Stress functions

It can be shown [1] that a complete solution to the equilibrium equations may be written as

${\displaystyle \sigma =\nabla \times \Phi \times \nabla }$

Using index notation:

${\displaystyle \sigma _{ij}=\varepsilon _{ikm}\varepsilon _{jln}\Phi _{kl,mn}}$

Engineering notation
${\displaystyle \sigma _{x}={\frac {\partial ^{2}\Phi _{yy}}{\partial z\partial z}}+{\frac {\partial ^{2}\Phi _{zz}}{\partial y\partial y}}-2{\frac {\partial ^{2}\Phi _{yz}}{\partial y\partial z}}}$		${\displaystyle \sigma _{xy}=-{\frac {\partial ^{2}\Phi _{xy}}{\partial z\partial z}}-{\frac {\partial ^{2}\Phi _{zz}}{\partial x\partial y}}+{\frac {\partial ^{2}\Phi _{yz}}{\partial x\partial z}}+{\frac {\partial ^{2}\Phi _{zx}}{\partial y\partial z}}}$
${\displaystyle \sigma _{y}={\frac {\partial ^{2}\Phi _{xx}}{\partial z\partial z}}+{\frac {\partial ^{2}\Phi _{zz}}{\partial x\partial x}}-2{\frac {\partial ^{2}\Phi _{zx}}{\partial z\partial x}}}$		${\displaystyle \sigma _{yz}=-{\frac {\partial ^{2}\Phi _{yz}}{\partial x\partial x}}-{\frac {\partial ^{2}\Phi _{xx}}{\partial y\partial z}}+{\frac {\partial ^{2}\Phi _{zx}}{\partial y\partial x}}+{\frac {\partial ^{2}\Phi _{xy}}{\partial z\partial x}}}$
${\displaystyle \sigma _{z}={\frac {\partial ^{2}\Phi _{yy}}{\partial x\partial x}}+{\frac {\partial ^{2}\Phi _{xx}}{\partial y\partial y}}-2{\frac {\partial ^{2}\Phi _{xy}}{\partial x\partial y}}}$		${\displaystyle \sigma _{zx}=-{\frac {\partial ^{2}\Phi _{zx}}{\partial y\partial y}}-{\frac {\partial ^{2}\Phi _{yy}}{\partial z\partial x}}+{\frac {\partial ^{2}\Phi _{xy}}{\partial z\partial y}}+{\frac {\partial ^{2}\Phi _{yz}}{\partial x\partial y}}}$

where ${\displaystyle \Phi _{mn}}$ is an arbitrary second-rank tensor field that is at least twice differentiable, and is known as the Beltrami stress tensor.[1] Its components are known as Beltrami stress functions. ${\displaystyle \varepsilon }$ is the Levi-Civita pseudotensor, with all values equal to zero except those in which the indices are not repeated. For a set of non-repeating indices the component value will be +1 for even permutations of the indices, and -1 for odd permutations. And ${\displaystyle \nabla }$ is the Nabla operator. For the Beltrami stress tensor to satisfy the Beltrami-Michell compatibility equations in addition to the equilibrium equations, it is further required that ${\displaystyle \Phi _{mn}}$ is at least four times continuously differentiable.

The Maxwell stress functions are defined by assuming that the Beltrami stress tensor ${\displaystyle \Phi _{mn}}$ is restricted to be of the form.[2]

${\displaystyle \Phi _{ij}={\begin{bmatrix}A&0&0\\0&B&0\\0&0&C\end{bmatrix}}}$

The stress tensor which automatically obeys the equilibrium equation may now be written as:[2]

${\displaystyle \sigma _{x}={\frac {\partial ^{2}B}{\partial z^{2}}}+{\frac {\partial ^{2}C}{\partial y^{2}}}}$		${\displaystyle \sigma _{yz}=-{\frac {\partial ^{2}A}{\partial y\partial z}}}$
${\displaystyle \sigma _{y}={\frac {\partial ^{2}C}{\partial x^{2}}}+{\frac {\partial ^{2}A}{\partial z^{2}}}}$		${\displaystyle \sigma _{zx}=-{\frac {\partial ^{2}B}{\partial z\partial x}}}$
${\displaystyle \sigma _{z}={\frac {\partial ^{2}A}{\partial y^{2}}}+{\frac {\partial ^{2}B}{\partial x^{2}}}}$		${\displaystyle \sigma _{xy}=-{\frac {\partial ^{2}C}{\partial x\partial y}}}$

The solution to the elastostatic problem now consists of finding the three stress functions which give a stress tensor which obeys the Beltrami–Michell compatibility equations for stress. Substituting the expressions for the stress into the Beltrami–Michell equations yields the expression of the elastostatic problem in terms of the stress functions:[3]

${\displaystyle \nabla ^{4}A+\nabla ^{4}B+\nabla ^{4}C=3\left({\frac {\partial ^{2}A}{\partial x^{2}}}+{\frac {\partial ^{2}B}{\partial y^{2}}}+{\frac {\partial ^{2}C}{\partial z^{2}}}\right)/(2-\nu ),}$

These must also yield a stress tensor which obeys the specified boundary conditions.

The Airy stress function is a special case of the Maxwell stress functions, in which it is assumed that A=B=0 and C is a function of x and y only.[2] This stress function can therefore be used only for two-dimensional problems. In the elasticity literature, the stress function ${\displaystyle C}$ is usually represented by ${\displaystyle \varphi }$ and the stresses are expressed as

${\displaystyle \sigma _{x}={\frac {\partial ^{2}\varphi }{\partial y^{2}}}~;~~\sigma _{y}={\frac {\partial ^{2}\varphi }{\partial x^{2}}}~;~~\sigma _{xy}=-{\frac {\partial ^{2}\varphi }{\partial x\partial y}}-(f_{x}y+f_{y}x)}$

Where ${\displaystyle f_{x}}$ and ${\displaystyle f_{y}}$ are values of body forces in relevant direction.

In polar coordinates the expressions are:

${\displaystyle \sigma _{rr}={\frac {1}{r}}{\frac {\partial \varphi }{\partial r}}+{\frac {1}{r^{2}}}{\frac {\partial ^{2}\varphi }{\partial \theta ^{2}}}~;~~\sigma _{\theta \theta }={\frac {\partial ^{2}\varphi }{\partial r^{2}}}~;~~\sigma _{r\theta }=\sigma _{\theta r}=-{\frac {\partial }{\partial r}}\left({\frac {1}{r}}{\frac {\partial \varphi }{\partial \theta }}\right)}$

The Morera stress functions are defined by assuming that the Beltrami stress tensor ${\displaystyle \Phi _{mn}}$ tensor is restricted to be of the form [2]

${\displaystyle \Phi _{ij}={\begin{bmatrix}0&C&B\\C&0&A\\B&A&0\end{bmatrix}}}$

The solution to the elastostatic problem now consists of finding the three stress functions which give a stress tensor which obeys the Beltrami-Michell compatibility equations. Substituting the expressions for the stress into the Beltrami-Michell equations yields the expression of the elastostatic problem in terms of the stress functions:[4]

${\displaystyle \sigma _{x}=-2{\frac {\partial ^{2}A}{\partial y\partial z}}}$		${\displaystyle \sigma _{yz}=-{\frac {\partial ^{2}A}{\partial x^{2}}}+{\frac {\partial ^{2}B}{\partial y\partial x}}+{\frac {\partial ^{2}C}{\partial z\partial x}}}$
${\displaystyle \sigma _{y}=-2{\frac {\partial ^{2}B}{\partial z\partial x}}}$		${\displaystyle \sigma _{zx}=-{\frac {\partial ^{2}B}{\partial y^{2}}}+{\frac {\partial ^{2}C}{\partial z\partial y}}+{\frac {\partial ^{2}A}{\partial x\partial y}}}$
${\displaystyle \sigma _{z}=-2{\frac {\partial ^{2}C}{\partial x\partial y}}}$		${\displaystyle \sigma _{xy}=-{\frac {\partial ^{2}C}{\partial z^{2}}}+{\frac {\partial ^{2}A}{\partial x\partial z}}+{\frac {\partial ^{2}B}{\partial y\partial z}}}$

The Prandtl stress function is a special case of the Morera stress functions, in which it is assumed that A=B=0 and C is a function of x and y only.[4]

• Sadd, Martin H. (2005). Elasticity - Theory, applications and numerics. New York: Elsevier Butterworth-Heinemann. ISBN 0-12-605811-3. OCLC 162576656.
• Knops, R. J. (1958). "On the Variation of Poisson's Ratio in the Solution of Elastic Problems". The Quarterly Journal of Mechanics and Applied Mathematics. Oxford University Press. 11 (3): 326–350. doi:10.1093/qjmam/11.3.326.

• Elasticity (physics)
• Elastic modulus
• Infinitesimal strain theory
• Linear elasticity
• Solid mechanics
• Stress (mechanics)