Missing Diagram is attached.
Answer:
a) 21.43 MPa
b) -14.2 MPa
Step-by-step explanation:
Given:







Calculating the stresses:

= 41.667 MPa

= 20.833 MPa

-9.325 MPa
For stress along x axis:
Tx = Tl - Ta
= 20.83 - 9.325
= 11.5 MPa

= 26.58 MPa

= -15.08 MPa
Mohr's circle angle = 2∅
= 2 * 35°
= 70°
a) for normal stress perpendicular to weld, we have:
Tx' = Tavg + Tmax (cos70°}
= 26.590 - 15.08(cos70°)
= 21.43 MPa
b) shearing stress parallel to weld:
= Tmax (sin70°}
= -15.08 sin70°
= -14.2 MPa