Location

Location ANSS

The ANSS event ID is usb000ry6y and the event page is at https://earthquake.usgs.gov/earthquakes/eventpage/usb000ry6y/executive.

2014/07/29 02:46:36 36.756 -98.045 5.3 4.3 Oklahoma

Focal Mechanism

USGS/SLU Moment Tensor Solution ENS 2014/07/29 02:46:36:0 36.76 -98.04 5.3 4.3 Oklahoma Stations used: AG.FCAR AG.HHAR AG.WHAR AG.WLAR GS.KAN10 GS.KAN12 GS.KAN13 GS.OK025 GS.OK026 GS.OK027 GS.OK028 GS.OK029 N4.237B N4.L34B N4.N33B N4.N35B N4.P38B N4.R32B N4.R40B N4.S39B N4.U38B N4.Z35B N4.Z38B NM.MGMO NM.UALR OK.BCOK OK.CROK OK.FNO OK.U32A OK.X37A TA.ABTX TA.BGNE TA.KSCO TA.MSTX TA.T25A TA.TUL1 TA.U40A TA.W39A TA.W41B TA.WHTX US.AMTX US.CBKS US.KSU1 US.MIAR US.WMOK Filtering commands used: cut o DIST/3.3 -40 o DIST/3.3 +60 rtr taper w 0.1 hp c 0.02 n 3 lp c 0.06 n 3 Best Fitting Double Couple Mo = 3.09e+22 dyne-cm Mw = 4.26 Z = 3 km Plane Strike Dip Rake NP1 305 65 -40 NP2 55 54 -149 Principal Axes: Axis Value Plunge Azimuth T 3.09e+22 6 2 N 0.00e+00 44 98 P -3.09e+22 45 265 Moment Tensor: (dyne-cm) Component Value Mxx 3.04e+22 Mxy -1.89e+20 Mxz 4.72e+21 Myy -1.52e+22 Myz 1.55e+22 Mzz -1.52e+22 ###### T ##### ########## ######### ############################ ############################## #--############################### ------------#######################- ------------------##################-- ----------------------##############---- ------------------------###########----- ----------------------------#######------- -------- -------------------####-------- -------- P ---------------------#--------- -------- --------------------##--------- -----------------------------#####------ --------------------------#########----- -----------------------############--- ------------------#################- -------------##################### ############################## ############################ ###################### ############## Global CMT Convention Moment Tensor: R T P -1.52e+22 4.72e+21 -1.55e+22 4.72e+21 3.04e+22 1.89e+20 -1.55e+22 1.89e+20 -1.52e+22 Details of the solution is found at http://www.eas.slu.edu/eqc/eqc_mt/MECH.NA/20140729024636/index.html

Preferred Solution

      STK = 305
      DIP = 65
     RAKE = -40
       MW = 4.26
       HS = 3.0

The NDK file is 20140729024636.ndk The waveform inversion is preferred.

Moment Tensor Comparison

The following compares this source inversion to those provided by others. The purpose is to look for major differences and also to note slight differences that might be inherent to the processing procedure. For completeness the USGS/SLU solution is repeated from above.

SLU

USGSMT

USGS/SLU Moment Tensor Solution ENS 2014/07/29 02:46:36:0 36.76 -98.04 5.3 4.3 Oklahoma Stations used: AG.FCAR AG.HHAR AG.WHAR AG.WLAR GS.KAN10 GS.KAN12 GS.KAN13 GS.OK025 GS.OK026 GS.OK027 GS.OK028 GS.OK029 N4.237B N4.L34B N4.N33B N4.N35B N4.P38B N4.R32B N4.R40B N4.S39B N4.U38B N4.Z35B N4.Z38B NM.MGMO NM.UALR OK.BCOK OK.CROK OK.FNO OK.U32A OK.X37A TA.ABTX TA.BGNE TA.KSCO TA.MSTX TA.T25A TA.TUL1 TA.U40A TA.W39A TA.W41B TA.WHTX US.AMTX US.CBKS US.KSU1 US.MIAR US.WMOK Filtering commands used: cut o DIST/3.3 -40 o DIST/3.3 +60 rtr taper w 0.1 hp c 0.02 n 3 lp c 0.06 n 3 Best Fitting Double Couple Mo = 3.09e+22 dyne-cm Mw = 4.26 Z = 3 km Plane Strike Dip Rake NP1 305 65 -40 NP2 55 54 -149 Principal Axes: Axis Value Plunge Azimuth T 3.09e+22 6 2 N 0.00e+00 44 98 P -3.09e+22 45 265 Moment Tensor: (dyne-cm) Component Value Mxx 3.04e+22 Mxy -1.89e+20 Mxz 4.72e+21 Myy -1.52e+22 Myz 1.55e+22 Mzz -1.52e+22 ###### T ##### ########## ######### ############################ ############################## #--############################### ------------#######################- ------------------##################-- ----------------------##############---- ------------------------###########----- ----------------------------#######------- -------- -------------------####-------- -------- P ---------------------#--------- -------- --------------------##--------- -----------------------------#####------ --------------------------#########----- -----------------------############--- ------------------#################- -------------##################### ############################## ############################ ###################### ############## Global CMT Convention Moment Tensor: R T P -1.52e+22 4.72e+21 -1.55e+22 4.72e+21 3.04e+22 1.89e+20 -1.55e+22 1.89e+20 -1.52e+22 Details of the solution is found at http://www.eas.slu.edu/eqc/eqc_mt/MECH.NA/20140729024636/index.html

Regional Moment Tensor (Mwr) Moment magnitude derived from a moment tensor inversion of complete waveforms at regional distances (less than ~8 degrees), generally used for the analysis of small to moderate size earthquakes (typically Mw 3.5-6.0) crust or upper mantle earthquakes. Moment 3.28e+15 N-m Magnitude 4.3 Percent DC 81% Depth 3.0 km Updated 2014-07-29 03:40:31 UTC Author us Catalog us Contributor us Code us_b000ry6y_mwr Principal Axes Axis Value Plunge Azimuth T 3.425 3 356 N -0.313 52 263 P -3.112 38 88 Nodal Planes Plane Strike Dip Rake NP1 229 66 -149 NP2 125 62 -27

Magnitudes

Given the availability of digital waveforms for determination of the moment tensor, this section documents the added processing leading to mLg, if appropriate to the region, and M_L by application of the respective IASPEI formulae. As a research study, the linear distance term of the IASPEI formula for M_L is adjusted to remove a linear distance trend in residuals to give a regionally defined M_L. The defined M_L uses horizontal component recordings, but the same procedure is applied to the vertical components since there may be some interest in vertical component ground motions. Residual plots versus distance may indicate interesting features of ground motion scaling in some distance ranges. A residual plot of the regionalized magnitude is given as a function of distance and azimuth, since data sets may transcend different wave propagation provinces.

mLg Magnitude

Left: mLg computed using the IASPEI formula. Center: mLg residuals versus epicentral distance ; the values used for the trimmed mean magnitude estimate are indicated. Right: residuals as a function of distance and azimuth.

ML Magnitude

Left: ML computed using the IASPEI formula for Horizontal components. Center: ML residuals computed using a modified IASPEI formula that accounts for path specific attenuation; the values used for the trimmed mean are indicated. The ML relation used for each figure is given at the bottom of each plot. Right: Residuals from new relation as a function of distance and azimuth.

Left: ML computed using the IASPEI formula for Vertical components (research). Center: ML residuals computed using a modified IASPEI formula that accounts for path specific attenuation; the values used for the trimmed mean are indicated. The ML relation used for each figure is given at the bottom of each plot. Right: Residuals from new relation as a function of distance and azimuth.

Context

Waveform Inversion using wvfgrd96

The focal mechanism was determined using broadband seismic waveforms. The location of the event (star) and the stations used for (red) the waveform inversion are shown in the next figure.

Location of broadband stations used for waveform inversion

The program wvfgrd96 was used with good traces observed at short distance to determine the focal mechanism, depth and seismic moment. This technique requires a high quality signal and well determined velocity model for the Green's functions. To the extent that these are the quality data, this type of mechanism should be preferred over the radiation pattern technique which requires the separate step of defining the pressure and tension quadrants and the correct strike.

The observed and predicted traces are filtered using the following gsac commands:

cut o DIST/3.3 -40 o DIST/3.3 +60
rtr
taper w 0.1
hp c 0.02 n 3 
lp c 0.06 n 3 

           DEPTH  STK   DIP  RAKE   MW    FIT
WVFGRD96    1.0   130    70   -25   4.10 0.5185
WVFGRD96    2.0   310    65   -35   4.19 0.5939
WVFGRD96    3.0   305    65   -40   4.26 0.6245
WVFGRD96    4.0   125    70   -30   4.28 0.6037
WVFGRD96    5.0   130    85   -10   4.28 0.5678
WVFGRD96    6.0   130    90   -15   4.30 0.5349
WVFGRD96    7.0   130    90   -20   4.31 0.5127
WVFGRD96    8.0   130    90   -30   4.34 0.4985
WVFGRD96    9.0   315    75    25   4.35 0.4878
WVFGRD96   10.0   315    75    25   4.35 0.4769
WVFGRD96   11.0   140    70    30   4.36 0.4689
WVFGRD96   12.0   140    70    30   4.36 0.4699
WVFGRD96   13.0   140    70    30   4.37 0.4690
WVFGRD96   14.0   140    70    25   4.37 0.4666
WVFGRD96   15.0   145    65    25   4.37 0.4629
WVFGRD96   16.0   145    65    25   4.37 0.4584
WVFGRD96   17.0   145    65    25   4.38 0.4527
WVFGRD96   18.0   140    60    15   4.38 0.4463
WVFGRD96   19.0   145    60    25   4.38 0.4403
WVFGRD96   20.0   145    60    25   4.39 0.4337
WVFGRD96   21.0   145    60    25   4.40 0.4258
WVFGRD96   22.0   145    55    20   4.39 0.4185
WVFGRD96   23.0   145    55    20   4.40 0.4108
WVFGRD96   24.0   145    55    20   4.40 0.4031
WVFGRD96   25.0   140    55    15   4.41 0.3951
WVFGRD96   26.0   140    55    15   4.41 0.3874
WVFGRD96   27.0   140    55    10   4.41 0.3798
WVFGRD96   28.0   140    55    10   4.42 0.3725
WVFGRD96   29.0   140    55    10   4.42 0.3655

The best solution is

WVFGRD96    3.0   305    65   -40   4.26 0.6245

The mechanism corresponding to the best fit is

Figure 1. Waveform inversion focal mechanism

The best fit as a function of depth is given in the following figure:

Figure 2. Depth sensitivity for waveform mechanism

The comparison of the observed and predicted waveforms is given in the next figure. The red traces are the observed and the blue are the predicted. Each observed-predicted component is plotted to the same scale and peak amplitudes are indicated by the numbers to the left of each trace. A pair of numbers is given in black at the right of each predicted traces. The upper number it the time shift required for maximum correlation between the observed and predicted traces. This time shift is required because the synthetics are not computed at exactly the same distance as the observed, the velocity model used in the predictions may not be perfect and the epicentral parameters may be be off. A positive time shift indicates that the prediction is too fast and should be delayed to match the observed trace (shift to the right in this figure). A negative value indicates that the prediction is too slow. The lower number gives the percentage of variance reduction to characterize the individual goodness of fit (100% indicates a perfect fit).

The bandpass filter used in the processing and for the display was

cut o DIST/3.3 -40 o DIST/3.3 +60
rtr
taper w 0.1
hp c 0.02 n 3 
lp c 0.06 n 3 

Figure 3. Waveform comparison for selected depth. Red: observed; Blue - predicted. The time shift with respect to the model prediction is indicated. The percent of fit is also indicated. The time scale is relative to the first trace sample.

Focal mechanism sensitivity at the preferred depth. The red color indicates a very good fit to the waveforms. Each solution is plotted as a vector at a given value of strike and dip with the angle of the vector representing the rake angle, measured, with respect to the upward vertical (N) in the figure.

A check on the assumed source location is possible by looking at the time shifts between the observed and predicted traces. The time shifts for waveform matching arise for several reasons:

• The origin time and epicentral distance are incorrect
• The velocity model used for the inversion is incorrect
• The velocity model used to define the P-arrival time is not the same as the velocity model used for the waveform inversion (assuming that the initial trace alignment is based on the P arrival time)

 Time_shift = A + B cos Azimuth + C Sin Azimuth

The time shifts for this inversion lead to the next figure:

The derived shift in origin time and epicentral coordinates are given at the bottom of the figure.

Velocity Model

The WUS.model used for the waveform synthetic seismograms and for the surface wave eigenfunctions and dispersion is as follows (The format is in the model96 format of Computer Programs in Seismology).

MODEL.01
Model after     8 iterations
ISOTROPIC
KGS
FLAT EARTH
1-D
CONSTANT VELOCITY
LINE08
LINE09
LINE10
LINE11
      H(KM)   VP(KM/S)   VS(KM/S) RHO(GM/CC)         QP         QS       ETAP       ETAS      FREFP      FREFS
     1.9000     3.4065     2.0089     2.2150  0.302E-02  0.679E-02   0.00       0.00       1.00       1.00    
     6.1000     5.5445     3.2953     2.6089  0.349E-02  0.784E-02   0.00       0.00       1.00       1.00    
    13.0000     6.2708     3.7396     2.7812  0.212E-02  0.476E-02   0.00       0.00       1.00       1.00    
    19.0000     6.4075     3.7680     2.8223  0.111E-02  0.249E-02   0.00       0.00       1.00       1.00    
     0.0000     7.9000     4.6200     3.2760  0.164E-10  0.370E-10   0.00       0.00       1.00       1.00