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Geomatics, Natural Hazards and Risk

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A stochastic model for earthquake slip distributionof large events

S.T.G. Raghukanth & S. Sangeetha

To cite this article: S.T.G. Raghukanth & S. Sangeetha (2016) A stochastic model for earthquakeslip distribution of large events, Geomatics, Natural Hazards and Risk, 7:2, 493-521, DOI:10.1080/19475705.2014.941418

To link to this article: http://dx.doi.org/10.1080/19475705.2014.941418

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Published online: 01 Aug 2014.

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A stochastic model for earthquake slip distribution of large events

S.T.G. RAGHUKANTH* and S. SANGEETHA

Department of Civil Engineering, Indian Institute of Technology, Madras 600036, India

(Received 13 January 2014; accepted 1 July 2014)

This paper presents a stochastic model to simulate spatial distribution of slip on

the rupture plane for large earthquakes (Mw> 7). A total of 45 slip models

coming from the past 33 large events are examined to develop the model.

The model has been developed in two stages. In the first stage, effective rupture

dimensions are derived from the data. Empirical relations to predict the rupture

dimensions, mean and standard deviation of the slip, the size of asperities and

their location from the hypocentre from the seismic moment are developed. In the

second stage, the slip is modelled as a homogeneous random field. Important

properties of the slip field such as correlation length have been estimated for the

slip models. The developed model can be used to simulate ground motion for

large events.

1. Introduction

Large-magnitude earthquakes (Mw> 7) occur frequently in active regions like Hima-

laya and northeast India. Even in the Indian shield, Gujarat region also experiences

such large events. Due to their intensity and the geographical extent of the damage,large earthquakes pose the highest risk to the society. The 2001 Kutch earthquake

(Mw D 7.7) caused severe fatalities and affected the economy of the Gujarat region.

Recently, Raghukanth (2011) developed the earthquake catalogue for India and

ranked the 48 urban agglomerations in India based on seismicity. The maximum pos-

sible magnitude in a control region of radius 300 km around the 24 urban agglomera-

tions lies in between Mw D 7.1 and Mw D 8.7. This necessitates the estimation of the

seismic input (design ground motion) in an accurate fashion for such large events to

reduce the damages to structures. Cases where the recorded strong motion data arenot available, the source mechanism models where in the earthquake slip distribution

and medium properties can be modelled analytically are preferred to simulate ground

motion for such large events. These models require the earthquake forces to be speci-

fied in terms of spatial distribution of slip on the rupture plane. Hartzell et al. (1999)

and Raghukanth and Iyengar (2009) have demonstrated that surface level ground

motions can be computed for an Earth medium for a given slip distribution on the

rupture plane. These models provide reliable ground motion predictions if the fault

and its slip distribution are known. Specifying the slip distribution on the ruptureplane for future events is the most challenging problem in mechanistic models. To

address this issue, there have been efforts to obtain spatial distribution of slip on the

rupture plane by inverting ground motion records of the past earthquakes (Hartzell

& Heaton 1983; Hartzell & Liu 1995; Ji et al. 2002; Raghukanth & Iyengar 2008).

*Corresponding author. Email: [email protected]

� 2014 Taylor & Francis

Geomatics, Natural Hazards and Risk, 2016

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Several such finite slip models are available in various journals and research reports.The obtained slip distribution of past events exhibit higher complexity which can be

modelled by stochastic approaches only. These techniques require very few parame-

ters to characterize the slip field. Much effort has been made by the previous investi-

gators in this direction (Somerville et al. 1999; Mai & Beroza 2002; Lavall�ee et al.

2006; Raghukanth & Iyengar 2009; Raghukanth 2010). Without going into the

details regarding time-dependent stresses on the fault plane, few parameters have

been identified from the slip distribution of past events. The slip distribution is mod-

elled as a random field with a specified power spectral density (PSD). A total of 15slip distributions with the magnitude of the events ranging from 5.66 to 7.22 have

been analysed by Somerville et al. (1999). The total number of large events included

in the database is two. Mai and Beroza’s (2002) slip database includes 11 large

events. This puts a serious limitation on the random field model developed by the

previous investigators for simulating slip distribution for large events. Due to advan-

ces in instrumentation, several large events have been recorded by the broadband

instruments operating around the world. These data have been processed and slip

models for 45 large events are available in the literature. Since large events are of con-cern to engineers, it would be interesting to examine these slip distributions. In this

paper, stochastic characterization of slip distribution is explicitly developed for large

events. Important properties of the random field are estimated from the PSD of slip

distribution. Empirical equations for estimating the slip field from magnitude are

developed in this paper.

2. Slip database of large events

Inversion for earthquake sources is fundamental to understand the mechanics of

earthquakes. The extracted slip models can be used to understand the damages in the

epicentral region. Much effort has been made by seismologists in developing meth-

ods to extract slip distribution on the rupture plane from ground motion records.

After the occurrence of a large event, the Incorporated Research Institutions for Seis-

mology data management centre reports the broadband velocity data recorded by

the Global Seismic Network (GSN). The preliminary earthquake slip distribution isdetermined from this data by several research groups. In case of local strong motion

data, global positioning system and ground deformation measurements become

available, these records are combined with the GSN data to obtain the spatial distri-

bution of slip on the rupture plane. Several such slip maps for large events are avail-

able in the published literature. In this study, the source models of large events,

reported by Chen Ji (http://www.geol.ucsb.edu6 faculty6 ji6 ) and tectonics observa-

tory, California Institute of Technology (http://www.tectonics.caltech.edu6 ), are

used to develop the model. The methodology for obtaining the rupture models isbased on Ji et al. (2002), and is uniform for all the events. The compiled database

from these two website consists of 45 rupture models coming from 33 earthquakes in

the magnitude range of Mw 7�9.15 from various seismic zones in the world. These

slip maps have been derived by the inversion of low-pass filtered ground motion

data. The location of the epicentre, average slip, total seismic moment, faulting

mechanism and dimensions of the fault plane of the 45 slip models are reported in

tables 1 and 2. The slip database consists of 36 thrust events, 2 normal faulting mech-

anism and 7 strike-slip earthquakes. The epicentres of these large events along with

494 S.T.G. Raghukanth and S. Sangeetha

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Table1.

Slipmodelsusedin

thisstudy.

S.

no.

Location

Date

(m6d

6yy)

Latitude(�)

Longitude(�)

Mech

(RV6N

6SS)

Mw

M0

(Nm)

Ref.

1KurilIslands

10604694

43.77

147.32

RV

8.36

3.89EC0

21

1

2Chile

07630695

¡23.34

¡70.29

RV

8.14

1.82EC0

21

1

3KurilIslands

12603695

44.66

149.30

RV

7.81

5.82EC0

20

1

4New

BritianRegion

11617600

¡05.50

151.78

RV

7.5

2.00EC0

20

1

5Bhuj,India

01626601

23.42

70.23

RV

7.6

2.82EC0

20

2

6Peru

06623601

¡16.26

¡73.64

RV

8.4

4.47EC0

21

1

7NorthSumatra

03628605

02.09

97.11

RV

8.68

1.17EC0

22

1

803628605

02.09

97.11

RV

8.5

6.31EC0

21

2

9NorthernCalifornia

06615605

41.29

¡125.95

SS

7.2

7.10EC0

19

2

10

India

07624605

07.92

92.19

SS

7.25

8.40EC0

19

1

11

Honshu,Japan

08616605

38.28

142.04

RV

7.19

6.80EC0

19

1

12

Kashmir,Pakistan

10608605

34.54

73.59

RV

7.6

2.82EC0

20

2

13

10608605

34.54

73.59

RV

7.64

3.24EC0

20

1

14

SouthernJava,Indonesia

07617606

¡09.28

107.42

RV

7.9

7.94EC0

20

2

15

KurilIslands

11615606

46.59

153.27

RV

8.3

3.16EC0

21

2

16

KurilIslands

01613607

46.24

154.52

N8.1

1.59EC0

21

1

17

01613607

46.24

154.52

N8.1

1.59EC0

21

2

18

SolomonIslands

04601607

¡08.47

157.04

RV

8.1

1.59EC0

21

1

19

Pisco,Peru

08615607

¡13.39

¡76.60

RV

81.12EC0

21

2

20

PagaiIsland,Indonesia

09612607

¡02.62

100.84

RV

7.9

7.94EC0

20

2

21

Benkulu,Indonesia

09612607

¡04.44

101.37

RV

8.5

4.47EC0

21

2

22

09612607

¡04.52

101.38

RV

8.5

4.47EC0

21

1

23

Kepulauan

09612607

¡02.62

100.84

RV

7.94

9.12EC0

20

1

24

Antofagasta,Chile

11614607

¡22.25

¡69.89

RV

7.81

5.82EC0

20

1

( continued

)

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Table1.

(Continued

)

S.

no.

Location

Date

(m6d

6yy)

Latitude(�)

Longitude(�)

Mech

(RV6N

6SS)

Mw

M0

(Nm)

Ref.

25

11614607

¡22.25

¡69.89

RV

7.78

3.98EC0

20

2

26

Sim

eulue,Indonesia

02620608

02.77

95.96

RV

7.4

1.41EC0

20

2

27

Tibet,China

03620608

35.49

81.47

N7.14

5.80EC0

19

1

28

EastSichuan,China

05612608

31.00

103.32

SS

7.9

7.94EC0

20

2

29

05612608

31.00

103.32

RV

7.97

1.01EC0

21

1

30

Sulawesi,Indonesia

11616608

01.27

122.1

RV

7.3

1.00EC0

20

2

31

Padang,Indonesia

09630609

¡00.72

99.87

SS

7.6

2.82EC0

20

2

32

09630609

¡00.72

99.87

RV

7.6

2.82EC0

20

2

33

Vanuatu

Islands

10607609

¡13.05

166.18

RV

7.6

2.82EC0

20

2

34

Haiti

01612610

18.44

¡72.57

SS

73.50EC0

19

2

35

Maule,Chile

02627610

¡36.12

¡72.90

RV

8.9

2.51EC0

22

1

36

02627610

¡35.84

¡72.72

RV

8.8

1.78EC0

22

2

37

ElMayor-Cucapah,Mexico

04604610

32.30

¡115.28

SS

7.2

7.10EC0

19

2

38

Kepulauan,Indonesia

10625610

¡3.480

100.12

RV

7.82

6.03EC0

20

1

39

Honshu,Japan

03609611

38.44

142.84

RV

7.4

1.41EC0

20

1

40

Honshu,Japan

03611611

38.32

142.34

RV

9.1

5.01EC0

22

1

41

03611611

38.32

142.34

RV

9.1

5.01EC0

22

1

42

03611611

38.10

142.86

RV

9.1

5.01EC0

22

1

43

03611611

38.10

142.86

RV

9.1

5.01EC0

22

1

44

03611611

38.10

142.80

RV

93.55EC0

22

2

45

Turkey

10623611

38.72

43.51

RV

7.13

5.60EC0

19

1

Note:1:www.geol.ucsb.edu;2:www.tectonics.caltech.edu;Faultingmechanism:RV�

reverse,SS�

strikeslip,N

�norm

al.

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Table2.

Sourcedim

ensionsandorientationofthefaultplane.

Length,

LWidth,

WMeanslip,

<D>

Subfaultsize,

dx

SubfaultSize,

dz

S.no.

(Km)

(Km)

(cm)

(Km)

(Km)

Strike(�)

Dip

(�)

Rake(�)

Area

(1.0EC0

5�sq.km)

1255

121

234.87

15

11

54

76

123.4

0.309

2240

156

96.32

15

13

418

90.9

0.374

3168

112

67.57

14

14

226

18

100.3

0.188

4168

100

27.68

12

10

240

32

63.5

0.168

565

41.6

357.89

55.2

82

51

75.7

0.027

6300

190.4

173.49

15

13.6

308.5

15

54.2

0.571

7380

260

255.67

20

20

326

8117.2

0.988

8416

320

119.38

16

16

325

10

90.1

1.331

9102

35

67.19

65

221

88

362.3

0.036

10

98

42

67.35

77

118

80

198.7

0.041

11

112

72

14.71

88

24

70

90.2

0.081

12

76

35

294.34

43.5

3206343

29

102.9

0.021

13

126

54

175.09

99

331

29

124.9

0.068

14

240

162.5

152.82

12

12.5

289

10

83.5

0.390

15

315

132

173.59

15

12

220

15

99.4

0.416

16

200

35

702.21

85

42

57.89

246.2

0.070

17

224

40

356.32

85

42

58

¡97.9

0.090

18

300

80

147.38

15

10

305

25

85.4

0.240

19

192

210

58.14

12

10

318

06620630

59.4

0.403

20

240

190

36.93

12

10

323

15

96.8

0.456

21

400

368

55.99

16

16

324

15

94.4

1.472

22

560

159.5

90.23

20

14.5

323

12

110.1

0.893

23

312.5

130

39.37

12.5

10

319

19

98.1

0.406

(continued

)

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Table2.

(Continued

)

Length,

LWidth,

WMeanslip,

<D>

Subfaultsize,

dx

SubfaultSize,

dz

S.no.

(Km)

(Km)

(cm)

(Km)

(Km)

Strike(�)

Dip

(�)

Rake(�)

Area

(1.0EC0

5�sq.km)

24

375

200

21.89

15

8355.08

16.56

95.7

0.750

25

162

126

87.95

99

520

85.6

0.204

26

152

112

15.27

88

302

790.5

0.170

27

140

45

33.21

10

9206

48

287.3

0.063

28

260

28

376.12

10

4229

33

136.8

0.073

29

315

40

278.51

15

5229

33

120.1

0.126

30

120

56

45.27

84

93

22

88.1

0.067

31

54

45

158.25

65

193

58

44.2

0.024

32

48

45

177.76

65

72

51

122.2

0.022

33

91

60

87.34

75

346

40

59.7

0.055

34

45

22.5

144.93

32.5

83625766

90

70655645

34.9

0.010

35

260

187

405.48

13

17

17.5

18

113.3

0.486

36

570

180

229.28

30

15

18

18

108.6

1.026

37

171

21

93.60

33

35563126131

45675660

¡6.3

0.036

38

270

100

72.51

15

10

322

7.5

99.7

0.270

39

171

104

47.62

88

190

11

80.4

0.083

40

475

200

1219.88

25

20

199

10

67.2

0.950

41

475

200

1219.88

25

20

198

10

67.2

0.950

42

475

200

1219.88

25

20

198

10

67.2

0.950

43

475

200

1254.31

25

20

198

10

67.1

0.950

44

625

280

782.86

25

20

201

989.5

1.750

45

45

45

90.39

55

248

45

65.1

0.020

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plate boundaries as reported by Bird (2003) are shown in figure 1. Slip fields of some

large earthquakes are shown in figure 2(a)�(d). It can be observed that the slip distri-

butions exhibit high complexity which cannot be modelled through simple mathe-matical functions. Although the slip is continuous, the fault geometry for Kashmir

and Mexico events is not planar. The source model of Mexico event consists of slip

distribution on four planes, whereas Kashmir event consists of two rupture planes.

3. Scaling laws for source dimensions

The first step in characterizing the slip models is to understand the relationship

between magnitude or seismic moment and the rupture dimensions. These relations

are fundamental to develop source models for simulating ground motions due to

large events. In figure 3, the length, width and area of the fault plane as reported

in the source inversion are shown as a function of seismic moment. The mean value

of the slip is estimated from its spatial distribution on the rupture plane and its varia-

tion with seismic moment is shown in figure 3. In the same figure, a straight line of

the form

log10ðY Þ ¼ C0 þ C1logðM0Þ (1)

where Y is the source dimension, is also fitted to the data. The regression constants

for L, W, D and fault area are reported in table 4 along with the standard error. It

can be observed that the slope C 1 for all the four parameters lies in between 0.28 and

0.55, respectively. The theoretical relation between seismic moment (M0) and the

source dimensions is given by (Aki & Richards 1980)

M0 ¼ mLWD (2)

where L andW are the length and width of the fault andD is the average slip. m is the

rigidity of the medium surrounding the fault. If stress drop remains constant,

increase in the seismic moment occurs due to proportionately equal changes in L , W

Figure 1. Large earthquakes used in this study (lines�plate boundaries from Bird (2003)).

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Figure 2. (a) Slip distribution of 2008 Kashmir earthquake (Mw 7.6). (b) Slip distribution of2010 El Mayor-Cucapah, Mexico earthquake (Mw 7.2). (c) Slip distribution of 2010 Indonesiaearthquake (Mw 7.82). (d) Slip distribution of 2010 Maule, Chile earthquake (Mw 8.9).

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and average slip D . The self-similar scaling can be expressed as M0 / L 16 3, M0 / W16 3, M0 / (LW )26 3 and M0 / D 16 3. Assuming the slope from the self-similar scaling,

the intercept can be found from the data. The obtained empirical equation assuming

self-similarity is shown in figure 3 along with the data. The self-similar scaling equa-

tions are reported in table 5 along with the standard error. The obtained slope from

the data (C1) for all the quantities is of the same order indicating self-similar scaling.

It can be observed that the source dimensions linearly increases with increasing seis-

mic moment for large events.

3.1. Effective source dimensions

In earthquake source inversion, fault dimensions are generally chosen large to map

the entire rupture. It can be observed from figure 2 that slip along the edges of the

rupture plane is zero or very small compared to the mean slip. In such cases, the

Figure 3. Source dimensions and mean slip as a function of seismic moment: (a) area of therupture plane versus moment; (b) rupture length versus moment; (c) rupture width versusmoment; (d) mean slip versus moment.

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length and the width of the reported slip models will overestimate the true rupturedimensions. Estimating the exact source dimension from the slip distribution is diffi-

cult. To circumvent this problem, there have been techniques developed based on

empirical approaches. Somerville et al. (1999) defined the rupture dimensions based

on the slip distribution. If the slip distribution along the edges of the fault is 0.3 times

less than the average slip, the entire row or the column is removed from the rupture

distribution. Mai and Beroza (2000) defined the effective source dimensions based on

autocorrelation function. To estimate the effective length and width, marginal slip

distributions are derived by summing the slip in both the along-strike and down-dipdirections. The autocorrelation function is estimated and the width of this function is

computed as (Bracewell 1986)

Wa ¼ 1

D�Dj0

Z 1

¡1D�Ddx (3)

where Wa is the autocorrelation width and � is the convolution operator. The effec-

tive length and width of the rupture plane are estimated from the marginal slip distri-

bution in along- strike and down-dip directions. In a similar fashion, effective lengthand width have been estimated for all the slip models. These are reported in table 3

for all the 45 slip models. In figure 4, a comparison between the effective area and

the area of fault dimensions used in the earthquake source inversion is shown. The

ratio between effective dimensions to original dimensions has been estimated. The

ratio between effective length to original length lies in between 0.51 and 0.95 with a

median value of 0.74. In down-dip direction, the median change in width is 0.76 and

it lies in between 0.43 and 0.96 for all the 45 rupture models used in this analysis. The

effective area of all the events lies in between 24% and 88% of the original sourcedimensions. Empirical equations to predict effective source dimensions from seismic

moment are derived from the data. The coefficients are reported in table 4. The fitted

equations are shown along with the data in figure 5. The self-similar scaling relations

by constraining the slope are also shown in figure 5. The effective source dimensions

increase with increase in the seismic moment. Since the effective area is less than the

original source dimensions, the slip on the fault plane has to be increased to conserve

the seismic moment. The average effective slip variation with moment is shown in

figure 5(d). The standard deviation around the mean value also increases withincrease in the seismic moment.

4. Asperities on the rupture plane

After deriving the equations for estimating the source dimensions, the next step is to

understand the regions of concentration of large slip relative to the mean slip on therupture plane. These regions are known as asperities. There is no guideline available

to determine the threshold value of slip to define an asperity. The approaches in the

literature have been empirical and based on personal judgement. Somerville et al.

(1999) define asperities as rectangular regions whose average slip is 1.5 times more

than the mean slip on the entire rupture plane. In this study, the approach of Mai

et al. (2005) based on the ratio of slip distribution on the rupture plane to the maxi-

mum slip is used to define asperities. The subfaults on which the ratio lies in between

0.33 � D6 Dmax � 0.66 are taken as large asperity. The regions where the ratio

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Table 3. Effective source parameters.

Leff Weff Aeff Deff s (D)

S. no. (Km) (Km) 1.0EC04 � sq.km 1.0EC03�(cm) (cm)

1 184.5 95.9 1.7706 0.4491 243.10

2 192.4 121.4 2.3368 0.2934 96.24

3 132.1 89.3 1.1794 0.1206 58.34

4 99.9 74.6 0.7452 0.0679 30.42

5 43.6 36.7 0.1605 0.7798 347.90

6 175.0 166.6 2.9151 0.1297 186.86

7 302.8 190.2 5.761 0.1531 273.07

8 263.3 175.8 4.6315 0.6073 200.46

9 79.6 22.2 0.177 0.0405 77.72

10 52.3 23.2 0.1215 0.0661 106.79

11 56.9 36.1 0.2056 0.0622 27.07

12 60.4 28.6 0.1729 0.6137 254.38

13 96.6 34.8 0.3364 0.1157 181.95

14 221.5 154.9 3.4333 0.0649 78.77

15 281.2 123.6 3.4772 0.2997 103.61

16 182.6 33.3 0.6095 0.8065 455.48

17 173.4 27.1 0.4712 0.1395 339.42

18 241.8 76.1 1.8412 0.1099 97.42

19 100.1 101.1 1.0124 0.3732 136.66

20 125.7 96.2 1.2096 0.0001 79.70

21 220.3 157.7 3.4759 0.0003 134.75

22 353.0 146.5 5.1724 0.2191 92.36

23 193.4 105.4 2.0386 0.0142 54.57

24 230.9 137.9 3.184 0.1063 39.41

25 153.9 84.5 1.3019 0.1912 75.16

26 84.4 77.1 0.6507 0.0001 23.65

27 115.2 27.6 0.3182 0.0188 36.40

28 191.7 24.3 0.4668 0.2003 361.89

29 243.6 30.6 0.7461 0.4845 250.51

30 90.3 32.4 0.2933 0.0675 58.52

31 39.7 32.0 0.1274 0.4502 153.47

32 37.3 34.3 0.1281 0.4564 154.06

33 77.3 43.3 0.3355 0.2337 90.63

34 37.5 17.4 0.0655 0.2378 114.97

35 178.5 178.6 3.1885 0.6108 321.43

36 483.6 170.2 8.236 0.2057 154.92

37 118.6 13.4 0.1596 0.0576 121.92

38 213.3 68.1 1.4518 0.0711 70.11

39 118.6 83.6 0.481 0.1587 48.62

40 282.4 162.5 4.5908 3.2795 1347.45

41 282.4 162.5 4.5908 3.2795 1347.45

42 282.4 162.5 4.5908 3.2795 1347.45

43 287.6 144.4 4.1549 1.8181 1526.18

44 484.7 194.3 9.4194 1.8136 764.28

45 29.2 36.2 0.1059 0.2992 93.10

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Figure 4. Comparison between effective and original rupture area.

Table 4. Scaling relations of slip models log10(Y) D C0 C C1 log10(M0).

Y C0 C1 s(e)

L ¡3.58 0.28 0.19

W ¡3.64 0.27 0.23

A ¡7.39 0.55 0.34

D ¡5.87 0.38 0.36

sD ¡5.49 0.36 0.31

Leff ¡3.52 0.27 0.19

Weff ¡4.34 0.29 0.21

Aeff ¡8.02 0.57 0.31

Deff ¡6.50 0.40 0.45

ALA ¡8.33 0.56 0.31

AVLA ¡6.75 0.47 0.27

ACA ¡7.45 0.53 0.29

RDmax ¡4.7 0.31 0.35

RLA ¡1.39 0.11 0.37

RVLA ¡3.97 0.24 0.41

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Figure 5. Effective source dimensions and effective mean slip as a function of seismicmoment: (a) area of the rupture plane versus moment; (b) rupture length versus moment;(c) rupture width versus moment; (d) mean slip versus moment; (e) standard deviation of slipversus moment.

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(D6 Dmax) is greater than 0.66 is defined as a very large asperity. A very large asperity

is always enclosed by large asperity. In figure 6, the area of very large asperity

(AVLA) and large asperity (ALA) are shown as function of seismic moment for all the

45 events. The combined area of asperities (ACA) is also shown in figure 6(c). It can

be observed that asperities increase with increasing seismic moment. Empirical equa-

tions between log(A) and log(M0) are fitted to the data and the constants are foundby regression analysis. These are reported in table 4 along with the standard error in

the regression. The large asperities occupy about 10%�55% of the effective rupture

area, whereas the area of very large asperities is about 2%�40% of Aeff for all the 45

events. The combined area of asperities lies in between 12% and 78% of the effective

area. It will be of interest to know how self-similar scaling relations model the data.

The self-similar scaling relations are derived by constraining the slope to be 26 3 and

the intercept is obtained from the regression on the data. It can be observed that the

area of very large asperities deviates from self-similarity, whereas large asperities arecloser to the self-similar relations.

Figure 6. Scaling of the size of asperities with seismic moment.

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4.1. Location of hypocentre and asperities

Another important aspect which affects the near-field ground motion is the location of

hypocentre and asperities on the fault plane. This information is important to under-

stand the crack propagation during the rupture which can be further used to developdynamic rupture models. The distance of the hypocentre from the edges of the fault in

along-strike (Hx ) and down-dip (Hz ) directions normalized by length and width of the

fault is computed for all the 45 slip models. Due to symmetry, the normalized distance in

along-strike direction (Hx ) lies in between 0 and 0.5, whereasHz lies in between 0 and 1.

Hx D 0 indicates that hypocentre is located on the edge of the fault, whereas Hx D 0.5

indicates the centre of the fault. Similarly,HzD 0 denotes the hypocentral location at the

top edge of the fault and Hz D 1 denotes the bottom edge of the rupture plane. These

non-dimensional quantities are shown in figure 7 as a function of magnitude. It can beobserved that Hx and Hz do not show any pattern with Mw. The histograms are also

shown in figure 7. The Hx is distributed with a mean of 0.30 and a standard deviation

0.13, whereas forHz, these two moments are 0.52 and 0.23, respectively. The hypocentre

is approximately located at the centre of the fault in down-dip direction.

To understand the relationship between the hypocentre and the location of the

asperity, the closest distance to the asperity from the hypocentre is determined from

the data. In figure 8, the variation of the closest distance to large and very large

asperities from hypocentre is shown as a function of seismic moment. The histogramsof these distances are also shown in the same figure. The closest distance increases

with increase in the seismic moment. Large asperities are located close to the hypo-

centre, whereas very large asperities are located at approximately 24 km from the

hypocentre. The regions of maximum slip are located approximately at a distance of

50 km from the hypocentre. Empirical equations between distance and moment are

derived from the data with and without constraining the slope, and constants are

reported in tables 4 and 5. Figure 9 shows the closest distance to asperities

Table 5. Scaling relations of slip models assuming self-similaritylog10(Y) D C0 C C1 log10(M0); C1 is fixed.

Y C0 C1 s(e)

L ¡4.70 0.33 0.19

W ¡5.03 0.33 0.24

A ¡9.74 0.67 0.36

D ¡4.87 0.33 0.37

sD ¡4.84 0.33 0.31

Leff ¡4.85 0.33 0.20

Weff ¡5.16 0.33 0.21

Aeff ¡10.02 0.67 0.32

Deff ¡5.16 0.33 0.45

ALA ¡10.54 0.67 0.33

AVLA ¡10.88 0.67 0.33

ACA ¡10.36 0.67 0.31

RDmax ¡5.47 0.33 0.35

RLA ¡6.02 0.33 0.42

RVLA ¡5.84 0.33 0.42

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Figure 7. Normalized hypocentre position in (a) along-strike and (b) down-dip directions.

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normalized by maximum distance to the farthest subfault on the plane, Rmax as a

function of moment magnitude. It can be observed that they do not show any pattern

with Mw. The histograms are also shown in the same figure. It is interesting to note

that asperities are not located randomly on the rupture plane but they lie close to thehypocentre.

5. Power spectral density (PSD)

The above empirical equations can be used to fix up the rupture dimensions, average

slip and location of hypocentre for a given seismic moment. However, to simulate

ground motion by source mechanism model requires complete slip distribution on

the rupture plane. One requires representation of the slip field in terms of mathemati-

cal functions. The previously derived equations provide information on the average

properties of the slip field. The possibility of representing the slip field in terms of

Figure 8. Scaling of the closest distance to asperities with seismic moment: (a) large asperity;(b) very large asperity; (c) location of maximum slip.

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simple mathematical expressions is ruled out due to the randomness in the derived

rupture models. It can be observed from figure 2 that the obtained slip component of

large events are erratic which can be attributed to randomness observed in ground

motion records. More number of parameters are required to characterize completelythe spatial distribution of slip. The only way to model the slip distribution is through

stochastic approaches where a few parameters are sufficient to explain the complex

data. The two striking features of the slip models are randomness and non-stationar-

ity in their spatial distribution. Assuming the slip as a homogeneous random field,

the spatial mean and standard deviation are computed for all the 45 slip models. For

estimating the further statistics, the slip field is standardized as

Dðx; zÞ ¼ Dðx; zÞ¡ hD isD

(4)

In second-order analysis, the variation of random field models at two different

locations is characterized either in space by an autocorrelation function or in the

Figure 9. Closest distances to asperities and Dmax normalized by maximum distance to thefarthest subfault on the plane.

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wave-number domain by a PSD. Assuming the slip field as ergodic, two-dimensionalPSD (S (kx,kz)) is obtained from the slip distribution as

Sðkx; kzÞ ¼����Z 1

¡ 1

Z 1

¡ 1Dðx; zÞ e¡ ikxx¡ ikzzdxdz

����2

(5)

where kx and kz are the spatial wave numbers. The obtained standardized slip field is

transformed into the two-dimensional wave-number domain using zero-padded gridsof size 1024 £ 1024 km. The Nyquist wave number in both the directions depends on

the size of the subfaults determined from the earthquake source inversion. It can be

observed from table 2 that the size of the subfaults is not uniform along the length

and width of the fault for all the 45 models. Hence the highest wave number for

which the slip model is valid will be different for all the events. The two-dimensional

PSD function computed from ‘equation (5)’ for Kashmir earthquake slip model

shown in figure 2(a) is shown in figure 10. A random field is known as isotropic, if

Figure 10. Two-dimensional power spectral density function for the slip model of Kashmirevent shown in figure 2(a).

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the correlation is independent of direction (Vanmarcke 1983). It can observed fromfigure 10 that the correlation structure is different in along-strike and dip-directions

indicating that the moment field is anisotropic. In figure 11, the PSD functions at

cross sections kx D 0 and kz D 0 are also shown. There are several theoretical two-

dimensional correlation functions available in the literature. Three correlation func-

tions widely used in literature are Gaussian, exponential and von Karman (Mai &

Beroza 2002). The expressions for the autocorrelation and PSD for these three ran-

dom field models are as follows:

Gaussian:

Rðzx; zzÞ ¼ e¡ z2x

a2x

þz2z

a2z

� �Sðkx; kzÞ ¼ axaz

2e¡ 1

4ða2xk2xþa2z k

2z Þ (6)

Exponential:

Rðzx; zzÞ ¼ e¡

ffiffiffiffiffiffiffiffiffiz2x

a2x

þz2z

a2z

qSðkx; kzÞ ¼ axaz

ð1þ a2xk2x þ a2zk

2z Þ

32

(7)

von Karman:

Rðzx; zzÞ ¼GH ðrÞGHð0Þ Sðkx; kzÞ ¼ axaz

ð1þ a2xk2x þ a2zk

2z ÞHþ1

(8)

where

GH ðrÞ ¼ rHKHðrÞ r ¼ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiz2xa2x

þ z2za2z

s(9)

ax and az are the correlation lengths along x and z-directions, respectively. H is the

Hurst exponent and KH is the modified Bessel function of the first kind. It can be

observed that when H D 0.5 von Karman is identical to the exponential PSD. The

parameters ax and az of the three random fields are estimated from the slip field by

minimizing the mean square error between the computed PSD and the expressionsshown in equations (6)�(8). The fitted Gaussian, exponential and von Karman PSD

at cross sections kx D 0 and kz D 0 are plotted in figure 11 along with the data for

Kashmir earthquake. Besides, the estimated parameters are also shown in the same

figure. The misfit associated with von Karman function is slightly lower than that

obtained from exponential and Gaussian function, and hence the slip fluctuation can

be modelled as a von Karman random field. Similarly, the correlation lengths are

estimated for all the slip models. These are reported in table 6 for Gaussian, exponen-

tial and von Karman PSD. The correlation length ax is much larger than az whichcan be attributed to large length compared to the width of the fault.

6. Scaling laws for correlation lengths

After estimating the spectral parameters from PSD, it remains to identify the pat-

terns with the previous determined effective source dimensions and moment

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Figure 11. Comparison with the Gaussian, exponential and von Karman PSD at the crosssections kx D 0 and kz D 0 for the slip model of Kashmir event shown in figure 2(a).

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Table 6. Estimates of correlation lengths and Hurst exponents, H, for slip models listed intable 1.

Gaussian Exponential von Karman

S. no. ax az ax az ax az H

1 42 28 23 16 6 4 12.3

2 70 43 43 26 49 31 0.3

3 40 27 22 15 6 4 11.1

4 30 40 16 25 7 10 4.1

5 11 19 6 12 6 12 0.5

6 54 93 30 55 21 37 1.4

7 104 55 60 30 38 20 1.6

8 148 55 73 32 90 41 0.2

9 33 8 20 4 9 2 3.5

10 21 10 12 5 4 2 6.1

11 22 14 12 8 3 2 12.7

12 16 10 9 6 6 2 1.8

13 44 12 27 6 11 3 3.8

14 41 45 22 25 13 14 2.2

15 76 54 43 30 60 43 0.1

16 44 12 27 8 38 11 0.1

17 140 10 76 6 82 6 0.4

18 47 58 28 31 39 43 0.1

19 33 33 18 18 12 12 1.6

20 33 37 20 21 29 28 0.1

21 90 45 48 25 44 22 0.7

22 99 100 56 64 45 50 0.9

23 34 78 20 38 28 50 0.1

24 67 42 35 24 30 21 0.8

25 123 27 69 15 51 11 1.2

26 28 32 15 18 5 6 7.1

27 53 10 33 5 27 4 0.9

28 25 12 14 7 20 10 0.1

29 86 9 44 5 37 4 0.9

30 42 14 26 8 20 6 1

31 15 11 8 6 3 2 6.8

32 12 10 7 5 2 2 7.1

33 42 13 25 8 35 11 0.1

34 16 6 10 3 5 3 2.4

35 39 100 21 79 14 50 1.5

36 63 90 37 50 40 50 0.4

37 115 4 32 3 51 3 0.1

38 117 24 68 13 55 33 0.5

39 17 30 9 18 4 7 4.3

40 81 83 45 50 11 11 13.7

41 81 83 45 50 11 11 13.7

42 81 83 45 50 11 11 13.7

43 92 62 51 36 12 8 14.6

44 150 85 114 48 44 19 4.3

45 8 17 4 10 2 4 4.1

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magnitude. Figures 12 and 13 show the variation of correlation lengths of the Von

Karman PSD with the Mw, effective length and width of the rupture plane. The cor-

relation lengths increase with increasing source dimensions. The Hurst exponent

does not show any pattern with the source dimensions. The variation of ax and azwith the source dimensions can be expressed as

log10ðY Þ ¼ C0 þ C1X (10)

where Y is correlation length in along-strike and down-dip directions, and X is the

Mw, Leff and Weff. The coefficients are obtained by regression analysis of the data.

These are reported in table 7 along with the standard error. The scaling laws derived

from the present study are shown in figures 12 and 13 along with the data.

Figure 12. Scaling of correlation length with effective rupture dimensions.

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7. Simulation of the slip field of large events

The proposed methodology for simulating spatial distribution of the slip field is asfollows:

(1) Fix the initial fault parameters such as strike, dip and rake angle based on the

tectonic set-up of the region. Select the moment magnitude, Mw, of the poten-

tial earthquake from the past seismicity of the region.

(2) Estimate the seismic moment from Mw from the relation of Hanks and

Kanamori (1979):

Mw ¼ 2=3 log10ðM0Þ¡ 10:7 (11)

(3) Determine the length, width, mean slip, correlation length and standard devia-

tion of slip from source scaling relations using the coefficients reported in table 4.

Figure 13. Correlation lengths and Hurst exponent of the von Karman PSD as a function ofmoment magnitude,Mw.

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For varying magnitudes, these parameters have been estimated from the scaling

relations developed in the present study and is reported in table 8.

(4) Once the correlation lengths are fixed, simulate the standardized slip as a von

Karman random field from the spectral representation method of Shinozukaand Deodatis (1996) or Fourier integral method of Pardo-Igu´zquiza and

Chica-Olmo (1993). Generate the slip field from equation (4). An ensemble of

slip models can be simulated from this procedure. Figure 14(a)�(d) shows the

simulated slip samples forMw D 7.5, 8, 8.5, 9, respectively.

Table 7. Coefficients for the scaling of correlation lengths ax and az for the autocorrelationfunction with source parameters log10(Y) D C0 C C1 (X).

X C0 C1 s(e)

Along-strike (Y D ax)

Mw ¡1.1090 0.2903 0.4194

Leff 0.7699 0.0025 0.3649

Weff 0.9705 0.0026 0.4284

Down-dip (Y D az)

Mw ¡2.5736 0.4475 0.3700

Leff 0.5171 0.0027 0.3500

Weff 0.4945 0.0056 0.3226

Table 8. Estimates of length, width, correlation lengths(ax, az) and Hurst exponents,H, forslip models for varying magnitudes.

Mw

Slip parameters 7.5 8 8.5 9

Subfault size, dx (km) 1 1 1 1

Subfault size, dz (km) 1 1 1 1

L (km) 100 176 312 551

W (km) 47 83 146 258

A (1EC005 sq. km) 0.047 0.146 0.456 1.422

D (cm) 67 119 211 373

sD (cm) 72 128 226 399

Leff (km) 71 125 221 390

Weff (km) 35 61 108 191

Deff (cm) 35 61 108 191

ALA (1EC005 sq. km) 0.012 0.037 0.116 0.370

AVLA (1EC005 sq. km) 0.005 0.017 0.053 0.169

ACA (1EC005 sq. km) 0.017 0.055 0.176 0.560

RDmax (km) 16.94 29.96 52.97 93.65

RLA (km) 4.77 8.44 14.93 26.39

RVLA (km) 7.23 12.78 22.59 39.95

Correlation length, ax (km) 11.70 16.35 22.83 31.89

Correlation length, az (km) 6.06 10.15 16.99 28.44

Hurst exponent,H 1.19 1.33 1.49 1.67

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(5) The location of the hypocentre can be decided based on the asperity location

as shown in figure 8.

8. Summary and conclusions

In this paper, a stochastic kinematic model has been developed to represent earth-

quake sources for large events. A total of 45 slip models coming from 33 events have

been used to develop the model. The development has been done in two stages. In

the first stage, scaling relations between seismic moment and source dimensions have

been derived from the data. The effective dimensions of the rupture plane are

Figure 14. (a) Simulated slip samples forMw D 7.5. (b) Simulated slip samples forMw D 8. (c)Simulated slip samples forMw D 8.5. (d) Simulated slip samples forMw D 9.

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estimated from the autocorrelation width. To conserve the seismic moment, slip on

the fault plane is increased by the ratio between area and effective area and effective

mean slip is obtained from the data. Scaling laws to estimate source dimensions from

seismic moment have been derived from the data. The data also have been used totest self-similarity of earthquakes. Empirical equations by constraining the slope in

the regression assuming self-similarity have been derived from the data. It can be

observed from figures 3 and 4 that the source dimensions follow self-similarity.

The area of asperities and their location on the rupture plane also have been exam-

ined for all the slip models. The asperities have been classified into large and very

large asperity based on the ratio of local slip to the average slip on the rupture plane.

It is observed that large asperities constitute 10%�55% of the effective rupture area,

and very large asperities constitute about 2%�40% of the Aeff, respectively. The areaof asperities also increases with increase in the seismic moment. Empirical equations

have been developed to estimate the area of asperities from the seismic moment. The

Figure 14. (Continued)

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large asperities are consistent with self-similarity, whereas the size of very large asper-ities deviates from self-similarity.

The hypocentre location on the rupture plane does not show any pattern with

magnitude, whereas the location of asperities from hypocentre increases with

increase in the seismic moment. The closest distance to regions of maximum slip and

very large asperity is consistent with self-similarity. The normalized distance from

hypocentre to asperities indicates that hypocentres are located closer to asperities.

Modelling the slip distribution on the rupture plane as a random field also has

been explored in this paper. This helps to understand the interaction between the slipon the neighbouring subfaults. The two-dimensional PSD is estimated from the slip

model by Fourier transform. The correlation lengths are different in along-strike and

down-dip directions indicating that the slip field is anisotropic. Gaussian, exponen-

tial and von Karman PSD are fitted to the data by estimating the correlation lengths

along the length and width of the rupture plane. It is observed that von Karman

PSD models the spectral decay of the slip field better than Gaussian and exponential

models. The correlation lengths increase with increase in the magnitude of the event.

Empirical equations to estimate the parameters in the von Karman PSD from magni-tude are derived from the data.

The results presented in this paper will be of use to engineers in simulating ground

motion for large events. Given a particular fault and magnitude, the developed

model can handle uncertainties in the slip distribution. The seismic moment can be

estimated from the magnitude through empirical relations. The length, width and

mean slip can be estimated from equations (1) and (2) from the seismic moment.

Once the rupture dimensions are known, correlation lengths can be determined by

using equation (10) and coefficients reported in table 7 from the magnitude of theevent. Sample realizations of the standardized slip field can be simulated by the spec-

tral representation of Shinozuka and Deodatis (1996) by replacing sequences of ran-

dom phase angles. The hypocentre should be located closely to the location of large

asperity on the rupture plane. An ensemble of slip fields can be generated from this

procedure. There are several methods available in the literature to generate ground

motion time histories for a given slip model (Douglas & Aochi 2008; Raghukanth

2008). Several samples of ground motion time histories can be generated from this

procedure. The developed stochastic source model for large events will find applica-tions in simulating ground motion for scenario earthquakes in seismic hazard analy-

sis. The equations developed in this study have to be updated as more slip models

become available.

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