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At section A-A, Sy=0 and Txy=0
Sx=(P/A) + ((M1*c)/I)
Tmax = Sx/2
Normal stress Sx = 158.4 MPa
Shear stress Tmax = 79.2 MPa
At section B-B, Sy=0 and Txy=0
Sx=((M1*c)/I)
Normal stress Sx = 194.4 MPa
Shear stress Tmax = 97.2 MPa
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