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In 1885 the French scientist Boussinesq obtained a solution for the stresses and strains in a homogeneous isotropic linear elastic half space, loaded by a vertical point force on the sur

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In 1885 the French scientist Boussinesq obtained a solution for the stresses and strains in a homogeneous isotropic linear elastic half space, loaded by a vertical point force on the surface, see Figure 28.1 A derivation of this solution is given in Appendix B, see also any textbook

.

.

.

.

.

. .

. .

. .

..

.

.

.

x

y

z

P

R σzz σrr σθθ

Figure 28.1: Point load on half space.

on the theory of elasticity (for instance S.P Timoshenko, Theory

of Elasticity, paragraph 123) The stresses are found to be

1 − 2ν

In these equations r is the cylindrical coordinate,

and R is the spherical coordinate,

The solution for the displacements is

160

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The vertical displacement of the surface is particularly interesting This is

For R → 0 this tends to infinity At the point of application of the point load the displacement is infinitely large This singular behavior is

a consequence of the singularity in the surface load, as in the origin the stress is infinitely large That the displacement in that point is also infinitely large may not be so surprising.

Another interesting quantity is the distribution of the stresses as a function of depth, just below the point load, i.e for r = 0 This is found

to be

These stresses decrease with depth, of course In engineering practice, it is sometimes assumed, as a first approximation, that at a certain depth

. . .

.

.

.

.

.

.

r

z P

Figure 28.2: Vertical normal stress σzz.

the stresses are spread over an area that can be found by drawing a line

a circle of radius z That appears to be incorrect (the error is 50 % if

r = 0), but the trend is correct, as the stresses indeed decrease with

represented as a function of the cylindrical coordinate r, for two values

of the depth z.

The assumption of linear elastic material behavior means that the en-tire problem is linear, as the equations of equilibrium and compatibility are also linear This implies that the principle of superposition of solu-tions can be applied Boussinesq’s solution can be used as the starting point of more general types of loading, such as a system of point loads,

or a uniform load over a certain given area.

As an example consider the case of a uniform load of magnitude p over a circular area, of radius a The solution for this case can be found by integration over a circular area (S.P Timoshenko, Theory of Elasticity, paragraph 124), see Figure 28.3.

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.

. .

r z p Figure 28.3: Uniform load over circular area The stresses along the axis r = 0, i.e just below the load, are found to be r = 0 : σzz = p(1 − z 3 b 3 ), (28.13) r = 0 : σrr = p[(1 + ν) z b − 1 2 (1 − z 3 b 3 )], (28.14) in which b = √ z 2 + a 2 The displacement of the origin is r = 0, z = 0 : uz = 2(1 − ν 2 ) pa E . (28.15) This solution will be used as the basis of a more general case in the next chapter Another important problem, which was already solved by Boussinesq (see also Timoshenko) is the problem of a half space loaded by a vertical force on a rigid plate The force is represented by P = πa 2 p, see Figure 28.4 The distribution of the normal stresses below the plate is found .

.

.

. .

r

z P

Figure 28.4: Rigid plate on half space.

to be

1

This stress distribution is shown in Figure 28.4 At the edge of the plate the stresses are infinitely large, as a consequence of the constant displacement of the rigid plate In reality the material near the edge of the plate will probably deform plastically It can be expected, however, that the real distribution of the stresses below the plate will be of the form shown in the figure, with the largest stresses near the edge The center of the plate will subside without much load.

The displacement of the plate is

When this is compared with the displacement below a uniform load, see (28.15), it appears that the displacement of the rigid plate is somewhat smaller, as could be expected.

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28.1 A circular area is loaded by a uniform vertical load p The stress distribution is approximated by assuming that the vertical normal stress at a depth

z is uniform, over an area πz2 Sketch the distribution of the stresses just below the load, as a function of depth, and compare the result with the exact solution (28.13).

28.2 From the expression of the previous problem, and using the relations ε = σ/E and ε = ∂uz/∂z, derive an expression for the displacement of the surface, and compare the result with eq (28.15).

28.3 In engineering practice the displacement due to a loaded plate is often expressed by a subgrade constant, by writing uz = p/c Derive a relation between the subgrade constant c and the elastic modulus E.

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