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+// Problem 11.2,Page no.274
+
+clc;clear;
+close;
+
+d=2 //cm //Diameter of specimen
+
+//Calculations
+
+//Let P be the Load on the section
+
+A=%pi*4**-1*d**2 //cm**2 //Area of section
+I=%pi*64**-1*d**4 //cm**4 //M.I of the section
+y=d*2**-1 //cm
+Z=I*y**-1 //cm**3 //Section modulus
+//M=P.e //Moment
+
+//Stress due to direct load
+//sigma_d=(4*P)*(%pi*d**2)**-1 //N/cm**2
+
+//stress due to moment
+//sigma_b=(32*P*e)*(%pi*d**3)**-1 N/cm**2
+
+//Maximum stress
+//sigma_r_max=(((4*P)*(%pi*d**2)**-1)+((32*P*e)*(%pi*d**3)**-1))
+
+//Mean stress 
+//sigma_r_mean=((4*P)*(%pi*d**2)**-1) 
+
+//Since the maximum stress is 20% greater than the mean stress 
+//(((4*P)*(%pi*d**2))+((32*P*e)*(%pi*d**3)))=1.2*4*P*(%pi*d**2)**-1
+
+//After substituing values and simplifyinf we get
+
+e=0.2*d*8**-1 //cm //distance of line of thrust from the axis
+
+//Result
+printf("The distance of line of thrust from the axis is %.2f",e);printf(" cm")