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diff --git a/2873/CH3/EX3.8/Ex3_8.sce b/2873/CH3/EX3.8/Ex3_8.sce
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+// Display mode
+mode(0);
+// Display warning for floating point exception
+ieee(1);
+clear;
+clc;
+disp("Engineering Thermodynamics by Onkar Singh Chapter 3 Example 8")
+T1=(627+273);//initial temperature of air in nozzle in K
+T2=(27+273);//temperature at which air leaves nozzle in K
+Cp=1.005*10^3;//specific heat at constant pressure in J/kg K
+disp("applying steady flow energy equation with inlet and exit states as 1,2 with no heat and work interaction and no change in potential energy")
+disp("h1+C1^2/2=h2+C2^2/2")
+disp("given that C1=0,negligible inlet velocity")
+disp("so C2=sqrt(2(h1-h2))=sqrt(2*Cp*(T1-T2))")
+disp("exit velocity(C2)in m/s")
+C2=sqrt(2*Cp*(T1-T2))
+disp("so exit velocity=1098.2 m/s")
+