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+// scilab Code Exa 18.3 Irreversible flow in nozzles
+pr=0.843; // pr=p/p0
+n_n=0.95; // nozzle efficiency
+gamma=1.4;
+Ms=0.5; // from gas tables for gammma and pr value
+Ma=sqrt((2/(gamma-1))*(n_n/(1-n_n+(2/((gamma-1)*(Ms^2))))));
+disp(Ma,"actual value of the Mach number is")