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diff --git a/3407/CH8/EX8.5/Ex8_5.sce b/3407/CH8/EX8.5/Ex8_5.sce
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+clear;
+clc;
+funcprot(0);
+
+//given data
+Z = 12;//number of vanes
+delW = 230;//in kW
+T01 = 1050;//stagnation temperature in K
+mdot = 1;//flow rate in kg/s
+eff_ts = 0.81;//total-to-static efficiency
+Cp = 1.1502;//in kJ/(kg.K)
+gamma = 1.333;
+R = 287;//gas constant
+cm3_U2 = 0.25;
+nu = 0.4;
+r3s_r2 = 0.7;
+w3av_w2 = 2.0;
+p3 = 100;//static pressure at rotor exit in kPa
+zetaN = 0.06;//nozzle enthalpy loss coefficient
+U2 = 538.1;//in m/s
+p01 = 3.109*10^5;//in Pa
+
+//Calculations
+S = delW/(Cp*T01);
+T03 = T01*(1-S);
+T3 = T03 - (cm3_U2^2)*(U2^2)/(2*Cp*1000);
+r2 = sqrt(mdot/((p3*1000/(R*T3))*(cm3_U2)*U2*%pi*(r3s_r2^2)*(1-nu^2)));
+D2 = 2*r2;
+omega = U2/r2;
+N = omega*30/%pi;
+ctheta2 = S*Cp*1000*T01/U2;
+alpha2 = (180/%pi)*acos(sqrt(1/Z));
+cm2 = ctheta2/tan(alpha2*%pi/180);
+c2 = ctheta2/sin(alpha2*%pi/180);
+T2 = T01 - (c2^2)/(2*Cp*1000);
+p2 = p01*(1-(((c2^2)*(1+zetaN))/(2*Cp*1000*T01)))^(gamma/(gamma-1));
+b2_D2 = (0.25/%pi)*(R*T2/p2)*(mdot/(cm2*r2^2));
+
+//Results
+printf('(i) The diamaeter of the rotor = %.4f m\n its speed of rotation = %.1f rad/s (N = %d rev/min)',D2,omega,N);
+printf('\n(ii) The vane width to diameter ratio at rotor inlet = %.4f',b2_D2);
+
+//there are some errors in the answers given in textbook