Purdue University

EAS 557

Introduction to Seismology

Robert L. Nowack

Lecture 6

 

Analysis of Stress

 

            The concept of stress involves the action of forces on a body.  Two types are considered:

 

1)   Body forces – .  Which are generally forces per unit volume.  For gravitational forces, these depend on the mass distribution within the body.  These are generally non-contact forces.

 

2)   Surface forces – .  These are forces per unit area acting along surfaces of elemental volumes and are contact forces with adjacent parts of the body.  These forces give rise to the concept of traction on external and internal surfaces.  The traction on an external surface of the body is related to the applied force by

 

 

 

 

 

      where  is the average force on the small surface  centered on the point P.   is called the traction vector.

 

 

            Units of traction and stress are in force/area.  In cgs, the units of stress are dyne/cm2.  In SI, the units of stress are 1 Newton/m2 = 1 Pascal (1 Pascal = 10 dyne/cm2).  Other units are

 

            1 bar = 106 dyne/cm2 = 105 Pascals

            1 bar = 1.0133 Atmospheres

            1 kilobar = 15,000 lb/in2

 

            We now want to investigate tractions on internal surfaces within a body. Consider a bar under tension

 

 

 

 

The external applied force, , results in tractions  on the ends.

 

Now, cut the bar and apply forces on the two sides of the cut so that the shape of either section of bar remains unchanged.  Equilibrium requires that .

 

            Now define the tractions  on the upper and lower faces of the cut.  From Newton’s Third Law, .  Thus,  on the arbitrary internal surface that we have constructed.

 

            In 3-D, consider a cut of area  at a point P.  Let  be the force applied to the side with normal

 

 

 

 

Again, .  On the other side of the cut, .

 

 

 

 

From Newton’s Third Law

 

 

Thus, as in the case for the bar, the tractions on either side of the cut are of the same magnitude, but opposite in sign.

 

If we made cuts in other directions, say with normals  and , we would obtain different values for the internal traction at P.  Note that for a fluid, the pressure is related to the traction by  for any .  But in a solid, the magnitude and direction of the traction depends on the orientation of the surface element .

 

Ex)  Consider the walls of a house.

 

 

 

 

For an elemental area of the wall at point , .  But, at point P,  will be non-zero and large.

 

It at first seems that there will be an infinite number of traction vectors at a given point depending on the orientation of the small surface.  But, Cauchy proved, that in fact all the various tractions at P can be derived from a set of six numbers collectively grouped as the “stress tensor”.

 

 

 

Stress Tensor

 

            The idea is instead of defining tractions on arbitrarily oriented planes at point P, we define tractions on the coordinate planes

 

 

 

 

where

 

 

 

where  and  are unit vectors in the x1 and x2 directions.  The vectors are oriented in the conventional positive directions.   Thus,  would be positive if they stretch the material.  Also, on the opposite faces

 

 

 

            In 3D, we will write

 

 

in which  is the stress tensor at the point P, where

 

             are tensional or compressive stresses

             are shear stresses

 

In index notation, the stress tensor is , where i is normal to coordinate plane in which the traction acts and j indicates the component of the traction vector.

 

 

 

 

            Cauchy showed that the stresses on any plane through an internal point P can be written as a linear combination of the elements of the stress tensor.  This is a fundamental theorem of solid mechanics.  Consider the triangle in 2D (tetrahedron in 3-D)

 

 

 

 

The traction on surface with normal  is

 

.

Now we must find the condition of equilibrium of the triangle.  Balancing forces in the x1 and x2 directions gives

 

In the x1 direction: 

 

In the x2 direction: 

 

or

 

 

 

From geometry

 

 

 

We then find

 

 

 

In index notation for 3-D, then

 

     (with implied sum on j)

 

Thus, the knowledge of the stress tensor  specifies completely the state of stress around the point P.

 

In order to prevent the body from spinning, we also require that the net torque be zero.  Evaluating the torque for a reference point at the center of the square, we get

 

 

where  is a force and  is a moment arm.  Then, .

 

In the general 3-D case, .  Because of this relation, the stress tensor is symmetrical, where

 

 

with , , and .  Thus, only six numbers are needed to completely describe the state of stress of an internal point P in a body.

 

It is important to separate between the isotropic and deviatoric part of the stress tensor .  We define

 

 

where  is independent of the coordinate system and P is the pressure.  The minus sign is used to require P to be positive when it is compressive.  The stress elements themselves are positive in tension.  We rewrite  as

 

 

or in index notation

 

 

where  is the deviatoric part of the stress tensor.

 

            For hydrostatic stress, .  For a hydrostatic increase of stress with depth due to a uniform overburden, then

 

 

where  is the density of the overburden, z is thickness, and g is the acceleration of gravity.  As an example, the hydrostatic pressure at a depth of 10 km underneath a thickness of rock with an average density of 3000 kilograms/m3 is

 

P = (3000 kilograms/m3) (10 x 103 m) (9.8 m/s2)

 

= 2.94 x 108 Pascals ~ 294 MPa

 

= 2.94 kbars

 

At an average thickness of the crust of 30 km, the hydrostatic pressure would be on the order of 1 GPa or 10 kbars.

 

 

 

Transformations of the Stress Tensor in Rotated Coordinate Systems

 

 

 

 

            The components of a vector in a rotated coordinate system can be related to the components in the original system by a coordinate rotation matrix .  For example, the components of the vector  above, in two coordinate systems, can be written

 

 

where the components of  are the direction cosines between the old and new coordinate axes.  The rotation matrix is,

 

 

As an example, if , then

 

 

Let , then  in the new coordinate system. 

 

Note for rotation matrices,  since these are orthogonal matrices.  Now assume a general relationship between two vectors  and  

 

 

            In a rotated coordinate system

 

 

Then, the general relationship between  and  can be written

 

 

or

 

 

Thus,  in the new coordinate system where  with .  This general relationship has the same form in any rotated coordinate system with the coefficients depending on the orientation of the coordinate system.

 

            Now, consider the traction vector on an internal plane with normal

 

 

Since , this can also be written

 

   or  

 

In a rotated coordinate system, the traction vector is

 

   with  

 

            Now, we choose  so that  is a diagonal matrix.  In this special coordinate system, all the shear stresses are zero and the normal stresses are called the principle stresses acting with respect to the three rotated coordinate axes.  Let

 

 

where  are the rotated axes with respect to the unrotated axes.  Then,  can be written as

 

 

or for each , then

 

 

forms an eigenvalue problem.  To find the eigenvalues , the determinant of  must be zero.  Thus,

 

 

to solve for .  Next solve for the eigenvectors  and make sure to adjust  to unit length.  Standard computer software, such as Matlab, can be used to find the principle stresses  and the principle stress directions  (i = 1,3).

 

            These can be ordered such that .  Since these are positive for tensional stresses,  provides the maximum compressive stress.  There are no shear or tangential stresses act on these new coordinate faces, only normal stresses.

 

            In the 2-D case, it is useful to derive these relations in detail

 

 

 

 

            Let  where  ,  , and .  Then,

 

 

This can be multiplied out and written in terms of components of  as

 

 

 

 

If we let , then we can find the rotation angle  to be

 

 

Since

 

 

If , then,  will be the maximum and minimum normal stress.  Thus,

 

 

These would then be the eigenvalues in the above eigenvector analysis in 2D.  From , we find that

 

 

on planes with normal 45o from the maximum compressive stress direction.

 

            This gives rise to the simplest theory of faulting where shear failure occurs on planes of maximum shear stress with normals at 45o from the axis of maximum compressional stress.

 

 

 

 

If rocks possess a cohesive strength and internal friction, the angle  will generally be different from 45o.  In 3D, different regimes of faulting can be inferred depending on the orientations of the principle stress directions

 

            For example, normal faulting, thrust faulting, and strike-slip faulting result when the principle stress directions are oriented as below.

 

 

            As an example of the calculation of the principle stresses in 2D, let

 

 

then,

 

 

 

This gives for the principle stresses,

 

    

Thus,

 

Then

 

   and  

 

These must then be normalized to unit length to get  and .  Using the 2-D formulas

 

 

 

            Stress maps showing the orientation of maximum horizontal shear stress have been developed based on orientations of earthquake faulting and in situ stress measurements.  One technique for finding this is from breakout zones in boreholes which align with the principle stress directions and are often consistent over regional distances.

 

 

 

 

(from Meisner, 1986)

 

            A second in situ approach uses the method of hydraulic fracturing in boreholes in which the induced fractures often align with the regional stress direction.

 

 

 

 

(from Meisner, 1986)

 

An example map of maximum horizontal compressive stress is shown below.