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CONTINUUM MECHANICS for ENGINEERS

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A most important feature of the field Eqs 6.4-1 through Eq 6.4-3 is that they<br />

are linear in the unknowns. Consequently, if ( 1)<br />

, ( 1)<br />

, and ( 1)<br />

σ are a solution<br />

ij ε ij ui 1 * 1 * <strong>for</strong> body <strong>for</strong>ces bi and surface tractions ti , whereas , , and are<br />

a solution <strong>for</strong> body <strong>for</strong>ces and surface tractions , then<br />

ˆn ( )<br />

( 2)<br />

( 2)<br />

( 2)<br />

σ ij ε ij ui 2 *<br />

2 *<br />

bi<br />

ti<br />

ˆn ( )<br />

( )<br />

( )<br />

( )<br />

σij = + , εij = + , and ui = +<br />

σ 1<br />

ij σ 2<br />

ij ε 1<br />

ij ε 2<br />

1<br />

ij<br />

ui 1 * 2 *<br />

offer a solution <strong>for</strong> the situation where bi = bi + bi and t<br />

( ˆn ) 1 * = + .<br />

i<br />

ti<br />

This is a statement of the principle of superposition, which is extremely useful<br />

<strong>for</strong> the development of solutions in linear elasticity.<br />

For those problems in which the boundary conditions are given in terms<br />

of displacements by Eq 6.4-4, it is convenient <strong>for</strong> us to eliminate the stress<br />

and strain unknowns from the field equations so as to state the problem<br />

solely in terms of the unknown displacement components. Thus, by substituting<br />

Eq 6.4-2 into Hooke’s law (Eq 6.4-3) and that result into the equilibrium<br />

equations (Eq 6.4-1), we obtain the three second-order partial<br />

differential equations<br />

ˆn ( ) 2 *<br />

ti<br />

ˆn ( )<br />

µu i,jj + (λ + µ)u j,ji + ρb i = 0 (6.4-7)<br />

which are known as the Navier equations. If a solution can be determined <strong>for</strong><br />

these equations that also satisfies the boundary condition Eq 6.4-4, that result<br />

may be substituted into Eq 6.4-2 to generate the strains and those in turn<br />

substituted into Eq 6.4-3a to obtain the stresses.<br />

When the boundary conditions are given in terms of surface tractions<br />

(Eq 6.4-5), the equations of compatibility <strong>for</strong> infinitesimal strains (Eq 4.7-32)<br />

may be combined with Hooke’s law (Eq 6.4-3b) and the equilibrium equations<br />

to arrive, after a certain number of algebraic manipulations, at the<br />

equations<br />

1<br />

v<br />

σ + σ + ρ( b + b )+ δ ρb<br />

1+ v<br />

1−v<br />

ij,kk kk,ij i,j j,i ij k,k<br />

= 0 (6.4-8)<br />

which are known as the Beltrami-Michell stress equations of compatibility. In<br />

combination with the equilibrium equations, these equations comprise a<br />

system <strong>for</strong> the solution of the stress components, but it is not an especially<br />

easy system to solve. As was the case with the infinitesimal strain equation<br />

of compatibility, the body must be simply connected.<br />

In elastodynamics, the equilibrium equations must be replaced by the<br />

equations of motion (Eq 5.4-4) in the system of basic field equations. There<strong>for</strong>e,<br />

all field quantities are now considered functions of time as well as of<br />

the coordinates, so that a solution <strong>for</strong> the displacement field, <strong>for</strong> example,<br />

( )<br />

( )<br />

u ( 2)<br />

i

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