Find the deflection of the following points

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A1=8*10-4m2
A2=5*10-4m2
E=70*109Pa
F1=-100*103N
F2=75*103N
F3=50*103N

[tex]\sigma[/tex]=F/A
[tex]\epsilon[/tex]=[tex]\sigma[/tex]/E = [tex]\frac{F}{A*E}[/tex]
[tex]\delta[/tex]=[tex]\epsilon[/tex]*L = [tex]\frac{F*L}{A*E}[/tex]


[tex]\delta[/tex]B = [tex]\frac{F1*1.75}{A1*E}[/tex] + [tex]\frac{F2*3}{A1*E}[/tex] + [tex]\frac{F3*3}{A2*E}[/tex] = 5.1785*10-3m


but that's not right


even looking at the second answer
i thought

[tex]\delta[/tex]D=[tex]\delta[/tex]B + [tex]\frac{F3*1.5}{A2*E}[/tex]
but if i plug in THEIR answer for [tex]\delta[/tex]D i get 2.924mm and not the 5.7 they say
 

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The forces used in the second and third terms of your equation for [tex]\delta_B[/tex] are wrong. You have to take a cut at each point, draw a free body diagram and sum the forces for equilibrium
 
for a similar problem, but where the diameter was constant and the E was different for the 2 parts, i did exactly that and it worked.