folded surfaces & classifications...gg303 lecture 28 11/26/07 1 stephen martel 28-1 university...

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GG303 Lecture 28 11/26/07 1 Stephen Martel 28-1 University of Hawaii FOLDED SURFACES & CLASSIFICATIONS I Main Topics A Curvature at a point along a curved surface B Fold nomenclature and classification schemes C Interference of folds D Superposition of folds II Curvature at a point along a curved surface A Local equation of a plane curve in a tangential reference frame At x= 0, y = 0. At x= 0, y’ = 0. Express the plane curve as a power series of linearly independent terms: 1 y = K + C 2 x 2 + C 1 x 1 [ ] + C 0 x 0 [ ] + C 1 x 1 + C 2 x 2 + C 3 x 3 + K [ ] . As y is finite at x= 0, all the coefficients for terms with negative exponents must be zero. At x= 0, all the terms with positive exponents equal zero. Accordingly, since y = 0 at x = 0, C 0 = 0. So equation (1) simplifies: 2 y = C 1 x 1 + C 2 x 2 + C 3 x 3 + K . The constraint y’ = 0 at x = 0 is satisfied at x = 0 only if C 1 = 0 3 y = C 1 x 0 + 2C 2 x 1 + 3C 3 x 2 + K = 0 . 4 y = C 2 x 2 + C 3 x 3 + K . Now examine the second derivative: 5 y = 2C 2 + 6C 3 x 1 + K . Only the first term contributes as x 0, hence 6 lim x 0 y = C 2 x 2 . So near a point of tangency all plane curves are second-order (parabolic). At x = 0, x is the direction of increasing distance along the curve, so 7 lim x 0 K = y ( s ) = y ( x ) = 2C 2

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Page 1: FOLDED SURFACES & CLASSIFICATIONS...GG303 Lecture 28 11/26/07 1 Stephen Martel 28-1 University of Hawaii FOLDED SURFACES & CLASSIFICATIONS I Main Topics A Curvature at a point along

GG303 Lecture 28 11/26/07 1

Stephen Martel 28-1 University of Hawaii

FOLDED SURFACES & CLASSIFICATIONS

I Main Topics

A Curvature at a point along a curved surface

B Fold nomenclature and classification schemes

C Interference of folds

D Superposition of folds

II Curvature at a point along a curved surface

A Local equation of a plane curve in a tangential reference frame

At x= 0, y = 0.

At x= 0, y’ = 0.

Express the plane curve as a power series of linearly independent terms:1

y = K+ C−2x−2 + C−1x

−1[ ] + C0x0[ ] + C1x

1 + C2x2 + C3x

3 +K[ ] .

As y is finite at x= 0, all the coefficients for terms with negative exponents

must be zero. At x= 0, all the terms with positive exponents equal zero.

Accordingly, since y = 0 at x = 0, C0 = 0. So equation (1) simplifies:

2

y = C1x1 + C2x

2 + C3x3 +K .

The constraint y’ = 0 at x = 0 is satisfied at x = 0 only if C1 = 0

3

′ y = C1x0 + 2C2x

1 + 3C3x2 +K = 0 .

4

y = C2x2 + C3x

3 +K . Now examine the second derivative:

5

′ ′ y = 2C2 + 6C3x1 +K . Only the first term contributes as x → 0, hence

6

limx→0

y = C2x2.

So near a point of tangency all plane curves are second-order (parabolic).

At x = 0, x is the direction of increasing distance along the curve, so7

limx→0

K = y(s ′ ′ ) = y(x ′ ′ ) = 2C2

Page 2: FOLDED SURFACES & CLASSIFICATIONS...GG303 Lecture 28 11/26/07 1 Stephen Martel 28-1 University of Hawaii FOLDED SURFACES & CLASSIFICATIONS I Main Topics A Curvature at a point along

GG303 Lecture 28 11/26/07 2

Stephen Martel 28-2 University of Hawaii

B Local equation of a surface in a tangential reference frame

In this local reference frame, at (x= 0, y = 0), z = 0, ∂z/∂x = 0, ∂z/∂y = 0.

Plane curves locally all of second order pass through a point on a surface z =

f(x,y) and contain the surface normal, so any continuous surface is locally

2nd order. The general form of such a surface in a tangential frame is

8

z = Ax 2 + Bxy + Cy 2 ,

where at (x= 0, y = 0), z = 0, and the xy-plane is tangent to the surface.

This is the equation of a paraboloid: near a point all surfaces are second-

order elliptical or hyperbolic paraboloids.

Example: curve (normal section) in the arbitrary plane y = mx9

limx→0,y→0

z = Ax 2 + Bx mx( ) + C mx( )2 = A + Bm + Cm2( )x 2.

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GG303 Lecture 28 11/26/07 3

Stephen Martel 28-3 University of Hawaii

C Directions and magnitudes of principal curvatures for a surface

Consider the family of curves (i.e., normal sections) formed by a surfaceintersecting a series of planes through the surface normal at a point (seediagram above). The curve with the most positive tangent a short distancefrom the point of tangency (the local origin), as measured in a tangentialreference frame, has a unit tangent that increases at the greatest rate(i.e., has the greatest curvature). The curve with the least positive tangenta short distance from the local origin has a unit tangent that increases atthe smallest rate (i.e., has the least curvature). Near the point of tangency,the values of dx and dy determine the direction of various curves. We seekthe direction, given by dx and dy, for which the curvature will be greatest(see diagram below, where dr is an incremental distance from the origin inthe tangent plane and dr2 = dx2 + dy2).

Cross section containing the normal to the surface (z). The intersection ofthe cross section with the surface yields a plane curve called a normalsection. The r-direction is in the tangent plane, with z = 0 at r = 0. The firstderivative at a small distance from the point of tangency will equal thesecond derivative multiplied by the distance dr.

The first partial differentials of a function z(x,y) represent the change in z(i.e., dz) for a given change in x (i.e., dx) or y (i.e., dy):

10a

∂ 2z∂x 2

dx +∂ 2z∂x∂y

dy =∂ dz( )∂x

10b

∂ 2z∂y∂x

dx +∂ 2z∂y 2

dy =∂ dz( )∂y

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GG303 Lecture 28 11/26/07 4

Stephen Martel 28-4 University of Hawaii

In the tangential frame dz = z, so (10a) and (10b) can be rewritten as

11a

∂ 2z∂x 2

dx +∂ 2z∂x∂y

dy =∂z∂x

11b

∂ 2z∂y∂x

dx +∂ 2z∂y 2

dy =∂z∂y

These can be written in matrix form:

12a

∂ 2z∂x 2

∂ 2z∂x∂y

∂ 2z∂y∂x

∂ 2z∂y 2

dxdy

=

∂z∂x∂z∂y

Stress: traction equivalent

σ xx σ yx

σ xy σ yy

nxny

=

TxTy

The first derivatives of z (on the right side of equation 12a) at a smalldistance dr from the point of tangency equals second derivatives multipliedby dr, and the second derivative in a tangential reference frame is a normalcurvature. Accordingly, equation (12a) can be rewritten in the form Ax = λx:

13a

∂ 2z∂x 2

∂ 2z∂x∂y

∂ 2z∂y∂x

∂ 2z∂y 2

dxdy

= k

dxdy

Stress: traction equivalent

σ xx σ yx

σ xy σ yy

nxny

= T

nxny

Solving equation (13a) yields the maximum and minimum curvatures and theirdirections (as measured in the tangent plane). The square matrix on the leftside of equation (13a) is symmetric because ∂2z/∂x∂y = ∂2z/∂y∂x. Itseigenvalues (i.e., the principal curvatures) are given by the term k on theright side of equation (13a). Its eigenvectors, given by dx and dy, are thedirections of the principal curvatures. An analogy between principalcurvatures and principal stresses is even more apparent if one writes∂2z/∂xi∂yj as kij:

14a

kxx kyxkxy kyy

dxdy

= k

dxdy

Stress: traction equivalent

σ xx σ yx

σ xy σ yy

nxny

= T

nxny

Since the square matrix in equations (13a) and (14a) is symmetric, theprincipal curvatures are orthogonal (see lecture notes on symmetricmatrices). The product of the principal curvatures is the Gaussiancurvature (K = k1k2), and their mean is the mean curvature (H = [k1+k2]/2).

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GG303 Lecture 28 11/26/07 5

Stephen Martel 28-5 University of Hawaii

D Euler’s equation on normal curvatureBy using the material in the previous section and in the notes on symmetricmatrices, equation (8) can be re-written to eliminate the xy-term by usingthe reference frame of the principal curvatures and surface normal:

(15) z = (1/2) (A*x*2 + C*y*2),where x* and y* are the directions of the principal curvatures k1 and k2,respectively. If we let x* = r cosθ and y* = r sinθ, we obtain the equation ofany normal section curve in the direction of θ

(16) z = (1/2) (A* cos2 θ + B* sin2 θ)r2

The second derivative of z with respect to r gives the normal curvature

(17) ∂2z/∂r2 = A* cos2 θ + B* sin2 θ

The r-direction is tangent to the curve at the point we are evaluating thecurvature, so the r- and s-directions coincide, so the second derivative of zwith respect to r gives the normal curvature

(18) k = k1 cos2 θ + k2 sin2 θ

This is Euler’s equation on normal curvature, developed in 1760. It showsthat for any direction the normal curvature is bracketed by the maximumcurvature and the minimum curvature.

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GG303 Lecture 28 11/26/07 6

Stephen Martel 28-6 University of Hawaii

II Fold nomenclature and classification schemesA Emerging fold terminology and classification

1 Classification of Lisle and Toimil, 2007*)

K < 0 (Anticlastic)

Principal curvatures

have opposite signs

K > 0 (Synclastic)

Principal curvatures

have same signs

H < 0 (∩) antiform Anticlastic antiform

k1 > 0, k2 < 0, |k2| > |k1|

“Saddle on a ridge”

Synclastic antiform

k1 < 0, k2 < 0

H > 0 (∪) synform Anticlastic synform

k1 > 0, k2 < 0, |k1| > |k2|

“Saddle in a valley”

Synclastic synform

k1 > 0, k2 > 0

• * Lisle and Toimil (2007) consider convex curvatures as positive

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GG303 Lecture 28 11/26/07 7

Stephen Martel 28-7 University of Hawaii

2 Classification of Mynatt et al., 2007

K < 0 (saddle)

Principal curvatures

have opposite signs

K = 0 K > 0 (bowl or dome)

Principal curvatures have

same signs

H < 0 (∩)

Antiform

Antiformal saddle

k1 > 0, k2 < 0, |k2| > |k1|

“Saddle on a ridge”

Antiform

k1 = 0, k2 < 0

Dome

k1 < 0, k2 < 0

H = 0 Perfect saddle

k1 > 0, k2 < 0, |k2| = |k1|

Plane

k1 = 0, k2 = 0

Not possible

H > 0 (∪)

Synform

Synformal saddle

k1 > 0, k2 < 0, |k1| > |k2|

“Saddle in a valley”

Synform

k1 > 0, k2 = 0

Basin

k1 > 0, k2 > 0

• Mynatt et al., (2007) consider convex curvatures as positive

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GG303 Lecture 28 11/26/07 8

Stephen Martel 28-8 University of Hawaii

function folds3d

% Prepares figures of 3D foldsx = -1:0.1:1;y = x;[X,Y] = meshgrid(x,y);

% Classification scheme of Lisle and Toimil (2007)figure (1)

% Anticlastic antiform: k1 > 0, k2 < 0, |k2| > |k1|k1 = 1; k2 = -2;Z = 0.5*(k1*X.^2 + k2*Y.^2);subplot(2,2,1)surf(X,Y,Z)title ('Anticlastic antiform: k1 > 0, k2 < 0, |k2| > |k1|')

% Synclastic antiform: k1 < 0, k2 < 0k1 = -1; k2 = -2;Z = 0.5*(k1*X.^2 + k2*Y.^2);subplot(2,2,2)surf(X,Y,Z)title ('Synclastic antiform: k1 < 0, k2 < 0 ')

% Anticlastic synform: k1 > 0, k2 < 0, |k1| > |k2|k1 = 2; k2 = -1;Z = 0.5*(k1*X.^2 + k2*Y.^2);subplot(2,2,3)surf(X,Y,Z)title ('Anticlastic synform: k1 > 0, k2 < 0, |k1| > |k2| ')

% Anticlastic antiform: k1 > 0, k2 > 0k1 = 2; k2 = 1;Z = 0.5*(k1*X.^2 + k2*Y.^2);subplot(2,2,4)surf(X,Y,Z)title ('Anticlastic antiform: k1 > 0, k2 > 0 ')

%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%

% Classification scheme of Mynatt et al. (2007)figure (2)

% Antiformal saddle: k1 > 0, k2 < 0, |k2| > |k1|k1 = 1; k2 = -2;Z = 0.5*(k1*X.^2 + k2*Y.^2);subplot(3,3,1)surf(X,Y,Z)title ('Antiformal saddle: k1 > 0, k2 < 0, |k2| > |k1| ')

% Antiform (cylindrical): k1 = 0, k2 < 0k1 = 0; k2 = -2;Z = 0.5*(k1*X.^2 + k2*Y.^2);

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GG303 Lecture 28 11/26/07 9

Stephen Martel 28-9 University of Hawaii

subplot(3,3,2)surf(X,Y,Z)title ('Antiform (cylindrical): k1 = 0, k2 < 0')

% Dome: k1 < 0, k2 < 0k1 = -1; k2 = -2;Z = 0.5*(k1*X.^2 + k2*Y.^2);subplot(3,3,3)surf(X,Y,Z)title ('Dome: k1 < 0, k2 < 0')

% Perfect saddle: k1 > 0, k2 < 0, |k2| = |k1|k1 = 1; k2 = -1;Z = 0.5*(k1*X.^2 + k2*Y.^2);subplot(3,3,4)surf(X,Y,Z)title ('Perfect saddle: k1 > 0, k2 < 0, |k2| = |k1|')

% Plane: k1 = 0, k2 = 0k1 = 0; k2 = 0;Z = 0.5*(k1*X.^2 + k2*Y.^2);subplot(3,3,5)surf(X,Y,Z)title ('Plane: k1 = 0, k2 = 0')

% Not Possiblesubplot(3,3,6)title ('Not Possible')

% Synformal saddle: k1 > 0, k2 < 0, |k1| > |k2|k1 = 2; k2 = -1;Z = 0.5*(k1*X.^2 + k2*Y.^2);subplot(3,3,7)surf(X,Y,Z)title ('Synformal saddle: k1 > 0, k2 < 0, |k1| > |k2|')

% Synform (cylindrical): k1 > 0, k2 = 0k1 = 1; k2 = 0;Z = 0.5*(k1*X.^2 + k2*Y.^2);subplot(3,3,8)surf(X,Y,Z)title ('Synform (cylindrical): k1 > 0, k2 = 0')

% Basin: k1 > 0, k2 > 0k1 = 2; k2 = 1;Z = 0.5*(k1*X.^2 + k2*Y.^2);subplot(3,3,9)surf(X,Y,Z)title ('Basin: k1 > 0, k2 > 0')

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GG303 Lecture 28 11/26/07 10

Stephen Martel 28-10 University of Hawaii

B “Traditional” Fold terminology and classification

1 Hinge point: point of local maximum curvature.

2 Hinge line: connects hinge points along a given layer.

3 Axial surface: locus of hinge points in all the folded layers.

4 Limb: surface of low curvature.

5 Cylindrical fold: a surface swept out by moving a straight line

parallel to itself

a Fold axis: line that can generate a cylindrical fold

b Parallel fold: top and bottom of layers are parallel and layer

thickness is preserved (assumes bottom and top of layer

were originally parallel).

c Curved parallel fold: curvature is fairly uniform.

d Angular parallel fold: curvature is concentrated near the hinges

and the limbs are relatively planar.

e Non-parallel fold: top and bottom of layers are not parallel; layer

thickness is not preserved (assumes bottom and top of

layer were originally parallel). Hinges typically thin and limbs

thicken.

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GG303 Lecture 28 11/26/07 11

Stephen Martel 28-11 University of Hawaii

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GG303 Lecture 28 11/26/07 12

Stephen Martel 28-12 University of Hawaii

E Non-cylindrical fold example: domeB Anticlines, synclines, antiforms, synforms, and monoclinesB Kinks: folds with sharp, angular hinge regionsC "Tightness" of foldsD Classification by orientation of axial plane and plunge of fold axisE Symmetrical folds vs. asymmetrical folds

III Ramsay's classification scheme; single-layer folds in profileA Relates the curvature of the inner and outer surfaces of a fold.B Dip isogons: lines that connect points of equal dip

Fold class Curvature (C) CommentI Cinner > Couter Dip isogons converge

1A Orthogonal thickness onlimbs exceeds thickness athinge; uncommon

1B Parallel folds1C Orthogonal thickness on

limbs is less than thickness athinge

2 Cinner = Couter Dip isogons are parallelClass 2 = similar folds)

3 Cinner < Couter Dip isogons are divergeClass 1C (or 1B) folds commonly are stacked with class 3 folds.

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GG303 Lecture 28 11/26/07 13

Stephen Martel 28-13 University of Hawaii

IV Mechanical interaction of folds (See Fig. 9-57 of Suppe)A Layers far apart will not interact as they foldB Layers of similar properties that are close together will tend to fold as

a single foldC Layers "near" each other will interact

V Superposition of foldsA Can produce highly complicated geometriesB Common in metamorphic rocksC "Demonstration" of z- and s- folds (parasitic)

References

Compton, R.R., 1962, Manual of Field Geology: Wiley, New York, 378 p.

Gauss, K.F., 1827, General Investigations of Curved Surfaces: Edited with an

Introduction and Notes by Peter Pesic, Dover Books, New York, 144 p.

Lisle, R.J., and Toimil, N.C., 2007, Defining folds on three-dimensional

surfaces: Geology, v. 35, p. 519-522.

Mynatt, I., Bergbauer, S., and Pollard, D.D., 2007, Using differential geometry

to describe 3-D folds: Journal of Structural Geology, v. 29, p. 1256-1266.

Ragan, D.M., 1973, Structural geology: Wiley, New York, 208 p.

Ramsay, J.G., 1967, Folding and fracturing of rocks: McGraw-Hill, New York,

568 p.

Ramsay, J.G., and Huber, M.I., 1987, The techniques of modern structural

geology, volume 2: Folds and fractures: Academic Press, New York, 700 p.

http://en.wikipedia.org/wiki/Paraboloid

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GG303 Lecture 28 11/26/07 14

Stephen Martel 28-14 University of Hawaii

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Stephen Martel 28-15 University of Hawaii

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Stephen Martel 28-16 University of Hawaii

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Stephen Martel 28-17 University of Hawaii

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Stephen Martel 28-18 University of Hawaii