Hi I'm trying to understand basic physics but with a more formal scheme. I'm reading P.K.Kundu book of mechanical fluids. In page 90 he proves that stress tensor is symmetric. But first applies torques to a infinitesimal volume element. I cannot understand why the torque in z direction gives that relation, it does not explain term by term, I'm very lost. I understand that $\tau_{ij}$ is force per unit area, the force is applied at center of cube's faces, and that we are interested in the ones that gives angular momenta to the volume element. The first term okay, then why appears again in third term no idea. Second and fourth term maybe are added and subtracted on purpose?. Same last terms. Here an image of the page.
Fluid Dynamics – Understanding Proof of Stress Tensor Symmetry
continuum-mechanicsfluid dynamicsstress-energy-momentum-tensorstress-strainsymmetry
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how on earth.....? A possible way to look at it goes like this, let's consider a little cube length $l$, then the stress force in the $i$th direction acting on $j$th surface element is $-\sigma_{ji}(x_i,x_j,x_k)*dA$ where $dA=l^2$. The force in the $i$th direction acting on the other surface element parallel to the first is $\sigma_{ji}(x_i+dx_i,x_j,x_k)*dA$, so the total stress force acting in the $i$th direction is $$(\sigma_{ji}(x_i+dx_i,x_j,x_k)-\sigma_{ji}(x_i,x_j,x_k))*dA$$ Now divide by the volume element $dV=dx_idx_jdx_k$ and consider $dA=dx_idx_k$ to obtain $$f_i^{(j)}=\frac{\sigma_{ji}(x_i+dx_i,x_j,x_k)-\sigma_{ji}(x_i,x_j,x_k)}{dx_j}=\frac{\partial\sigma_{ji}}{\partial x_j}$$ Then total force per unit volume in the $i$th direction is given by your desired equation
Ok, so figuring that stress is defined to be the force per unit area around a point, I'd like to know why it's defined that way, rather than say force per unit volume enclosing a point.
Here is the intuitive explanation.
Suppose you have a string S from which a weight W is hanging. We will suppose that the amount of weight is so much that the string is near the regime where it would snap, but is not quite there yet. We're going to think about what happens when we add another length of string S.
If you add it in parallel, so there are two strings holding W, then it seems obvious that you could then increase the mass to about 2W before the combined two-string system would be near-breaking.
By contrast, if you add it in series (W hangs from S hanging from S), then we know that the tension force is the same in both strings, and it seems likely that they'd simply both be near-breaking. The top string might even break, if the weight of the string underneath it is enough to put it past breaking.
This tells us that the material properties which concern us (like when a string breaks) respond to stresses, defined as forces divided by an area perpendicular to that force. The direction that lies alongside the force doesn't matter, qualitatively because it propagates the force rather than responding to it.
You can also examine this two-string thought-experiment with much smaller forces not near breaking, where Hooke's law should hold for lengthening, to find that if the original deforms by $\delta L = \ell$, the two-strings-in-parallel should deform by $\ell/2$ while the two-strings-in-series should deform by $2\ell,$ so that there seems to be a constant "stress / strain" relationship where the "strain" is defined as $\delta L / L.$ In other words you can look at a system with the normal spring-constant $F = k ~ \delta L$ relationship, but it is more helpful from a materials perspective to divide by the length of the "spring" $L$ and also its cross-sectional area $A$ to find $$\sigma = \frac FA = \frac {kL}{A} ~ \frac{\delta L}{L} = \lambda ~ \epsilon.$$ The elastic modulus $\lambda$ then also has units of pressure (force per unit area) and is more fundamental to the material (a material-property) that you're studying than the spring constant (a property of both the material and the setup) is.
Since the elastic modulus is a material-property, this hints that "stress" is the right definition of "force" and "strain" is the right definition of "displacement" at the more-microscopic level when we're peeking inside the substance.
In turn, it becomes very common in materials science to show the "stress/strain" curve of various materials. This starts out of course as a straight line through the origin with slope $\lambda$, but then as a substance deforms it will describe some sort of curve as added stress leads to further strain. So for example the plastic bags from the supermarket will curve upwards; they get stiffer as they stretch more.
Once you know that the stress is the right way to "microscopically" define force, elastic systems start to show off a similar problem: the simplest stretching of a beam consists in that beam not only lengthening but also narrowing. Microscopically, a little box inside the substance is not only feeling a force $+\sigma~dA$ on one side and a force $-\sigma~dA$ on the other side (so it is in force balance and provides tension), but it must also be feeling some forces on its other sides which "pinch" it smaller. So: the force is direction-dependent, and we therefore have not a stress vector (which we already didn't quite have -- the stress is in opposite directions on the top and bottom of the box), but a stress tensor: give me a direction and I'll give you the stress vector on a plane normal to that direction. (This also solves nicely the "stress on the top of the box is negative the stress on the bottom of the box" problem.)
Usually this simplifies a lot because there are eigenvectors of the stress tensor: directions where the stress points exactly normal to the plane it deforms. Those are called the "principal stresses". However there is no reason why they'd have to be orthogonal, especially, for example, in a crystal lattice which is not cubic.
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(Why show text that refers to Fig. 4.6 and then show only Fig. 4.5?)
I don't like this presentation. The stresses are shown to act on the faces in Fig. 4.5, but in Fig. 4.6, they're clearly considered to act on the cube center, since the stresses are essentially Taylor expanded to $$\tau(\text{edge})=\tau(\text{center})+\frac{\partial\tau}{\partial (\text{distance})}(\text{center–edge distance, or half the side length}),$$
or
$$\tau=\tau_{12}+\frac{\partial\tau_{12}}{\partial x_i}\frac{dx_1}{2}$$
in one example. OK, so call that the stress on the surface with normal unit vector $+x_1$. Hopefully it's then clear that the corresponding force is $\tau dx_2dx_3=\tau dx_2$ (because $dx_3$ is taken as 1), and then the moment arm is $\frac{x_1}{2}$, so that particular torque component is
$$\left(\tau_{12}+\frac{\partial\tau_{12}}{\partial x_i}\frac{dx_1}{2}\right)dx_2\frac{dx_1}{2}.$$
There's the first term.
But then the authors write $\tau_{12}$ on the opposite face, which should strictly be $\tau_{(-1)2}$ according to their indicial convention (with the arrow pointing toward $+x_2$), but then seem to assume implicitly that $\tau_{(-1)2}=\tau_{1(-2)}$ so that they can flip the arrow to obtain the label $\tau_{12}$. Maybe I'm missing something, but that seems to assume symmetry already.
All this is underexplained in the main text, as you note. But if you accept the indicial flip-flops, then the rest of the terms are straightforward, as the Taylor expansion when moving in the $-x_1$ direction to the plane pointing with normal unit vector $-x_2$ should be
$$\tau=\tau_{12}-\frac{\partial\tau_{12}}{\partial x_i}\frac{dx_1}{2},$$
for example.