What Are the Normal and Shear Stresses on the Inclined Butt Weld?

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The discussion focuses on calculating the normal and shear stresses on an inclined butt weld subjected to tensile stresses in both x and y directions, with given values of σ(x) = 54 N/mm² and σ(y) = 38 N/mm². The transformation matrices are employed to analyze the stresses, where τxy is initially set to zero due to the absence of applied torque in the first part of the calculation. The maximum normal stress direction is determined by evaluating the stress tensor and using the unit normal to the weld. The normal and shear stress equations are derived, highlighting the dependence on the angle β. Understanding these calculations is crucial for evaluating weld integrity under varying stress conditions.
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Homework Statement
Calcul of stresses
Relevant Equations
1- σ'x=σx*cos(β)^2+σy*sin(β)^2+2*τxy*cos(β)*sin(β)

2- σ'y=σx*sin(β)^2+σy*cos(β)^2-2*τxy*cos(β)*sin(β)

3- τxy'=-σx*sin(β)*cos(β)+σy*sin(β)*cos(β)+τxy*(cos(β)^2-sin(β)^2)
Hi! i have this exercise and solution :

Exercise:
steel plate given in figure (a) is joined by an inclined butt weld ,the plate is subjected to tensile stresses in both x and y directions, σ(x)=54 N/mm^2 and σ(y)=38 N/mm^2 ,
1) Determine the normal and shear stresses of the butt weld.
1.PNG


this is transformation matrices :
2.PNG


2)second question :
in which direction the stress normal will be maximum ?

3.PNG


My problem: is τxy ( why in first we made it 0 in transformation matrice (and why it's 0) and in second question it's calculed .
 
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As far as I can make out, the first part is a calculation for a special case where there is no applied torque, whereas the second finds the weld direction that maximises stress in the more general case.
 
In this system, the stress tensor is given by$$\boldsymbol{\sigma}=\sigma_x\mathbf{i_x}\mathbf{i_x}+\sigma_y\mathbf{i_y}\mathbf{i_y}$$and the unit normal to the weld is given by: $$\mathbf{n}=\sin{\beta}\mathbf{i_x}+\cos{\beta}\mathbf{i_x}$$So the traction vector on the weld is given by: $$\boldsymbol{T}=\boldsymbol{\sigma}\centerdot \mathbf{n}=\sigma_x \sin{\beta}\mathbf{i_x}+\sigma_y \cos{\beta}\mathbf{i_y}$$The normal component of the traction vector on the weld is equal to the traction vector dotted with the unit normal: $$\sigma_n=\boldsymbol{T}\centerdot \mathbf{n}=\sigma_x \sin^2{\beta}+\sigma_y\cos^2{\beta}=\frac{(\sigma_x+\sigma_y)}{2}-\frac{(\sigma_x-\sigma_y)}{2}\cos{2\beta}$$The unit tangent vector to the weld is given by $$\mathbf{t}=\cos{\beta}\mathbf{i_x}-\sin{\beta}\mathbf{i_y}$$The shear component of the traction is obtained by dotting the traction vector with the unit tangent:$$\tau=(\sigma_x-\sigma_y)\sin{\beta}\cos{\beta}=\frac{(\sigma_x-\sigma_y)}{2}\sin{2\beta}$$
 
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