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-rw-r--r--629/CH12/EX12.3/example12_3.sce9
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diff --git a/629/CH12/EX12.3/ex12_3.txt b/629/CH12/EX12.3/ex12_3.txt
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+
+ The surface temperature of the aircraft = 337 K. \ No newline at end of file
diff --git a/629/CH12/EX12.3/example12_3.sce b/629/CH12/EX12.3/example12_3.sce
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+clear
+clc
+//Example 12.3 TOTAL TEMPERATURE CALCULATION
+T=273+(-50) //static temperature [K]
+k=1.4;
+M=1.6; //Mach number
+//Total temperature
+Tt=T*(1+(k-1)*M^2/2) //[K]
+printf("\n The surface temperature of the aircraft = %.f K.\n",Tt) \ No newline at end of file