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9.2 Flexure from a point load               289

            where it is written as the sum of the deflection from the weight of the beam and the deflec-
            tion from the end load. The solution can be used to find the maximum deflection at the free
            end, which is
                                      w(ˆ=1) = 3w 1 + 2w 2 ,                   (9.29)
                                         x
            where the maximum deflection due to the weight of the beam is 3w 1 and the maximum
            deflection due to the end load is 2w 2 .
              The surface load becomes q 0 = W 0 g/l when the beam has the weight W 0 , and the end
            load becomes F 0 = W b g when it is due to a weight W b . It is then seen that the weight of
            the beam and the end load contribute equally to the deflection when the beam has 3/8of
            the weight of the end load.
              The force F 0 can also be represented as a load per unit length by use of the Dirac delta
            function δ(x) as F 0 δ(x − l), which makes the total surface load per unit length q(x) =
            q 0 + F 0 δ(x − l). The Dirac delta function is defined by the integral

                                     ∞




                                       f (x )δ(x − x ) dx = f (x)              (9.30)
                                    −∞
            and it is seen to be zero everywhere, except at x = 0 where it is infinite.
                                   9.2 Flexure from a point load
            The flexure of a 2D elastic plate under a point load has a solution that turns out to be
            simple and useful. It is useful because any load q(x) can be discretized into a series
            of discrete point loads, and the flexure from the full load q(x) can then be approxi-
            mated by superposition of the solutions for the discrete point loads (see Note 9.3). A
            point load in 2D is actually a line load in 3D because it extends along a line (normal
            to the cross-section) through the point where it is applied. The point load V 0 is placed
            at x = 0 and it is assumed that the plate is unaffected at large distances away from the
            load, which gives w = 0for x →±∞. Equation (9.14) for the deflection of the plate
            becomes
                                          4
                                         d w
                                       D     +   gw = 0                        (9.31)
                                         dx 4
            where    =   m −   c , because the load is zero everywhere except at x = 0. It is a
            fourth-order equation and we therefore need four boundary conditions. We already have
            two and the third follows from symmetry around x = 0, which implies that dw/dx = 0
            for x = 0. The fourth condition, which involves the point load, is the force balance in the
            vertical direction. The load on the plate must be balanced by the buoyancy of the displaced
            mantle, which is written as

                                        ∞                ∞

                              V 0
                                 +   c g  w(x)dx =   m g   w(x)dx.             (9.32)
                              2        0                0
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