I'm going to present the approach that I have found simple and easy to understand and apply, and am sure that you will too. But, before I do, I'd just like to answer a couple of your questions.
fog37 said:
So, in physics problems, is it correct to talk about the tension force or is it better to talk about the force produced by the tension (which is a component of the stress tensor)?
In my expert judgment (based on my PhD training in material science and many years of practical experience), it is unquestionably better fundamentally to talk about it in relation to the stress tensor.
As far as the Cauchy's theorem, I think it relates the stress tensor to the strain tensor... Does stress cause strain or vice versa? I don't think there is a cause-effect relation...
No. Cauchy's relationship is not related to the strain tensor at all. It establishes the relationship between the stress tensor and the traction vector (also sometimes referred to as the stress vector) on a plane of specified arbitrary orientation within a material.
VECTORS (FIRST ORDER TENSORS) AND SECOND ORDER TENSORS
Using 3D Cartesian coordinates, we can express a vector (AKA a first order tensor) as a summation of three terms, involving 3 components (and three unit vectors) as follows: $$\mathbf{v}=v_x\mathbf{i_x}+v_y\mathbf{i_y}+v_z\mathbf{i_z}$$
By analogy, we can express a 2nd order tensor as a summation of 9 terms, involving 9 components as follows:
$$\mathbf{T}=T_{xx}\mathbf{i_x}\mathbf{i_x}+T_{xy}\mathbf{i_x}\mathbf{i_y}+T_{xz}\mathbf{i_x}\mathbf{i_z}+T_{yx}\mathbf{i_y}\mathbf{i_x}+T_{yy}\mathbf{i_y}\mathbf{i_y}+T_{yz}\mathbf{i_y}\mathbf{i_z}+T_{zx}\mathbf{i_z}\mathbf{i_x}+T_{zy}\mathbf{i_z}\mathbf{i_y}+T_{zz}\mathbf{i_z}\mathbf{i_z}$$
You will notice in this summation that there are pairs of unit vectors (e.g. ##\mathbf{i_x}\mathbf{i_y}##) placed right next to one another (i.e., in juxtaposition) with no mathematical operation (such as the dot product or the cross product) implied between them.
Such a juxtaposition of vectors is called a dyadic, and, more generally, a dyadic can be formed in terms of any two arbitrary vectors ##\mathbf{v_1}## and ##\mathbf{v_2}## as ##\mathbf{v_1}\mathbf{v_2}##. A dyadic of two vectors has no special physical significance until it fulfills its main mission in life, which is getting dotted with another vector according to the following rule:$$(\mathbf{v_1}\mathbf{v_2})\centerdot \mathbf{v_3}=\mathbf{v_1}(\mathbf{v_2}\centerdot \mathbf{v_3})$$This equation says that dotting the vector ##\mathbf{v_3}## with the dyadic ##\mathbf{v_1}\mathbf{v_2}## maps ##\mathbf{v_3}## into a new vector what has the same direction as ##\mathbf{v_1}##, and with a new magnitude.
It is also possible to dot a dyadic by a vector in front of it by writing:$$\mathbf{v_3} \centerdot(\mathbf{v_1}\mathbf{v_2})=(\mathbf{v_3} \centerdot \mathbf{v_1})\mathbf{v_2}$$In this case, the equation says that dotting the vector ##\mathbf{v_3}## in front with the dyadic ##\mathbf{v_1}\mathbf{v_2}## maps ##\mathbf{v_3}## into a new vector what has the same direction as ##\mathbf{v_2}##, and with a new magnitude.
STRESSES, TENSIONS, AND PRESSURES
Now the big question is how all this dyadic stuff relates to the stresses and tensions within materials. Well, first of all, we can represent the stress tensor in a material in terms of this notation simply by writing:
$$\boldsymbol{\sigma}=\sigma_{xx}\mathbf{i_x}\mathbf{i_x}+\sigma_{xy}\mathbf{i_x}\mathbf{i_y}+\sigma_{xz}\mathbf{i_x}\mathbf{i_z}+\sigma_{yx}\mathbf{i_y}\mathbf{i_x}+\sigma_{yy}\mathbf{i_y}\mathbf{i_y}+\sigma_{yz}\mathbf{i_y}\mathbf{i_z}+\sigma_{zx}\mathbf{i_z}\mathbf{i_x}+\sigma_{zy}\mathbf{i_z}\mathbf{i_y}+\sigma_{zz}\mathbf{i_z}\mathbf{i_z}$$
Secondly, Cauchy showed that we can calculate the "traction" vector ##\boldsymbol {\tau}## (force vector per unit area aka stress vector) on a differential surface of arbitrary orientation within a material simply by dotting the stress tensor ##\boldsymbol{\sigma}## with a unit normal vector ##\mathbf{n}## to the surface:
$$\boldsymbol{\tau}=\boldsymbol{\sigma}\centerdot \mathbf{n}$$with ##\mathbf{n}=n_x\mathbf{i_x}+n_y\mathbf{i_y}+n_z\mathbf{i_z}##
Now, if we apply our dyadic multiplication rule with this equation, we obtain:
$$\boldsymbol{\tau}=\boldsymbol{\sigma}\centerdot \mathbf{n}=(\sigma_{xx}n_x+\sigma_{xy}n_y+\sigma_{xz}n_z)\mathbf{i_x}+(\sigma_{yx}n_x+\sigma_{yy}n_y+\sigma_{yz}n_z)\mathbf{i_y}+(\sigma_{zx}n_x+\sigma_{zy}n_y+\sigma_{zz}n_z)\mathbf{i_z}$$
Note that the traction vector on the surface can be resolved into components both normal and tangent to the surface. Therefore, in general, there will be both a normal stress on any surface and a tangential (shear) stress on the surface. Only for special orientation of the surface is the shear stress zero.
APPLICATION TO TENSION IN ROPES AND PRESSURES IN FLUIDS
For a rope or a rod under uniaxial tension load, the stress tensor reduces simply to: $$\boldsymbol{\sigma}=\frac{T}{A}\mathbf{i_x}\mathbf{i_x}$$where T is the tension and A is the cross sectional area. If we dot this with a unit vector perpendicular to the rope cross section, in the positive x direction ##\mathbf{n}=\mathbf{i_x}##, we have $$\boldsymbol{\tau}=\boldsymbol{\sigma}\centerdot \mathbf{n}=\frac{T}{A}\mathbf{i_x}$$This is the stress vector on the surface exerted by the material to the right of the surface on the material to the left of the surface. The tension force exerted by the material to the right on the material to the left is obtained simply by multiplying by the cross sectional area A.
If we want to determine stress vector on the cross section exerted by the material to the left on the material to the right, we simply dot the stress tensor by the normal unit vector in the negative x direction: $$\boldsymbol{\tau}=\boldsymbol{\sigma}\centerdot \mathbf{n}=\frac{T}{A}\mathbf{i_x}\mathbf{i_x}\centerdot (-\mathbf{i_x})=-\frac{T}{A}\mathbf{i_x}$$
In the case of hydrostatic pressure in a fluid, the (tensile) stress tensor is "isotropic," and can be expressed as:
$$\boldsymbol{\sigma}=-p\mathbf{i_x}\mathbf{i_x}-p\mathbf{i_y}\mathbf{i_y}-p\mathbf{i_z}\mathbf{i_z}$$where p is the pressure. If we dot this stress tensor with a unit normal vector in any arbitrary direction, we obtain
$$\boldsymbol{\tau}=\boldsymbol{\sigma}\centerdot \mathbf{n}=-p(n_x\mathbf{i_x}+n_y\mathbf{i_y}+n_z\mathbf{i_z})=-p\mathbf{n}$$Note from this equation that the magnitude of the stress vector is equal to the fluid pressure and that its direction is normal to our arbitrarily oriented surface. Thus, under hydrostatic conditions, there is no shear stress component on any surface.