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SolMech
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Homework Statement
A beam supported at two locations is subjected to two equal loads at the end points
Compute the central deflection W.
Schematic:
[itex]\downarrow[/itex]........[itex]\downarrow[/itex]
____________________________
<--->Δ<-------><------->Δ<--->
...a...L...L...a
The delta's are the supports the arrows the forces F and a & L distances
Homework Equations
M(x) = E*I*W"(X)
The Attempt at a Solution
At first I try to formulate the momentum along the beam. x = 0 at the center of the beam.
I thought it would be zero at the points where the Forces are, and maximum at the center.
So I came up with:
M(x) = F(1+[itex]\frac{x}{a+L}[/itex])*(a+L) with x left from the center and
M(x) = F(1-[itex]\frac{x}{a+L}[/itex])*(a+L) with x right from the center.
w" = EI/M(x)
Integrating this twice should yield the result:
w'(x) = [itex]\frac{F}{2EI}[/itex]x[itex]^{2}[/itex] + [itex]\frac{F}{EI}[/itex](a+L)x + C
But w'(0) = 0 so C = 0
integrating once more gives:
w(x) = [itex]\frac{F}{6EI}[/itex]x[itex]^{3}[/itex] + [itex]\frac{F}{EI}[/itex](a+L)x[itex]^{2}[/itex] + C
solving for C with w(L)=0 gives: C = - [itex]\frac{FL^{2}}{EI}[/itex]([itex]\frac{a}{2}[/itex]+[itex]\frac{2L}{3}[/itex])
which therefore should be the max deflection, because at x=0 deflection is max and w(0) = C
The problem is I have no way to check my result, and I'm not quite sure of the result. Could someone check me and explain me where I went wrong (if so)