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-rwxr-xr-x3257/CH2/EX2.1/Ex2_1.sce14
-rwxr-xr-x3257/CH2/EX2.1/Ex2_1.txt4
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diff --git a/3257/CH2/EX2.1/Ex2_1.sce b/3257/CH2/EX2.1/Ex2_1.sce
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+// Calculation of ultimate tensile strength
+clc
+K = 689655 // in kPa
+n = 0.5
+A0 = 1 // let
+printf("\n Example 2.1")
+sigma = K*n^n
+A_neck = A0*exp(-n)
+P= sigma*A_neck
+UTS = P/A0
+printf("\n True ultimate tensile strength is %.2fkPa",sigma)
+printf("\n Engineering UTS of material is %.2f kPa",UTS)
+// Answer in book is 295521.79 kPa
+
diff --git a/3257/CH2/EX2.1/Ex2_1.txt b/3257/CH2/EX2.1/Ex2_1.txt
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+
+ Example 2.1
+ True ultimate tensile strength is 487659.73kPa
+ Engineering UTS of material is 295780.58 kPa \ No newline at end of file