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Cauchy's formula and equilibrium equations

Short answer

Traction on a plane with normal (l,m,n) is t_i = σ_ij n_j, derived from force equilibrium of a tetrahedron. Equilibrium equations: ∂σ_x/∂x + ∂τ_xy/∂y + ∂τ_xz/∂z + X = 0, and similarly for y and z; τ_ij = τ_ji.

Derive Cauchy's formula relating the traction on an arbitrary plane to the stress tensor, using an elemental tetrahedron. State the equilibrium equations for a deformable body in terms of stress components.

Cauchy's formula

Take a tetrahedron at a point with three faces on the coordinate planes and a fourth inclined face of area dAdA and unit normal n=(l,m,n)\mathbf{n} = (l, m, n) (direction cosines). The coordinate-plane faces then have areas

dAx=l dA,dAy=m dA,dAz=n dAdA_x = l\,dA,\quad dA_y = m\,dA,\quad dA_z = n\,dA

Let t=(tx,ty,tz)\mathbf{t} = (t_x, t_y, t_z) be the traction (stress vector) on the inclined face. The faces on the coordinate planes have outward normals along −x,−y,−z-x, -y, -z, so their stresses act opposite to the positive components.

        z
        |  C
        | /|\
        |/ | \
        A--+--B  (inclined face ABC)
       /  O
      y       x

Force equilibrium in the x-direction (body force and inertia are of higher order, since volume ∝h3\propto h^3 while area ∝h2\propto h^2 as the tetrahedron shrinks):

tx dA−σx(l dA)−τyx(m dA)−τzx(n dA)=0tx=σxl+τyxm+τzxn\begin{aligned} t_x\, dA - \sigma_x (l\,dA) - \tau_{yx}(m\,dA) - \tau_{zx}(n\,dA) &= 0 \\ t_x &= \sigma_x l + \tau_{yx} m + \tau_{zx} n \end{aligned}

Similarly for yy and zz. In matrix form (symmetric tensor):

{txtytz}=[σxτxyτxzτxyσyτyzτxzτyzσz]{lmn}\begin{Bmatrix} t_x \\ t_y \\ t_z \end{Bmatrix} = \begin{bmatrix} \sigma_x & \tau_{xy} & \tau_{xz} \\ \tau_{xy} & \sigma_y & \tau_{yz} \\ \tau_{xz} & \tau_{yz} & \sigma_z \end{bmatrix} \begin{Bmatrix} l \\ m \\ n \end{Bmatrix}

or ti=σijnjt_i = \sigma_{ij} n_j. The normal and shear stress on the plane are then

σn=t⋅n,τ=∣t∣2−σn2\sigma_n = \mathbf{t}\cdot\mathbf{n},\qquad \tau = \sqrt{|\mathbf{t}|^2 - \sigma_n^2}

So the six components of σij\sigma_{ij} determine the traction on every plane through the point.

Equilibrium equations

For a body force per unit volume (X,Y,Z)(X, Y, Z):

∂σx∂x+∂τxy∂y+∂τxz∂z+X=0∂τxy∂x+∂σy∂y+∂τyz∂z+Y=0∂τxz∂x+∂τyz∂y+∂σz∂z+Z=0\begin{aligned} \frac{\partial \sigma_x}{\partial x} + \frac{\partial \tau_{xy}}{\partial y} + \frac{\partial \tau_{xz}}{\partial z} + X &= 0 \\ \frac{\partial \tau_{xy}}{\partial x} + \frac{\partial \sigma_y}{\partial y} + \frac{\partial \tau_{yz}}{\partial z} + Y &= 0 \\ \frac{\partial \tau_{xz}}{\partial x} + \frac{\partial \tau_{yz}}{\partial y} + \frac{\partial \sigma_z}{\partial z} + Z &= 0 \end{aligned}

Moment equilibrium gives the symmetry τij=τji\tau_{ij}=\tau_{ji}. At the boundary, the traction must satisfy ti=σijnjt_i = \sigma_{ij}n_j equal to the applied surface load.

✓ Answer checked by Claude Sonnet 5.5

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