Location

Location ANSS

The ANSS event ID is usc000p6gp and the event page is at https://earthquake.usgs.gov/earthquakes/eventpage/usc000p6gp/executive.

2014/04/05 12:42:17 36.131 -97.631 2.2 3.8 Oklahoma

Focal Mechanism

 USGS/SLU Moment Tensor Solution
 ENS  2014/04/05 12:42:17:0  36.13  -97.63   2.2 3.8 Oklahoma
 
 Stations used:
   AG.FCAR AG.HHAR AG.LCAR AG.WHAR AG.WLAR GS.OK025 GS.OK026 
   GS.OK027 GS.OK028 GS.OK029 N4.237B N4.N33B N4.N35B N4.P38B 
   N4.R32B N4.R40B N4.S39B N4.T35B N4.T42B N4.U38B N4.Z35B 
   N4.Z38B NM.UALR OK.CROK OK.FNO OK.U32A OK.X34A TA.U40A 
   TA.W39A TA.X40A US.CBKS US.KSU1 US.MIAR US.WMOK 
 
 Filtering commands used:
   cut a -30 a 180
   rtr
   taper w 0.1
   hp c 0.03 n 3 
   lp c 0.06 n 3 
 
 Best Fitting Double Couple
  Mo = 5.69e+21 dyne-cm
  Mw = 3.77 
  Z  = 4 km
  Plane   Strike  Dip  Rake
   NP1      130    90     5
   NP2       40    85   180
  Principal Axes:
   Axis    Value   Plunge  Azimuth
    T   5.69e+21      4     355
    N   0.00e+00     85     130
    P  -5.69e+21      4     265

 Moment Tensor: (dyne-cm)
    Component   Value
       Mxx     5.58e+21
       Mxy    -9.84e+20
       Mxz     3.80e+20
       Myy    -5.58e+21
       Myz     3.19e+20
       Mzz    -4.33e+13
                                                     
                                                     
                                                     
                                                     
                     #### T #######                  
                 ########   ###########              
              ###########################-           
             ###########################---          
           ---#########################------        
          ------######################--------       
         ---------##################-----------      
        ------------###############-------------     
        --------------###########---------------     
       ------------------#######-----------------    
         ------------------###-------------------    
       P ----------------------------------------    
         ------------------####------------------    
        ------------------########--------------     
        ----------------############------------     
         -------------################---------      
          -----------###################------       
           --------#######################---        
             ----##########################          
              -###########################           
                 ######################              
                     ##############                  
                                                     
                                                     
                                                     
 Global CMT Convention Moment Tensor:
      R          T          P
 -4.33e+13   3.80e+20  -3.19e+20 
  3.80e+20   5.58e+21   9.84e+20 
 -3.19e+20   9.84e+20  -5.58e+21 


Details of the solution is found at

http://www.eas.slu.edu/eqc/eqc_mt/MECH.NA/20140405124217/index.html
        

Preferred Solution

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

      STK = 130
      DIP = 90
     RAKE = 5
       MW = 3.77
       HS = 4.0

The NDK file is 20140405124217.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  2014/04/05 12:42:17:0  36.13  -97.63   2.2 3.8 Oklahoma
 
 Stations used:
   AG.FCAR AG.HHAR AG.LCAR AG.WHAR AG.WLAR GS.OK025 GS.OK026 
   GS.OK027 GS.OK028 GS.OK029 N4.237B N4.N33B N4.N35B N4.P38B 
   N4.R32B N4.R40B N4.S39B N4.T35B N4.T42B N4.U38B N4.Z35B 
   N4.Z38B NM.UALR OK.CROK OK.FNO OK.U32A OK.X34A TA.U40A 
   TA.W39A TA.X40A US.CBKS US.KSU1 US.MIAR US.WMOK 
 
 Filtering commands used:
   cut a -30 a 180
   rtr
   taper w 0.1
   hp c 0.03 n 3 
   lp c 0.06 n 3 
 
 Best Fitting Double Couple
  Mo = 5.69e+21 dyne-cm
  Mw = 3.77 
  Z  = 4 km
  Plane   Strike  Dip  Rake
   NP1      130    90     5
   NP2       40    85   180
  Principal Axes:
   Axis    Value   Plunge  Azimuth
    T   5.69e+21      4     355
    N   0.00e+00     85     130
    P  -5.69e+21      4     265

 Moment Tensor: (dyne-cm)
    Component   Value
       Mxx     5.58e+21
       Mxy    -9.84e+20
       Mxz     3.80e+20
       Myy    -5.58e+21
       Myz     3.19e+20
       Mzz    -4.33e+13
                                                     
                                                     
                                                     
                                                     
                     #### T #######                  
                 ########   ###########              
              ###########################-           
             ###########################---          
           ---#########################------        
          ------######################--------       
         ---------##################-----------      
        ------------###############-------------     
        --------------###########---------------     
       ------------------#######-----------------    
         ------------------###-------------------    
       P ----------------------------------------    
         ------------------####------------------    
        ------------------########--------------     
        ----------------############------------     
         -------------################---------      
          -----------###################------       
           --------#######################---        
             ----##########################          
              -###########################           
                 ######################              
                     ##############                  
                                                     
                                                     
                                                     
 Global CMT Convention Moment Tensor:
      R          T          P
 -4.33e+13   3.80e+20  -3.19e+20 
  3.80e+20   5.58e+21   9.84e+20 
 -3.19e+20   9.84e+20  -5.58e+21 


Details of the solution is found at

http://www.eas.slu.edu/eqc/eqc_mt/MECH.NA/20140405124217/index.html
	
Moment
7.22e+14 N-m
Magnitude
3.8
Percent DC
66%
Depth
4.0 km
Updated
2014-04-05 13:20:47 UTC
Author
us
Catalog
us
Contributor
us
Code
us_c000p6gp_mwr
Principal Axes

Axis	Value	Plunge	Azimuth
T	6.614	19	2
N	1.096	47	115
P	-7.709	36	258
Nodal Planes

Plane	Strike	Dip	Rake
NP1	307°	79	-41
NP2	46°	49	-166


        

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 ML by application of the respective IASPEI formulae. As a research study, the linear distance term of the IASPEI formula for ML is adjusted to remove a linear distance trend in residuals to give a regionally defined ML. The defined ML 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

The left panel of the next figure presents the focal mechanism for this earthquake (red) in the context of other nearby events (blue) in the SLU Moment Tensor Catalog. 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). Thus context plot is useful for assessing the appropriateness of the moment tensor of this event.

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 a -30 a 180
rtr
taper w 0.1
hp c 0.03 n 3 
lp c 0.06 n 3 
The results of this grid search are as follow:

           DEPTH  STK   DIP  RAKE   MW    FIT
WVFGRD96    1.0   130    80   -10   3.59 0.5264
WVFGRD96    2.0   130    75   -15   3.70 0.6339
WVFGRD96    3.0   130    80   -15   3.74 0.6738
WVFGRD96    4.0   130    90     5   3.77 0.6778
WVFGRD96    5.0   310    90     0   3.79 0.6637
WVFGRD96    6.0   310    90     0   3.81 0.6407
WVFGRD96    7.0   310    85     5   3.83 0.6179
WVFGRD96    8.0   315    75    15   3.86 0.6022
WVFGRD96    9.0   315    75    15   3.87 0.5842
WVFGRD96   10.0   315    75    15   3.88 0.5690
WVFGRD96   11.0   315    75    15   3.89 0.5563
WVFGRD96   12.0   315    75    20   3.90 0.5458
WVFGRD96   13.0   315    80    30   3.93 0.5386
WVFGRD96   14.0   315    80    25   3.93 0.5302
WVFGRD96   15.0   315    80    25   3.94 0.5220
WVFGRD96   16.0   315    75    20   3.94 0.5149
WVFGRD96   17.0   315    75    20   3.94 0.5079
WVFGRD96   18.0   315    75    20   3.95 0.5011
WVFGRD96   19.0   315    75    20   3.96 0.4944
WVFGRD96   20.0   315    80    25   3.97 0.4880
WVFGRD96   21.0   315    75    20   3.97 0.4821
WVFGRD96   22.0   315    75    20   3.98 0.4763
WVFGRD96   23.0   315    75    20   3.99 0.4706
WVFGRD96   24.0   315    80    25   4.00 0.4653
WVFGRD96   25.0   315    75    20   4.00 0.4604
WVFGRD96   26.0   315    75    20   4.01 0.4553
WVFGRD96   27.0   315    80    20   4.01 0.4512
WVFGRD96   28.0   315    80    20   4.02 0.4470
WVFGRD96   29.0   315    80    20   4.03 0.4425

The best solution is

WVFGRD96    4.0   130    90     5   3.77 0.6778

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 a -30 a 180
rtr
taper w 0.1
hp c 0.03 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:

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.

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    
Last Changed Fri Apr 26 05:03:06 PM CDT 2024