Location

2010/02/27 22:22:27 35.54 -96.75 4.0 4.40 Oklahoma

SLU Location

 Error Ellipse  X=   0.3690 km  Y= 0.5651 km  Theta =  71.8577 deg

 RMS Error        :               0.110              sec
 Travel_Time_Table:          CUS     
 Latitude         :             35.5585 +-    0.0049 N         0.5491 km
 Longitude        :            -96.7383 +-    0.0044 E         0.3924 km
 Depth            :                4.17 +-      0.73 km
 Epoch Time       :      1267309347.889 +-      0.09 sec
 Event Time       :  20100227222227.889 +-      0.09 sec
 Event (OCAL)     :  2010 02 27 22 22 27 889
 HYPO71 Quality   :                  CC
 Gap              :                  79              deg

The SLU location is made using the program elocate and arival time picks from the NetQuake instruments in the source region and adjacent TA stations. The output is given in elocate.txt. The CUS model provides a smaller RMS errors (0.11 sec vs 0.17 sec) and the WUS model gives a depth of 17 km. Thus depth is highly model dependent. The waveform solution is 7 km.

USGS Location

MAG     DATE      TIME      LAT     LON  H(km)   State
4.1Mw 2010/02/27 22:22:27  35.623 -96.762 3.8  Oklahoma

Arrival Times (from USGS)

Arrival time list

Felt Map

USGS Felt map for this earthquake

USGS Felt reports main page

Focal Mechanism

 USGS/SLU Moment Tensor Solution
 ENS  2010/02/27 22:22:27:0  35.54  -96.75   4.0 4.4 Oklahoma
 
 Stations used:
   NM.MGMO NM.UALR TA.129A TA.131A TA.133A TA.134A TA.135A 
   TA.232A TA.233A TA.234A TA.332A TA.333A TA.334A TA.335A 
   TA.434A TA.435B TA.ABTX TA.O31A TA.O32A TA.P29A TA.P30A 
   TA.P31A TA.P32A TA.P33A TA.Q29A TA.Q30A TA.Q32A TA.Q33A 
   TA.R28A TA.R29A TA.R30A TA.R31A TA.R32A TA.R33A TA.S28A 
   TA.S29A TA.S30A TA.S31A TA.S32A TA.S33A TA.T28A TA.T29A 
   TA.T30A TA.T31A TA.T32A TA.T33A TA.TUL1 TA.U27A TA.U29A 
   TA.U30A TA.U31A TA.U32A TA.U34A TA.V31A TA.V32A TA.V33A 
   TA.V34A TA.W28A TA.W29A TA.W30A TA.W31A TA.W32A TA.W33A 
   TA.W34A TA.WHTX TA.X29A TA.X31A TA.X32A TA.X33A TA.X34A 
   TA.Y30A TA.Y31A TA.Y32A TA.Y33A TA.Y34A TA.Z31A TA.Z32A 
   TA.Z33A TA.Z34A TA.Z35A US.AMTX US.KSU1 US.MIAR 
 
 Filtering commands used:
   hp c 0.02 n 3
   lp c 0.06 n 3
 
 Best Fitting Double Couple
  Mo = 2.11e+22 dyne-cm
  Mw = 4.15 
  Z  = 4 km
  Plane   Strike  Dip  Rake
   NP1       40    80   -160
   NP2      306    70   -11
  Principal Axes:
   Axis    Value   Plunge  Azimuth
    T   2.11e+22      7     172
    N   0.00e+00     68      66
    P  -2.11e+22     21     265

 Moment Tensor: (dyne-cm)
    Component   Value
       Mxx     2.03e+22
       Mxy    -4.61e+21
       Mxz    -1.72e+21
       Myy    -1.78e+22
       Myz     7.42e+21
       Mzz    -2.47e+21
                                                     
                                                     
                                                     
                                                     
                     ##############                  
                 ######################              
              ###########################-           
             ###########################---          
           ---##########################-----        
          ----------###################-------       
         ---------------#############----------      
        -------------------#########------------     
        ----------------------#####-------------     
       ------------------------------------------    
       ---   -------------------###--------------    
       --- P ------------------######------------    
       ---   ----------------##########----------    
        -------------------#############--------     
        ------------------################------     
         ---------------###################----      
          ------------######################--       
           ---------#########################        
             -----#########################          
              -###########################           
                 ############   #######              
                     ######## T ###                  
                                                     
                                                     
                                                     
 Global CMT Convention Moment Tensor:
      R          T          P
 -2.47e+21  -1.72e+21  -7.42e+21 
 -1.72e+21   2.03e+22   4.61e+21 
 -7.42e+21   4.61e+21  -1.78e+22 


Details of the solution is found at

http://www.eas.slu.edu/eqc/eqc_mt/MECH.NA/20100227222227/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 = 40
      DIP = 80
     RAKE = -160
       MW = 4.15
       HS = 4.0

This earthquake is east of the other earthquakes located in this part of Oklahoma in January and February. The low pass filtered seismogram fits show short period surface waves which is indicative of the shallow velocity structure that is not built into the WUS model. The surface-wave analysis was performed because of the well dispersed surface waves at short distance. This was especially observed in the Love waves. Such information can be used to refine the local velocity model and Q. The dispersion will be incorporated in the continental surface-wave tomography study. The surface waves like a 4 km depth, which the waveform inversion results depend on the frequency band used, which was purposely chosen to be less sensitive to the short-period surface waves, which are indicative of a shallow depth. For this event, the surface-wave solution is used since the waveforms do not have great depth sensitivity.

Moment Tensor Comparison

The following compares this source inversion to others
SLU
SLUFM
 USGS/SLU Moment Tensor Solution
 ENS  2010/02/27 22:22:27:0  35.54  -96.75   4.0 4.4 Oklahoma
 
 Stations used:
   NM.MGMO NM.UALR TA.129A TA.131A TA.133A TA.134A TA.135A 
   TA.232A TA.233A TA.234A TA.332A TA.333A TA.334A TA.335A 
   TA.434A TA.435B TA.ABTX TA.O31A TA.O32A TA.P29A TA.P30A 
   TA.P31A TA.P32A TA.P33A TA.Q29A TA.Q30A TA.Q32A TA.Q33A 
   TA.R28A TA.R29A TA.R30A TA.R31A TA.R32A TA.R33A TA.S28A 
   TA.S29A TA.S30A TA.S31A TA.S32A TA.S33A TA.T28A TA.T29A 
   TA.T30A TA.T31A TA.T32A TA.T33A TA.TUL1 TA.U27A TA.U29A 
   TA.U30A TA.U31A TA.U32A TA.U34A TA.V31A TA.V32A TA.V33A 
   TA.V34A TA.W28A TA.W29A TA.W30A TA.W31A TA.W32A TA.W33A 
   TA.W34A TA.WHTX TA.X29A TA.X31A TA.X32A TA.X33A TA.X34A 
   TA.Y30A TA.Y31A TA.Y32A TA.Y33A TA.Y34A TA.Z31A TA.Z32A 
   TA.Z33A TA.Z34A TA.Z35A US.AMTX US.KSU1 US.MIAR 
 
 Filtering commands used:
   hp c 0.02 n 3
   lp c 0.06 n 3
 
 Best Fitting Double Couple
  Mo = 2.11e+22 dyne-cm
  Mw = 4.15 
  Z  = 4 km
  Plane   Strike  Dip  Rake
   NP1       40    80   -160
   NP2      306    70   -11
  Principal Axes:
   Axis    Value   Plunge  Azimuth
    T   2.11e+22      7     172
    N   0.00e+00     68      66
    P  -2.11e+22     21     265

 Moment Tensor: (dyne-cm)
    Component   Value
       Mxx     2.03e+22
       Mxy    -4.61e+21
       Mxz    -1.72e+21
       Myy    -1.78e+22
       Myz     7.42e+21
       Mzz    -2.47e+21
                                                     
                                                     
                                                     
                                                     
                     ##############                  
                 ######################              
              ###########################-           
             ###########################---          
           ---##########################-----        
          ----------###################-------       
         ---------------#############----------      
        -------------------#########------------     
        ----------------------#####-------------     
       ------------------------------------------    
       ---   -------------------###--------------    
       --- P ------------------######------------    
       ---   ----------------##########----------    
        -------------------#############--------     
        ------------------################------     
         ---------------###################----      
          ------------######################--       
           ---------#########################        
             -----#########################          
              -###########################           
                 ############   #######              
                     ######## T ###                  
                                                     
                                                     
                                                     
 Global CMT Convention Moment Tensor:
      R          T          P
 -2.47e+21  -1.72e+21  -7.42e+21 
 -1.72e+21   2.03e+22   4.61e+21 
 -7.42e+21   4.61e+21  -1.78e+22 


Details of the solution is found at

http://www.eas.slu.edu/eqc/eqc_mt/MECH.NA/20100227222227/index.html
	



The first motion plot agrees with the waveform inversion. Triangles are strong dilations, - is a weak dilatation, + a weak compression and a circle is a strong compression. The X indicates a nodal arrival. The takeoff angles and picks are in the elocate.txt file.

Waveform Inversion

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:

hp c 0.02 n 3
lp c 0.06 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    0.5   305    70   -15   3.86 0.3594
WVFGRD96    1.0   310    90     5   3.86 0.3856
WVFGRD96    2.0   310    90     0   3.95 0.4713
WVFGRD96    3.0   310    85     5   3.99 0.5059
WVFGRD96    4.0   310    85     5   4.02 0.5236
WVFGRD96    5.0   310    90    -5   4.05 0.5312
WVFGRD96    6.0   310    80     5   4.07 0.5337
WVFGRD96    7.0   310    75     5   4.10 0.5351
WVFGRD96    8.0   130    85    15   4.12 0.5359
WVFGRD96    9.0   130    85    20   4.14 0.5297
WVFGRD96   10.0   310    70     5   4.15 0.5224
WVFGRD96   11.0   310    70     0   4.16 0.5163
WVFGRD96   12.0   130    90    20   4.17 0.5100
WVFGRD96   13.0   310    85    25   4.18 0.5048
WVFGRD96   14.0   310    85    20   4.19 0.5002
WVFGRD96   15.0   310    80    20   4.20 0.4951
WVFGRD96   16.0   310    80    20   4.20 0.4891
WVFGRD96   17.0   310    80    20   4.21 0.4823
WVFGRD96   18.0   310    80    15   4.22 0.4749
WVFGRD96   19.0   310    80    15   4.22 0.4672
WVFGRD96   20.0   310    80    15   4.23 0.4588
WVFGRD96   21.0   310    80    15   4.24 0.4497
WVFGRD96   22.0   310    80    15   4.24 0.4409
WVFGRD96   23.0   310    80    15   4.25 0.4318
WVFGRD96   24.0   310    80    15   4.25 0.4226
WVFGRD96   25.0   310    80   -10   4.26 0.4129
WVFGRD96   26.0   310    80   -10   4.26 0.4041
WVFGRD96   27.0   310    80   -10   4.27 0.3953
WVFGRD96   28.0   310    80   -10   4.28 0.3865
WVFGRD96   29.0   310    80   -10   4.28 0.3779

The best solution is

WVFGRD96    8.0   130    85    15   4.12 0.5359

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 componnet is plotted to the same scale and peak amplitudes are indicated by the numbers to the left of each trace. The number in black at the rightr of each predicted traces 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 bandpass filter used in the processing and for the display was

hp c 0.02 n 3
lp c 0.06 n 3
Figure 3. Waveform comparison for selected depth
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.

Surface-Wave Focal Mechanism

The following figure shows the stations used in the grid search for the best focal mechanism to fit the surface-wave spectral amplitudes of the Love and Rayleigh waves.
Location of broadband stations used to obtain focal mechanism from surface-wave spectral amplitudes

The surface-wave determined focal mechanism is shown here.


  NODAL PLANES 

  
  STK=      40.00
  DIP=      79.99
 RAKE=    -160.00
  
             OR
  
  STK=     306.38
  DIP=      70.32
 RAKE=     -10.63
 
 
DEPTH = 4.0 km
 
Mw = 4.15
Best Fit 0.8729 - P-T axis plot gives solutions with FIT greater than FIT90

First motion data

The P-wave first motion data for focal mechanism studies are as follow:

Sta Az    Dist   First motion

Surface-wave analysis

Surface wave analysis was performed using codes from Computer Programs in Seismology, specifically the multiple filter analysis program do_mft and the surface-wave radiation pattern search program srfgrd96.

Data preparation

Digital data were collected, instrument response removed and traces converted to Z, R an T components. Multiple filter analysis was applied to the Z and T traces to obtain the Rayleigh- and Love-wave spectral amplitudes, respectively. These were input to the search program which examined all depths between 1 and 25 km and all possible mechanisms.
Best mechanism fit as a function of depth. The preferred depth is given above. Lower hemisphere projection

Pressure-tension axis trends. Since the surface-wave spectra search does not distinguish between P and T axes and since there is a 180 ambiguity in strike, all possible P and T axes are plotted. First motion data and waveforms will be used to select the preferred mechanism. The purpose of this plot is to provide an idea of the possible range of solutions. The P and T-axes for all mechanisms with goodness of fit greater than 0.9 FITMAX (above) are plotted here.


Focal mechanism sensitivity at the preferred depth. The red color indicates a very good fit to the Love and Rayleigh wave radiation patterns. 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. Because of the symmetry of the spectral amplitude rediation patterns, only strikes from 0-180 degrees are sampled.

Love-wave radiation patterns

Rayleigh-wave radiation patterns

Broadband station distribution

The distribution of broadband stations with azimuth and distance is
Listing of broadband stations used

Waveform comparison for this mechanism

Since the analysis of the surface-wave radiation patterns uses only spectral amplitudes and because the surfave-wave radiation patterns have a 180 degree symmetry, each surface-wave solution consists of four possible focal mechanisms corresponding to the interchange of the P- and T-axes and a roation of the mechanism by 180 degrees. To select one mechanism, P-wave first motion can be used. This was not possible in this case because all the P-wave first motions were emergent ( a feature of the P-wave wave takeoff angle, the station location and the mechanism). The other way to select among the mechanisms is to compute forward synthetics and compare the observed and predicted waveforms.

The fits to the waveforms with the given mechanism are show below:

This figure shows the fit to the three components of motion (Z - vertical, R-radial and T - transverse). For each station and component, the observed traces is shown in red and the model predicted trace in blue. The traces represent filtered ground velocity in units of meters/sec (the peak value is printed adjacent to each trace; each pair of traces to plotted to the same scale to emphasize the difference in levels). Both synthetic and observed traces have been filtered using the SAC commands:

hp c 0.02 n 3
lp c 0.06 n 3

Discussion

The Future

Should the national backbone of the USGS Advanced National Seismic System (ANSS) be implemented with an interstation separation of 300 km, it is very likely that an earthquake such as this would have been recorded at distances on the order of 100-200 km. This means that the closest station would have information on source depth and mechanism that was lacking here.

Acknowledgements

Dr. Harley Benz, USGS, provided the USGS USNSN digital data. The digital data used in this study were provided by Natural Resources Canada through their AUTODRM site http://www.seismo.nrcan.gc.ca/nwfa/autodrm/autodrm_req_e.php, and IRIS using their BUD interface.

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

Appendix A


Spectra fit plots to each station

Velocity Model

The WUS 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:

DATE=Tue Mar 2 11:56:44 CST 2010

Last Changed 2010/02/27