Location

Location ANSS

2017/06/07 02:54:34 36.448 -98.756 5.0 3.3 Oklahoma

Focal Mechanism

 USGS/SLU Moment Tensor Solution
 ENS  2017/06/07 02:54:34:0  36.45  -98.76   5.0 3.3 Oklahoma
 
 Stations used:
   GS.OK032 GS.OK035 OK.CROK OK.NOKA OK.U32A 
 
 Filtering commands used:
   cut o DIST/3.3 -25 o DIST/3.3 +35
   rtr
   taper w 0.1
   hp c 0.04 n 3 
   lp c 0.15 n 3 
 
 Best Fitting Double Couple
  Mo = 5.62e+20 dyne-cm
  Mw = 3.10 
  Z  = 5 km
  Plane   Strike  Dip  Rake
   NP1      295    70   -35
   NP2       38    57   -156
  Principal Axes:
   Axis    Value   Plunge  Azimuth
    T   5.62e+20      8     349
    N   0.00e+00     50      89
    P  -5.62e+20     39     253

 Moment Tensor: (dyne-cm)
    Component   Value
       Mxx     5.02e+20
       Mxy    -1.99e+20
       Mxz     1.57e+20
       Myy    -2.95e+20
       Myz     2.47e+20
       Mzz    -2.07e+20
                                                     
                                                     
                                                     
                                                     
                     ## T #########                  
                 ######   #############              
              ###########################-           
             ############################--          
           ##############################----        
          ###############################-----       
         ----------######################------      
        ------------------###############-------     
        ----------------------##########--------     
       ---------------------------#####----------    
       ------------------------------#-----------    
       -------   --------------------##----------    
       ------- P -------------------######-------    
        ------   ------------------#########----     
        -------------------------############---     
         -----------------------###############      
          --------------------################       
           ----------------##################        
             -----------###################          
              -----#######################           
                 ######################              
                     ##############                  
                                                     
                                                     
                                                     
 Global CMT Convention Moment Tensor:
      R          T          P
 -2.07e+20   1.57e+20  -2.47e+20 
  1.57e+20   5.02e+20   1.99e+20 
 -2.47e+20   1.99e+20  -2.95e+20 


Details of the solution is found at

http://www.eas.slu.edu/eqc/eqc_mt/MECH.NA/20170607025434/index.html
        

Preferred Solution

The preferred solution from an analysis of the surface-wave spectral amplitude radiation pattern, waveform inversion and first motion observations is

      STK = 295
      DIP = 70
     RAKE = -35
       MW = 3.10
       HS = 5.0

The NDK file is 20170607025434.ndk The waveform inversion is preferred.

Moment Tensor Comparison

The following compares this source inversion to others
SLU
 USGS/SLU Moment Tensor Solution
 ENS  2017/06/07 02:54:34:0  36.45  -98.76   5.0 3.3 Oklahoma
 
 Stations used:
   GS.OK032 GS.OK035 OK.CROK OK.NOKA OK.U32A 
 
 Filtering commands used:
   cut o DIST/3.3 -25 o DIST/3.3 +35
   rtr
   taper w 0.1
   hp c 0.04 n 3 
   lp c 0.15 n 3 
 
 Best Fitting Double Couple
  Mo = 5.62e+20 dyne-cm
  Mw = 3.10 
  Z  = 5 km
  Plane   Strike  Dip  Rake
   NP1      295    70   -35
   NP2       38    57   -156
  Principal Axes:
   Axis    Value   Plunge  Azimuth
    T   5.62e+20      8     349
    N   0.00e+00     50      89
    P  -5.62e+20     39     253

 Moment Tensor: (dyne-cm)
    Component   Value
       Mxx     5.02e+20
       Mxy    -1.99e+20
       Mxz     1.57e+20
       Myy    -2.95e+20
       Myz     2.47e+20
       Mzz    -2.07e+20
                                                     
                                                     
                                                     
                                                     
                     ## T #########                  
                 ######   #############              
              ###########################-           
             ############################--          
           ##############################----        
          ###############################-----       
         ----------######################------      
        ------------------###############-------     
        ----------------------##########--------     
       ---------------------------#####----------    
       ------------------------------#-----------    
       -------   --------------------##----------    
       ------- P -------------------######-------    
        ------   ------------------#########----     
        -------------------------############---     
         -----------------------###############      
          --------------------################       
           ----------------##################        
             -----------###################          
              -----#######################           
                 ######################              
                     ##############                  
                                                     
                                                     
                                                     
 Global CMT Convention Moment Tensor:
      R          T          P
 -2.07e+20   1.57e+20  -2.47e+20 
  1.57e+20   5.02e+20   1.99e+20 
 -2.47e+20   1.99e+20  -2.95e+20 


Details of the solution is found at

http://www.eas.slu.edu/eqc/eqc_mt/MECH.NA/20170607025434/index.html
	

Magnitudes

mLg Magnitude


(a) mLg computed using the IASPEI formula; (b) mLg residuals ; the values used for the trimmed mean are indicated.

ML Magnitude


(a) ML computed using the IASPEI formula for Horizontal components; (b) 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.


(a) ML computed using the IASPEI formula for Vertical components (research); (b) 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.

Context

The next figure presents the focal mechanism for this earthquake (red) in the context of other events (blue) in the SLU Moment Tensor Catalog which are within ± 0.5 degrees of the new event. This comparison is shown in the left panel of the figure. The right panel shows the inferred direction of maximum compressive stress and the type of faulting (green is strike-slip, red is normal, blue is thrust; oblique is shown by a combination of colors).

Waveform Inversion using wvfgrd96

The focal mechanism was determined using broadband seismic waveforms. The location of the event and the and stations used for 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 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 -25 o DIST/3.3 +35
rtr
taper w 0.1
hp c 0.04 n 3 
lp c 0.15 n 3 
The results of this grid search from 0.5 to 19 km depth are as follow:

           DEPTH  STK   DIP  RAKE   MW    FIT
WVFGRD96    1.0   120    55    -5   2.72 0.2997
WVFGRD96    2.0   290    75   -50   2.96 0.3835
WVFGRD96    3.0   285    70   -55   3.04 0.4696
WVFGRD96    4.0   290    65   -45   3.07 0.4981
WVFGRD96    5.0   295    70   -35   3.10 0.5039
WVFGRD96    6.0   300    75   -30   3.13 0.4929
WVFGRD96    7.0   300    80   -25   3.16 0.4711
WVFGRD96    8.0   295    65   -35   3.22 0.4467
WVFGRD96    9.0   295    65   -35   3.24 0.4112
WVFGRD96   10.0   295    60   -35   3.26 0.3792
WVFGRD96   11.0   295    60   -35   3.27 0.3500
WVFGRD96   12.0   295    60   -35   3.29 0.3267
WVFGRD96   13.0   205    65    15   3.30 0.3268
WVFGRD96   14.0   205    60    10   3.31 0.3267
WVFGRD96   15.0     0    55    25   3.29 0.3260
WVFGRD96   16.0     0    55    25   3.31 0.3327
WVFGRD96   17.0     0    55    30   3.32 0.3398
WVFGRD96   18.0     5    50    35   3.35 0.3445
WVFGRD96   19.0     5    50    35   3.36 0.3492
WVFGRD96   20.0     5    50    35   3.37 0.3507
WVFGRD96   21.0    10    50    50   3.38 0.3550
WVFGRD96   22.0    10    50    50   3.39 0.3631
WVFGRD96   23.0    10    50    50   3.40 0.3649
WVFGRD96   24.0    15    50    55   3.41 0.3707
WVFGRD96   25.0    10    55    50   3.40 0.3764
WVFGRD96   26.0    15    55    55   3.41 0.3847
WVFGRD96   27.0    15    55    55   3.42 0.3943
WVFGRD96   28.0    15    55    55   3.42 0.3996
WVFGRD96   29.0    15    55    55   3.43 0.4046

The best solution is

WVFGRD96    5.0   295    70   -35   3.10 0.5039

The mechanism correspond 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 and because the velocity model used in the predictions may not be perfect. 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 -25 o DIST/3.3 +35
rtr
taper w 0.1
hp c 0.04 n 3 
lp c 0.15 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.
Focal mechanism sensitivity at the preferred depth. The red color indicates a very good fit to thewavefroms. 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:

Assuming only a mislocation, the time shifts are fit to a functional form:

 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.

Discussion

Acknowledgements

Thanks also to the many seismic network operators whose dedication make this effort possible: University of Nevada Reno, University of Alaska, University of Washington, Oregon State University, University of Utah, Montana Bureas of Mines, UC Berkely, Caltech, UC San Diego, Saint Louis University, University of Memphis, Lamont Doherty Earth Observatory, the Iris stations and the Transportable Array of EarthScope.

Velocity Model

The WUS.model used for the waveform synthetic seismograms and for the surface wave eigenfunctions and dispersion is as follows:

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    

Quality Control

Here we tabulate the reasons for not using certain digital data sets

The following stations did not have a valid response files:

Last Changed Tue Jun 6 23:24:41 CDT 2017