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Page 1: STRUCTURAL GEOLOGY Lectures Series 2.pdf

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Lect. 25 - Strike-Slip Faulting 129

Figure 25-1: The San Andreas (adapted from Twiss and Moores, 1992).

Strike-slip faults are rarely planar. This is best illustrated by the big bend on the

San Andreas Fault just north of Los Angeles. The San Andreas is a right lateral strike-

slip fault with Pacific Plate moving north relative to the North American Plate. This

means that Los Angeles and San Francisco on the Pacific Plate are moving north relativeto the rest of North America. The big bend north of Los Angeles is called a restraining

 bend largely because the westward jump in the fault when tracing the fault to the north,

leaves rocks in the way for further slip (Figure 25-2). These ‘extra’ rocks must be movedout of the way for further slip. Depending on the shape of the irregularities along strike-

slip faults relative to the motion along the fault, there may also be releasing bends. These

are places where cavities open because opposite sides of an irregularity move away fromeach other (Figure 25-2).

Figure 25-2: A. A planar strike-slip fault. B. Strike-slip movement along irregularly

curved faults producing gaps at releasing bends and crowding at restraining bends

(adapted from Crowell, 1974).

Restraining and releasing bends produce diagnostic structures. The restraining

 bend produces a ‘flower structure’ which is a series of vertical faults of compressionalduplexes that are subparallel to the parent fault. The vertical faults divide upthrown

 blocks the spread near the surface in a manner resembling a flower. The upthrown blocks

are sometimes called popups.

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Lect. 25 - Strike-Slip Faulting 130

 Figure 25-3: Restraining bend with a compressional duplex (adapted from Twiss and

Moores (199)).

Releasing bends produce pull-apart basins. Like the restraining bend, a series of 

faults that form subparallel to the parent fault produce a structure that in cross section iscalled a ‘flower structure’ (Figure 25-4).

Figure 25-4: Extensional duplexes at releasing bends (adapted from Twiss and Moores,1992).

An example of a restraining bend is found along the San Andreas Fault where thecontraction expected at a left bend in a dextral fault is seen as the block uplifts on the

Transverse Ranges (Figure 25-5). The restraining bend of the San Andreas is reflected in

the blocks bounded by east-west thrust faults. Extensional basins are also presentincluding the Salton Sea trough between the San Andreas and San Jacinto faults.

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Lect. 25 - Strike-Slip Faulting 131

 Figure 25-5: The San Andreas Fault system showing the block uplifts of the Transverse

Ranges of southern California (adapted from Twiss and Moores, 1992).

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Lect. 25 - Strike-Slip Faulting 132

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Lect. 25 - Strike-Slip Faulting 133

STRUCTURAL GEOLOGY

Lecture 26

Folding of Rocks(Analysis of Fold Geometry)

Folds are the second important component of fold-thrust belts and rock 

deformation in general. Whereas faults were treated as a general manifestation of brittledeformation within the upper 10 km of the crust, folds are generally regarded as a

manifestation of ductile deformation. In fold-thrust belts folds are necessary to

accommodate faulting. Folds are most commonly marked by bedding, a surface referredto as S0 in structural geology. Folds are characterized by axial surfaces, S1, and a fold

axis (Fig. 26-1). The plane perpendicular to the fold axis is that surface on which the

 profile of a fold is projected. A fold that has a planar axial surface is said to be a plane

fold, otherwise it is a nonplanar fold.

(Fig. 26-1)

One ideal fold is cylindrical with any profile the same as any other profile (Fig.

26-2). Real folds are rarely cylinderical but rather conical in shape. The ideal fold can be

divided into the hinge area where the radius of curvature of the fold is smallest and thelimb area where the radius of curvature of the fold is largest. Figure 26-2 shows a profile

or cross section through a set of cylinderical folds constituting a wave train. The

Amplitude and wave length of the wave train are shown.

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Lect. 25 - Strike-Slip Faulting 134

 (Fig. 26-2)

Folds are sometimes overturned as in Fig. 26-3. In that figure the sandstone is

younger than the limestone, yet in the overturned limb the older limestone appears over 

the younger sandstone. The direction of younging is said to be downward. Theenveloping surface of the folds as well as the crest and trough are indicated.

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Lect. 25 - Strike-Slip Faulting 135

(Fig. 26-3)

Folds have many shapes in cross section depending on their intralimb angle. Four 

general classes of folds based on intralimb angle are: Gentle, Open, Tight, and Isoclinal.

Other shapes of folds are indicated in Fig. 26-4 as Rounded, Angular, Chevron, and Box.

(Fig. 26-4)

Folds may be classified based on the orientation of their hinge line and axial

surface. Turner and Weiss (1963) have identified seven types of folds including:

horizontal normal, plunging normal, horizontal inclined, plunging inclined, Reclined,Vertical, and Recumbent (Fig. 26-5).

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Lect. 25 - Strike-Slip Faulting 136

 

(Fig. 26-5)

Ramsay's classification of folds is based on the dip isogon. A dip isogon is theline joining points of equal dip as shown in Fig. 26-6. Two common types of folds are the

similar and parallel folds. In similar folds the bedding shape remains the same from bed

to bed whereas in parallel folds the bedding thickness remains unaltered from bed to bed.

(Fig. 26-6)

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Lect. 25 - Strike-Slip Faulting 137

In order to maintain similarity from bed to bed, material within the beds must be

moved out of the limbs and into the hinges (Fig. 26-7).

(Fig. 26-7)

In parallel folds the shape of the beds must change from layer to layer in order themaintain constant bed thickness throughout (Fig. 26-8).

(Fig. 26-8)

Folds

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Lect. 25 - Strike-Slip Faulting 138

Structural Geology

Lecture 27

Buckle Folds(Mechanics of Folding)

The mechanics of folding of layered rocks has evolved from the model for the

folding of an elastic plate. Figure 27-1 shows an elastic plate with a thickness of 2y. The

 plate is folded upon the application of a force P distributed on the area ∆A at the ends of 

the plate. As the plate is folded the upper portion of the plate is stretched (stippled area)whereas the lower portion of the plate is compressed. A plane between the compressed

and stretched portion of the plate is folded but neither stretched nor compressed. This

 plane is referred to as the neutral surface. A plane normal to the fold axis cuts the neutral

surface to form a line called the neutral fiber. In Figure 27-1 the neutral fiber has the

length l. A line a distance of y above the neutral fiber has the length l+ ∆l. The stretch

∆l is proportional to

∆l/l = y/R .

(Fig. 27-1)

An elastic fold such as is shown in Figure 27-1 is known as a buckle. The force P 

necessary to cause the buckle is proportional to the distance from the neutral fiber. For 

the force per unit area on a small strip at y from the neutral fiber 

∆P/ ∆A = E.y/R  

σ = E ε 

ε = ∆l / l

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Lect. 25 - Strike-Slip Faulting 139

where E is the Young's modulus. For elastic plates the bending moment (M) is defined as

the torque about the neutral fiber.

M = ∫ ydP

cross section 

or let

dP = E.y/R dA

then

˙ 

M = E/R ∫ y2dA

cross section 

 Now the moment of inertia (I) about a horizontal axis through its "unit mass" is

I = ∫ y2dA

so

M = E/R I.

Curvature is defined as the rate of change of a curve (i.e. the neutral fiber) in the verticaldirection (y) as a function of distance in the horizontal direction (Fig. 26-2).

1/R   ≈ - (d2y / d2x).

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Lect. 25 - Strike-Slip Faulting 140

 

(Fig. 26-2)

Folds can also be defined in terms of a bending moment at x where the equationfor a beam is

M(x) = EI (d2y / d2x) = Py

Rearranging this equation we can construct a homogeneous 2nd order differential

equation

Py

d2y / d2x = - ___ EI 

The same equation for the buckling of a plate is

M(x) = EI/(1- ν). d2y / d2x.

where ν is the Poisson's ratio for that plate. For small deflections the shape of a buckled beam can be represented by the equation

y = yosin πx/

where L is the half-wave length of the buckle fold. If we take the derivative of this

equation

dy

dx= yo

π  

 Lcos

π   x

 L 

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Lect. 25 - Strike-Slip Faulting 141

and then take the second derivative

d 2 y

d 2 x= yo

π  2

 L2 sinπ   x

 L 

Replacing terms on the right side of this equation, we derive

d2

y

d2

x= −

π  2y

L2

,

the second order differential equation for the bending moment can be written in terms of 

the force necessary to cause the buckle. Taking the homogeneous 2nd order differential

equation from above and rewriting it in terms of P, we derive

P = d 2

 yd 2 x

 EI  y

 

Substituting for d 2 y

d 2 x 

P = π  2EI

L2

.

If the end of the buckle fold is fixed P =4π  

2 EI 

 L2 

The physical significance of this force P is that if P is less than a certain value there will be no bending but if the force is slightly greater, the beam will bend suddenly where

π  2EI

L2

= the Euler force at which a beam will buckle.

Figure 26-2 shows a first and second mode fold. The second mode is modeled as

y = yo sin ( 2π/L) 2 

The Euler buckling formula for the second mode fold is

P2 = EI(2π/L) 2 

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Lect. 25 - Strike-Slip Faulting 142

 

This equation is the load necessary to hold a member of length 2L in a 2nd mode of  buckling.

Rocks layers differ from the single member which is constrained neither on top of 

 bottom. Rather anytime that a rock layer folds, that layer has to contend with moving

aside the rock layers above and below. In modeling folds these adjacent layers arehandled in several manners. We will consider two approaches to the "confined member"

fold. First we will consider the situation where both the layer of interest and those above

and below are elastic. The layer in question is considered competent and located in anincompetent elastic media.

Johnson (1970) considers the problem of a confined member loaded axially (Fig.

26-3). The elastic member is responding to axial loads, P, shear forces, Q; bendingmoments, M; and a distributed load, q. The distributed load is due to the elastic medium

having an elastic constant k. The load on the confining medium is then proportional to

the deflection, y, of the folded layer. Consider a small element of length δx and thicknessequal to the confined member. The axial load on both ends are P but they are not

colinear so that they bend the member where bending moment on one end is M and themoment on the other end is M + δM.

This element can be examined by summing the moments around the right end

(Fig. 26-3). The moments exerted by P and Q + δQ on the right-hand end vanish, because their lever arms are zero. Summing moments

ΣM = 0

- M + (M + δM) - Q δx + P( δy) = 0

δM - Q δx + P δy = O

 Now divide by δx and take the limits as δx approaches zero.

dM/dx - Q + pdy/dx = 0

Q = p dy/dx + dM/dx.

By summing the forces in the y direction we find that

Q - (Q + δQ) - k(y) δx = 0

dQ/dx = - ky

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Lect. 25 - Strike-Slip Faulting 143

This is equivalent to the relation between the shear force and the distributed load derived

earlier for a member that was not supporting an axial load.

Combining the equation for forces in y direction and the moments we have

d2

M / d2

x + p (d2

y / d2

x) = -kyWe learned earlier that

M = EI (d2y / d2x)

So now

EI (d4y / d4x) + P (d2y / d2x) + ky = 0

The general solution to this equation has the form of a sinusoidal deflection of the rod.

y = y0cos lx

(Fig. 26-3)

Where the wave length of the deformation is L the wave number is l

L = 2π/l 

The force with which the rod is pushing against the lateral constrain is

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Lect. 25 - Strike-Slip Faulting 144

-ky = Pl2y - EIl4y

where Pl2y is the driving force generated by compression P and EIl4y is the restraint

against deformation by bending rigidity. There is a wave length for which -ky = 0 and

the two terms are equal. This value for l is the Euler Wave Length.

Le = 2π√(EI/P).

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Lect. 25 - Strike-Slip Faulting 145

STRUCTURAL GEOLOGY

Lecture 28

Kink Bands and Chevron Folds(Analysis of Fold Geometry)

Kink bands occur in strongly anisotropic rock where the anisotropy is either beds

with a finite thickness or foliation with very thin layers. These two are fundamentallydifferent types of geological material that kink in different manners. The first is a well

cleaved schist where individual microlithons are very thin. This material resembles a

 pack of computer cards where folding is vary sharp at the hinges. In the secondgeological material the bedding has a finite thickness where any folding at the hinges has

to respond to the thickness of the hinges. Kinks in bedded material resemble the common

chevron folds which will also be discussed within this lecture.

The terminology for kink bands is shown in Fig. 28-1 where the kink band is thatzone within the beds or foliation has been rotated. In the case of Fig. 28-1 the geological

material has an anisotropy developed by the bedding planes. Within the kink band the beds have been rotated from horizontal to a steeply dipping position. The kink plane isthe boundary between the rotated and unrotated portion of the beds. The kink axis is the

same as a fold axis with the strike of the axis parallel to the strike of the kink plane

 provided the beds were initially horizontal.

(Fig. 28-1)

Kink-bands and kink-like folds may develop by flexural slip or continuous

simple shear. The deformation within a kink band can be described in terms of an

external rotation (ϕ) and an internal rotation (θ). The external rotation takes the bedding

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Lect. 25 - Strike-Slip Faulting 146

 planes or foliation and rotates them through an angle ϕ so that the beds or foliation arerotated into the obtuse angle sector between the kink band boundary (kink plane) and the

foliation outside the band (Fig. 28-2). The internal rotation (θ) is shown in Fig. 28-2 asthe rotation of the radius of an undeformed circle to the deformed ellipse. The strain

ellipse within the kink band shows the opposite sense of rotation from the shear couple

 parallel to the kink-band boundary. The shear S indicated by the internal rotation (θ) can be measured according to the rule

1 - cos (α + ϕ) sec αS = tan θ = __________________ 

sin (α + ϕ) sec α 

Compressive strain parallel to the foliation is

ef  = 1 - cos ϕ

(Fig. 28-2)

Kink bands develop one of two senses of rotation known as normal and reverse

respectively (Fig. 28-3). Largely the difference is determined by the acute angle between

the foliation and the kink-band boundary. For the normal kink band the external rotation

is opposite in sign from the acute angle measured from the kink plane to the foliation. Inthe reverse kink band the external rotation has the same sign. The limbs of kinks are

distinguished on the bases of whether the kink band constitutes the long limb or short

limb. Often the rotated limb is the short limb.Chevron folds resemble kink bands except there is generally one fold plane

where kinks are distinguished by a pair of kink planes. Figure 28-4 shows a three beds

and gives an indication of the nature of deformation associated with the limbs and hingearea. The sandstone in the hinge is above the neutral fiber and as a consequence extends

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Lect. 25 - Strike-Slip Faulting 147

along fractures as shown in black. The hinge area in this fold is not as sharp as was the

case for the kink bands. As the hinge develops there are room problems where holesopen and other portions of the fold wants to overlap. Usually in the areas of overlap the

folds take the overlap by pressure solution where part of the bed is dissolved and carried

away in solution or redeposited in the form of veins.

Three types of rotation can be distinguished in association with the fold. Therotation #1 is an external rotation as indicated by the change in orientation of the

 bedding. This is ƒ in the previous figures. Rotation #2 is an internal rotation and is

shown on the strain ellipse of figure 28-2. Rotation #3 develops off of beds of limestonethat have been shortened by cleavage development. Each block of limestone is bounded

 by pressure solution cleavage that dissolves the beds and permits shortening without the

total rotation shown as #1 for the sandstone beds.

(Fig. 28-3)

Fault-bend folds are a consequence of décollement tectonics where bedding

 parallel detachments climb section by cutting across several beds. A model of fault-bend

folding is shown in figure 28-5 where the thrust plane comes from the right, cuts upward

across bedding, and continues parallel with bedding off to the left. Upon the initiation of the fault across bedding two kink bands develop at the bends in the footwall because

these bends cause folding in the upper sheet of the thrust system. The axial surfaces A

and B terminate a the bends in the detachment where it changes from bedding parallel tocross cutting. The axial surfaces A' and B' terminate at the transitions between

crosscutting and bedding-plane fault segments in the hanging wall at points X' and Y'

which match points X and Y in the footwall. As slip continues kink bands A-A' and B-B'grow in with and the anticline above the crosscutting fault grows in height. Axial

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Lect. 25 - Strike-Slip Faulting 149

 (Fig 28-5)

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Lect. 25 - Strike-Slip Faulting 150

 (Fig. 28-6)

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Lect. 25 - Strike-Slip Faulting 151

STRUCTURAL GEOLOGY

Lecture 29

Fold-Thrust Belt Deformation(Overthrust Belts Reexamined)

Overthrust terrains can be divided into two general classes: 1.) Those where the

decollement surface is parallel to bedding within the sedimentary section. The centralAppalachian Valley and Ridge and the Canadian Rockies are representative examples.

2.) Those terrains where a horizontal thrust sheet develops in crystalline basement and

 breaks upward through the sedimentary overburden. The Wyoming Province of the U.S.Rockies is a type example of structures in sedimentary rocks developing over crystalline

upthrusts. The Brevard fault zone in the southern Appalachians is believed to be another 

example.

(Fig. 29-1)

Three general classes of thrust faults develop within thrust sheets whose

decollement is within the sedimentary section. Geiser (1986) has labeled these structures

as: Break Thrusts, Fold Thrusts, and Shortening Thrusts (Fig. 29-1). Each of the threehas a different mechanical behavior as explained below.

Break thrusts develop where the Coulomb-Mohr failure criterion is favored over 

folding and shortening. Fold-thrust belts developed in a thick but reasonably

homogeneous stratigraphic section seem to favor the break thrust style. The southernAppalachians is one example of the break thrust style. This style seems to be the most

common throughout the upper crust.

Fold thrusts develop where the viscosity contrast between a sheet of sediments

(¥) and the underlying rock (η) is large.

η > η1 

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Lect. 25 - Strike-Slip Faulting 152

 

In this case the Euler Buckling Force is relatively low conpared with the Coulomb-Mohr failure criterion.

πEI/L2 < S0 + µiσn

A fine example of fold thrusts may be found in the Swiss Jura where thin box folds form

over a Mesozoic salt.

Shortening thrusts develop in association with volume loss strain. An example isthe Appalachian Plateau where the plateau is folded slightly over blind thrusts but the

dominant mechanism for absorbing the decollement slip layer parallel shortening. The

mechanism for shortening is the development of solution cleavage where the dissolved

rock is carried out of the section in circulating water. Shortening occurs because theyield stress for pressure solution cleavage is less than the Euler Buckling Force and the

Coulomb-Mohr failure criterion

σyield < πEI/L2

σyield < S0 + µiσn

(Fig. 29-2)

In map view the structural style of the Appalachians changes from the Central to

Southern Appalachians (Fig. 29-2). In the Central Appalachians the stratigraphic section breaks into two mechanical units: the lower carbonates are mechanically strong relative

to the cover of clastic rocks. this difference in strength is manifest by blind thrusting

where the carbonates duplex below a roof thrust. The cover folds in response to thechange in shape of the underlying duplex. In contrast, the southern Appalachians consist

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Lect. 25 - Strike-Slip Faulting 153

of a suite of emergent thrusts. Here the cover is relatively thinner. This decrease in

thickness of the cover is thought to be responsible for the lack in development of a roof thrust and subsequent differential behavior between the basement and cover rocks.

When crystalline rocks break through cover, the folds that develop within cover 

are called drape folds. This indicates that the folding is not in response to end loading but

rather the folds develop as passive sheets which fall into place over the changing shape of  basement rock. The force for this type of folding derives from the change in shape of the

 basement as it is uplifted on listric shaped reverse faults.

In terrain where crystalline thrusts break to the surface two types of behavior areknown for the cover rocks (Fig. 29-3). If the cover rocks consist of thick sections of 

carbonates and shale, then the drape folds break into blocks which slide on decollement

(detachment) surfaces. If the cover consists of thin clastic sections without an obviousdetachment layer, then the cover thins over the crystallin upthrust. The mechanism for 

this thinning is often cataclastic flow.

(Fig. 29-3)

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Lect. 25 - Strike-Slip Faulting 154

STRUCTURAL GEOLOGY

Lecture 30

Cleavage(continuous and spaced)

 Nature of Cleavage

Geometric relationship of cleavage to folding

Geometric relationship of cleavage to shearing

Domainal character of cleaved rocks

cleavage domains

microlithon domains

Types of CleavageContinuous cleavage

slaty - fine grained rocks

 phyllitic - soft, pearly, satiny luster 

schistosity - medium grained rocks

Disjunctive cleavage

Crenulation cleavage

Spaced Cleavage

Microscopic properties of cleavage

Slaty Cleavage

Mica-rich domains

Quartz-feldspar domains

Schistosity

Crenulation Cleavage

Spaced Cleavage

Strain Significance of Cleavage

Expression of Shortening

Alignment of Mica without grain rotationEstimates of Volume Loss

Crenulation Cleavage vs. Shortening

Classification of Spaced Cleavage

Passive Folding

Characteristics of Passive Folding

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Lect. 25 - Strike-Slip Faulting 155

Transposition

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Lect. 25 - Strike-Slip Faulting 156

STRUCTURAL GEOLOGY

Lecture 31

Lineation & Foliation(foliation)

Foliation - any mesoscopically penetrative parallel alignment of planar fabric elements inrock.

Primary foliations: flow banding in rhyolite and axial planar cleavage in slump

folds

Secondary foliations: cleavages and mylonitic foliation

Metamorphic foliations: slaty cleavage, schistosity, gneissic structure

Mylonite foliations: Protomylonite < 50% matrixMylonite - 50% to 90% matrix

Ultramylonite - > 90% matrix

Lineation - parallel alignment of elongate linear fabric elements in a rock body.

Mineral lineation

Stretched-Pebble conglomerate

Rodding

Mullion

Pencil Structure

Boudin

Tectonites:

S-tectonite

L- tectonite

LS - tectonite

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Lect. 25 - Strike-Slip Faulting 157

 

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Lect. 25 - Strike-Slip Faulting 158

STRUCTURAL GEOLOGY

Lectures 33-34

Mechanisms for Ductile Flow(dislocations, recrystallization, pressure solution)

In addition to brittle fracture several other mechanisms are responsible for the

structures of the earth. Each mechanism alone or combined with other mechanisms actsto facilitate the changes in the shape of rocks at various levels in the crust of the earth.

The higher the temperature (i.e. the deeper within the crust), the more likely that ductile

mechanisms dominate over brittle mechanisms in controlling the style of deformation.Ductile mechanisms can be divided into intergranular and intragranular processes.

Higher temperatures favor intragranular processes.

 Near the surface of the crust pressure solution is the most common intergranular 

deformation mechanism. It is manifested by cleavage in low-grade metamorphic rocks,the subject of lecture 17. The basic process involves a dissolution at contact points

 between grains of rock. Characteristically one grain will dissolve faster than the other.The product of this differential dissolution is a stylolite in fine-grained rocks or pits and beards in pebbles of a conglomerate. The dissolution process is believed to be activated

 by the high normal stress between grain contacts. The rock, dissolved from the high

stress contacts, then diffuses into the pore spaces of the rock where pore fluid exerts theonly normal stress at pressures much less than found along grain-to-grain contacts (Fig.

33-1).

(Fig. 33-1)

In two or more component systems one material will dissolve faster than another.

For example, in a pelagic limestone the calcite dissolves and clay forms as an insoluble

residue. In a one component system, the single component dissolves uniformly. In a

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Lect. 25 - Strike-Slip Faulting 159

shale (clay) the composition of the shale after 50% shortening is the same as the initial

shale. In quartzites the grain boundaries are irregular as the grains penetrate each other.There are several possible sinks for the dissolved material. In conglomerates

 beards appear in the pore space. Many rocks contain veins opening normal to the

maximum principal stress. These veins are filled with the material dissolved from grain-

to-grain contacts. In other geologic settings it is clear that the dissolved material iscarried completely out of the system.

Figure 33-2 shows the orientation of σ1 relative to the formation of stylolites and

 pressure solution cleavage. The maximum rate of dissolution is in the direction of σ1.

This favors the formation of a cleavage with its "planar" direction normal to σ1.

(Fig. 33-2)

The rate limiting process in cleavage formation by the pressure solution is the

diffusion of the dissolved rock. Two steps in the diffusion process include: 1.)

Circulation of pore water within the open pore space, and 2.) grain-boundary diffusion.Because grain-boundary diffusion occurs on the scale of mm to cm, circulation of pore

water can account for larger amounts of strain.

A second intergranular deformation mechanism is Coble Creep. This processoccurs by grain-boundary sliding. The sliding may be enhanced by films on the grain

 boundaries. Cataclasis may be a low temperature example of Coble creep involving

 brittle fracture (Fig 33-3).

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Lect. 25 - Strike-Slip Faulting 160

 (Fig. 33-3)

Intragranular deformation involves processes internal to grains and crystals of rocks. No crystalline material is perfect. In a crystalline lattice there are always single

atoms (i.e. point defects) or rows of atoms (i.e. line defects or dislocations) missing.These defects can migrate or diffuse within the crystalline lattice. In fact it is the motionof these defects that allows a crystalline lattice to strain or change shape without brittle

fracture. A crystalline lattice may contain as many as 108

defects per cm3. The motion of 

these defects is controlled by the stress and the temperature to which the crystal issubjected. As both the stress and temperature increase these defects move more often

(i.e. the strain rate increases as a function of differential stress and T (Fig. 33-4).

(Fig. 33-4)

Figure 33-4 shows the cross section of an edge dislocation. The edge dislocation

is the plane of missing atoms extending downward in the figure. The motion of line

defects or dislocation is mapped using the Burger's Vector. For Figure 12-4 the Berger'svector is horizontal. In two dimensions a line defect moves by changing places with a

row or column of existing atoms (Fig. 33-5). The column of atoms marked on black in

Figure 33-5 is about to have its bond on the bottom broken to then occupy the positionabove the plane of missing atoms. By this process the atoms in the upper half of the

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Lect. 25 - Strike-Slip Faulting 161

diagram move to their right relative to the crystalline lattice in the bottom half of the

diagram. We would say that the edge dislocation is moving to the left.

(Fig. 33-5)

This process of dislocation motion in a single plane of atoms is called slip. If asecond line defect intersects the migrating dislocation, the dislocation can climb to

another plane of atoms (Fig. 33-6). In Figure 33-6 the lattice in the top of the figure is

moving to the right relative to the bottom portion of the lattice. A vacancy is shown.

When the lattice hits the vacancy then the edge dislocation grows upward into the latticein the upper portion of the figure. The edge dislocation moves to the right to intersect the

line vacancy.

(Fig. 33-6)

Many dislocations can become piled up in a single plane. Because lattice strain

occurs over each dislocation, the crystal has a different birefringence in the vicinity of the

dislocation. A line of these dislocations can cause the crystal to have a different

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Lect. 25 - Strike-Slip Faulting 162

 birefringence just above the line. This is known as a deformation lamellae and marks line

 piled-up dislocations (Fig. 33-7).

(Fig. 33-7)

Another type of dislocation plane can spiral through the crystal. This is a screw

dislocation. Twin boundaries in calcite are screw dislocations (Fig. 12-8).

(Fig. 33-8)

Recovery and recrystallization are two more intragranular processes. Recovery

is the process of returning the crystal to its original undeformed state. If dislocations

 pile-up in a line perpendicular to their direction of motion or Burger's vector, then asubgrain boundary is formed (Fig. 33-9).

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Lect. 25 - Strike-Slip Faulting 163

 (Fig. 33-9)

Polygonization is the process where edge dislocations climb by atom or vacancy

diffusion and glide to low-energy polygonal networks. Here the subgrain boundaries are

at very small angles to neighbors. Recrystallization takes place when high angle grain boundaries sweep through the crystal. the high angle grain boundaries sweep out many

of the defects in the crystal. The process of normal grain growth tries to reduce grain

 boundary tension by putting grains next to each other with the smallest energy. Heregrains meet at dihedral angles (fig. 33-10).

(Fig. 33-10)

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