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The AAPG/Datapages Combined Publications Database
Houston Geological Society Bulletin
Abstract
STUDENT POSTER SESSION COMPETITION
Abstract: Mechanical
Models
of
Compressional Fault-Related Folds:
Controls on Deformation
and Internal Stress
Models
of
Compressional Fault-Related Folds:
Controls on Deformation
and Internal StressBy
Plane strain finite element
models
were used to investigate
how rock properties and layering control the sequential
development of fault-bend and fault propagation folds and
their internal stress state. The
models
use an elastic-plastic
rheology, displacement boundary conditions, and special
elements for frictional surfaces and fault tips. Layer deformation
and stress and strain distribution are computed at
discrete intervals of displacement for
models
that vary ramp
angle (10°-30°), layer thickness (500-1000 m.), and material
properties (e.g., yield stress, 50-200 MPa). A comparison of
our results to those based on geometric
models
illustrates
the strengths and weaknesses of each method for modeling
the deformation and stress state in fault-related folds.
The results for fault-bend folds are: 1) fold shape and
amplitude are little affected by material contrasts between
layers
; 2) fold geometries are smooth rather than kinked; 3)
the strength of the layer at the ramp controls stress and
strain distribution in the structure; 4) deformation is very
sensitive to the relative magnitudes of the frictional coefficient
and yield stress. In fault propagation folds, the
stress state results from superposition of fault tip stresses
and the shortening and buckling of the upper plate. The
mechanical
models
of fault-bend and fault propagation folds
do not reproduce the distinct dip domains predicted by
geometric
models
. However, the external fold shape is
similar to that predicted by geometric
models
involving
flexural slip. Flattening of the fault ramp and foot wall
deformation with increasing displacement in finite element
models
accounts for the smooth profile of these folds.
End_Pages 54 and 55---------------