a study of the dynamic response of a fractured tunnel to plane waves pei-cheng xu swri,...
TRANSCRIPT
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A STUDY OF THE DYNAMIC RESPONSE OF A FRACTURED TUNNEL
TO PLANE WAVES
Pei-cheng Xu
SwRI, SanAntonio,TexasSept. 7, 2000
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x
z
y
vacuum
host medium
tunnel
fracture
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Objectives of Study
• Develop a computational tool to predict dynamic response of a fractured tunnel to plane waves
• Investigate the effects of fracture properties on the displacement and stress field, using the slip interface model
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Method of Approach:The Boundary Integral Equation Method
• Discretize the boundary only
• Suitable for an unbounded host medium
• Additional efficiency when large numbers of sources and detectors are involved
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)()()(),()()(2
1 0 dSnuTuu iik
ijkk
The Boundary Integral Equation
}{}{][ 0u = u M
Solve BIE for boundary displacements
Traction free
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x
The Boundary Integral
)()(),()()( 0 dSnuxTxuxu iik
ijkk
)(2,,);(3,1,,, SHkjiSVPkjix
* Displacement off boundary: direct integration
* Stresses: Hooke’s law / differentiation
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jkisikjs
ijkspkijkpk
ij
rkHrkH
rkHrkHrkHiTs
,0,0
,002
,02
)]([)]([
)]()([)]()[1(4 22
Green’s Functions and Associated Stresses
iksikspkik rkHrkHrkHGiS
)()]()([4 0,0012
Uniform, isotropic
Layered (fractured)
dkxikxkFI )](exp[|]|exp[)( 1133
)Re(||22 kkkk
)Re(||22 kkkki
x1
x3 3
1
r
x
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wh b
a
1
2
3 4 5
6
7
8
1
2
3
4 5
6 7 8
9
10
1112
Boundary Mesh
Basic type of elements
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n1 columns
n 2 ro
ws
detector
fracture
tunnel
Detector Mesh
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The Slip Model of Fracture
n
s
s
sss
n
nnn
sss
nnn
Kuu
Kuu
)2(
Stiffnesscoefficients
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The Stiffness Calculation in theE-Model of Fracture
Kn(
Virtual thicknessin BIE
Slip line stiffness
Combined stiffness across the slip line =
1Kn
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I-model
ks
kn
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E-model
ks
kn
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Fractured host medium
I-model
ks kn
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Uniform host medium
E-model
ks kn
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Comparison of I-Model and E-Model of Fracture
• Zero thickness• Infinite length• Longer computer time• Numerically unstable
when elements are small
• No mesh on the fracture
• Finite thickness• Finite length• More efficient• Numerically unstable
when virtual thickness is too small
• Mesh on the fracture
I-Model E-Model
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Features of the Current Program
• Predicts displacements and stresses on the boundary and in the surrounding area
• Handles multiple sources and a large number of detectors efficiently.
• Two alternative slip interface models for the fracture: Implicit and Explicit.
• A user friendly interface for input data.
• A variety of display means of output data, including deformed meshes, hoop stresses on the boundary, and quiver and contour plots of field stresses.
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Limitations of the Current Program
• The Implicit slip model encounters numerical instability when boundary elements are small.
• The Explicit slip models works but the input value of virtual thickness may depend on the frequency and geometry.
• Needs a user friendly output interface.
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= +
1 1/2 1/21/2 -1/2
Decomposition based on Symmetry
nn n/2n/2 n/2n/2
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Frequency loop
Symmetry loop
Incidence loop
Boundary mesh
Decomposed boundary Matrix
Input
Decomposed boundary response w.o. tunnel
Decomposed boundary response w. tunnel
Detector mesh
Total boundary response
PROGRAM STRUCTURE
Detector response Output files
Solving equation
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SUBROUTINE LAYOUT
IN P U T M E S H TM E S H N E T
G R E E NG R E E N S
IN C D N TIN C S Y M
COEFF
CGARCFAR
M A TD O M G R E E N 0
CSUM
W A V E
O M E G A
S O U R C E
B A N D
F U L L
G L O B A L
L O C A TEL O C A TE 3
S O R T
G R E E N Z D IV ID E IN S E R T M C C F S C
S TM S C 2
S F S C
S TM 2
IN TX R
M C C IN T
C H E B S HC H E B S H 3
TC N P P O S ITIO N
F ITA IL R O TA TR O TA T3
E X P F C N C O N F C T
R E C IN TR E C IN T3
F ITIN T
G R E E N SG R S N 2
IN TG F 0IN TG F 0 2
G F IK XG F IK X 2
G A U S S 4
IN TL IN
W E IG H T
M A TR IXM A TS Y M
C E Q S L V
N O R M P L O T R A D IP L O T
P R B IE B
COEFF
CGPARRCFPAR
IN TG F SIN TG F S Q
G F IK SG F IK S Q
IN TL IN
W E IG H T
M F IE L D SM F IE L D S Q
CVF
G R E E N P
CSUM
G R E E N S
R E S U L TS D E F O R M M O H R H O O K E
M A IN
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INPUT FILESparalst2.h ------------ basic numeric settingstunnel.in ------------ general input data
OUTPUT FILES tunnel.out ----------- general output
mesh.dat ------------ coordinates of boundary nodesmeshr.dat ----------- coordinates of Gaussian points on
boundarymeshnet.dat -------- coordinates of network nodes
bform.dat ------------ deformation of boundary meshform.dat ------ deformation of network nodes
ub.dat ---------------- nodal displacements on boundarybplot.dat ------------- nodal stress on boundary for plottingps.dat ---------------- principal stresses at network nodescross.dat ------------ principal stresses at network nodes for
plotting
I/O Files
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10 2
4
6 7 8
53
Geometry ofCavities orInclusions
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9
12 13 14
15 16 17
1011
Geometry ofCavities orInclusions
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Select type of medium structureCavityFree solidHost & inclusion
Select type of geometry
Select type of dynamic sourceConcentrated line force in the inclusion Concentrated line force in the host domainIncident plane P-wave in the host domainIncident plane SV-wave in the host domainIncident plane SH-wave in the host domain Pressure center in the host domain
Torsion center in the host domain
Determine boundary conditionFree surfaceFixed surfaceFree surface & internal slip interfaceFixed surface & internal slip interface
Input Parameters (1)
Enter maximum number of nodes
Is the geometry symmetric?
Select type of medium
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Number of sources 2
Are the detectors aligned in a network? NY
If no, then enter number of individuallyspecified detectors 10
Number of frequencies 1
Choose one of the following calculation options:BIE solution onlyMesh without solution
Choose the component of response to plot along the boundaryHorizontal or radial displacementVertical or tangential displacementRadial normal stressTangential shear stressTangential normal (hoop) stress
Input Parameters (2)
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Is the geometry symmetric? Y/N
Are you using an Implicit (I)or Explicit (E) model of fracture? I/E
Parameters of fracture for the Explicit Model (used when nfrct=0 and id3=3)Virtual normal thickness oft fracture [m](suggested range=0.1-0.5) 0.2
Virtual shear thickness oft fracture [m](suggested range=0.1-0.5) 0.2
Define dividing value of weak and strong slip coefficient(suggested range = 0.8-2.0 ) 1.0
Input Parameters (3)
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Parameters controlling element and mesh sizesEnter number of elements per wavelength(suggested range=2-5) 2.0
Define far field in terms of number of wavelengths(suggested range=2-5) 2.0
Parameters associated with physical properties of the mediumSource domainDensity P-wave vel. S-wave vel. Q Q[g/cm**3] [km/s] [km/s] (P-wave) (S-wave)1.00 1.754 1.200 100.0 50.0
The other domain (used only when med.=2 but must be present for all cases)Density P-wave vel. S-wave vel. Q Q[g/cm**3] [km/s] [km/s] (P-wave) (S-wave)0.80 1.500 1.000 100.0 50.0
Input Parameters (4)
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Parameters associated with dynamic sourcesEnter x-coordinate of sources or reference point in the order of their labels [m] 0.00 0.00Enter z-coordinate of sources or reference point in the order of their labels [m] 0.00 1.00
Components of dynamic sourcesEnter x-component of force [Newton/m] or plane wave in the order of labels of dynamicsources 0.00 1.00Enter z-component of force [Newton/m] or plane wave in the order of labels of dynamicsources 1.00 0.00Enter y-component of force [Newton/m] or plane wave in the order of labels of dynamicsources 0.00 0.00
Input Parameters (5)
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Parameters associated with the of detectors aligned in a networkEnter number of divisions in direction parallel to the fracture in the network of detectors 20
Enter number of divisions in direction perpendicular to the fracture in the network of detectors 20
Enter minimum value of rotated x-coordinate in the network of detectors 4.0
Enter maximum value of rotated x-coordinate in the network of detectors 4.0
Enter minimum value of rotated z-coordinate in the network of detectors 2.0
Enter maximum value of rotated z-coordinate in the network of detectors 6.0
Parameters associated with frequencyEnter minimum value of frequency [kHz] 0.25
Enter maximum value of frequency [kHz] 0.50
Enter increment value of frequency [kHz] 0.25
Input Parameters (6)
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Welded Half Spaces
x
y
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2
x
y
Circular
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Round-head Semi-infinite Layer
x
y
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h
Infinite Layer
x
z
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12
Pinch-out Layer
x
z
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h
h2
h1
2
1
Split Layer
xz
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h
w
d
Wash-out Layer
xz
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2
1
12h2
h1
Faulted Layer 1
z
xd
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h2
h1
Faulted Layer 2
x
zd
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w
h 0 0
Rounded Block/Slot
x
y
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w
h
Dome
x
z
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Loaf Shaped
2 2
1
3
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Half Space with Semi-Circular Notch
x
z
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Cracked Circular Hole
w w
2 x
z
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Half Spaces Divided by Slip Line
x
z
s n
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Circular Hole Crossed by Slip Line
h x
z
ns
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w
h
h1
Dome Crossed by Horizontal Slip Line
x
z
s n
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Lahey FORTRAN 95
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