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+clear
+//
+//
+
+//Initilization of Variables
+
+d=150 //mm //Diameter
+T=20*10**6 //N //Torque
+M=12*10**6 //N-mm //B.M
+F=200*10**3 //N //Axial Thrust
+
+//Calculations
+
+//M.I
+I=(%pi*64**-1*d**4)
+
+//Bending stress
+f_A=M*I**-1*(d*2**-1) //N/mm**2
+f_B=-f_A //N/mm**2
+
+//Axial thrust due to thrust
+sigma=F*(%pi*4**-1*d**2)**-1
+
+//At A
+p_x=f_A-sigma //N/mm**2
+
+//At B
+p_x2=f_B-sigma //N/mm**2
+
+p_y=0 //At A and B
+
+//Polar Modulus
+J=%pi*32**-1*d**4 //mm**4
+
+//Shearing stress at A and B
+q=T*J**-1*(d*2**-1) //N/mm**2
+
+
+//Principal Stresses
+//At A
+P1=(p_x+p_y)*2**-1+(((p_x-p_y)*2**-1)**2+q**2)**0.5 //N/mm**2
+P2=(p_x+p_y)*2**-1-(((p_x-p_y)*2**-1)**2+q**2)**0.5 //N/mm**2
+
+//Max shear stress
+q_max1=(((p_x-p_y)*2**-1)**2+q**2)**0.5 //N/mm**2
+
+//At B
+P1_2=(p_x2+p_y)*2**-1+(((p_x2-p_y)*2**-1)**2+q**2)**0.5 //N/mm**2
+P2_2=(p_x2+p_y)*2**-1-(((p_x2-p_y)*2**-1)**2+q**2)**0.5 //N/mm**2
+
+//Max shear stress
+q_max2=(((p_x2-p_y)*2**-1)**2+q**2)**0.5 //N/mm**2
+
+
+//Result
+printf("\n MAx Principal Stresses:P1 %0.2f N/mm**2",P1)
+printf("\n :P2 %0.2f N/mm**2",P2)
+printf("\n Min Principal Stresses:P1_2 %0.2f N/mm**2",P1_2)
+printf("\n :P2_2 %0.2f N/mm**2",P2_2)