scilab Code Exa 2.6 calculation on a gas turbine

+

+funcprot(0);

+p1=5; // Inlet Pressure in bar

+p2=1.2; // Exit Pressure in bar

+T1=500;  // Initial Temperature in K

+gamma=1.4;

+m=20; // mass flow rate of the gas in kg/s

+cp=1.005; // Specific Heat at Constant Pressure in kJ/(kgK)

+n_T=0.9; // Overall Efficiency 

+pr=p1/p2; // Pressure Ratio

+// part(a)

+T2s=T1/(pr^((gamma-1)/gamma));

+T2=T1-(n_T*(T1-T2s));

+n_p=(log(T1/T2))/(log(T1/T2s));

+disp("%",n_p*100,"(a)small stage Efficiency or polytropic efficiency of the expansion is")

+P=m*cp*(T1-T2);

+disp("kW",P,"and Power developed is")

+

+// part(b)

+AR=2.5; // Area Ratio of Diffuser

+R=0.287; // Universal Gas Constant in kJ/kgK

+p3=1.2; // Exit Pressure for diffuser in bar

+c2=75; // Velocity of gas at turbine exit in m/s

+c3=c2/AR;

+n_d=0.7; // Efficiency of the diffuser

+ro2=p2/(R*T2);

+delp=n_d*(0.5*0.001*ro2*((c2^2)-(c3^2))); // delp=p3-p2d

+disp("mm W.G.",delp*100000/9.81,"(b)static pressure across the diffuser is")

+p2d=p3-delp;

+prd=p1/p2d;

+T2sd=T1/(prd^((gamma-1)/gamma));

+T2d=T1-(n_T*(T1-T2sd));

+Pd=m*cp*(T1-T2d);

+disp("kW",Pd-P,"and Increase in the power output of the turbine is")

+

+disp("Comment: Error in Textbook, Answers vary due to Round-off Errors")