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+clc
+//
+//
+
+//Variable declaration
+n=-1
+Sx=6
+Sy=3.5
+OC=4.75
+CA=3.25
+BC=3.25
+
+//Calculation
+// Case(a) Principal Planes and Principal Stresses
+Save=(Sx+Sy)/2.0 // Average stress(ksi)
+R=sqrt(1.25**2 + 3**2) // Radius of circle(ksi)
+Sa=OC+CA // Principal stress(ksi)
+Sb=OC-BC // Principal stress(ksi)
+phyp=(67.4)/2.0
+
+// Case(b) Maximum shearing stress
+tmax=(1/2.0)*(Sa) // Maximum torque(ksi)
+
+//Result
+printf("\n Case(a) Principal stress at A = %0.3f ksi' ,Sa)
+printf("\n Case(a) Principal stress at B = %0.3f ksi' ,Sb)
+printf("\n Case(b) Principal plane = %0.3f ksi' ,phyp)
+printf("\n Case(c) Maximum shearing stress = %0.3f ksi' ,tmax)