Need help with multi-segment deflection problem

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SUMMARY

The discussion focuses on solving a multi-segment deflection problem for a uniform beam of 4.8m, supported by a pin at x = 0 and a roller at x = 3.2m. The beam experiences a distributed load of 12kN/m from x = 0 to x = 1.6m and a concentrated force of 2.4kN at x = 4.8m. The moment equations derived for each segment are M1 = 13.2x - 6x^2, M2 = -6x + 15.36, and M3 = 2.4x - 11.52. The user correctly identifies the need for boundary conditions to determine the coefficients of integration for the deflection equations, ultimately concluding that V' is 0 at x = 1.1, which aids in finding the remaining coefficients.

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Homework Statement


There is a uniform, horizontal beam 4.8m in length supported by a pin at x = 0 and a roller at x= 3.2m. There is a distributed weight of 12kN/m from x = 0 to x = 1.6m. There is a concentrated, vertical force of 2.4kN in the downward direction at x = 4.8.
Find the deflection and define the coefficients of integration for each segment

Homework Equations


EIY'' = double integral of Mdx
Y is deflection

The Attempt at a Solution


I calculated the moment for each segment, but I can't seem to figure out what the coefficients are. I think I'm supposed to use symmetry conditions, and I know the deflection is 0 at x = 0 and x = 3.2 where there are supports. I can't figure out past that though.

M1 = 13.2x - 6x^2
M2 = -6x + 15.36
M3 = 2.4x - 11.52

EIV1 = 2.2x^3 - .5x^5 + C1x + C2
C2 = 0

EIV2 = -x^3 + 7.68x^2 + C1x + C2

EIV3 = .4x^3 - 5.76x^2 + C1x + C2

I believe the moments I calculated are correct, but I'm not sure. Any help would be appreciated.
 
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Oh, I think I figured it out. V' is 0 at x = 1.1, from there I can find the rest of the coefficients
 

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