Location

SLU Location

BEcause of concerns about the effect of a mislocation on the moment tensor, first arrival times were read and elocate was used to locate. The solution is very similar to the PR solution except for the depth. The time delay versus azimith plot(below) indicates that this is better. The free depth of the SLU solution is greater. The depth control is better. The first motions agree. The SLU data and run are given in elocate.txt.

Location ANSS

This is the location given by PR. The initial US location was about 20 km south.
2020/01/26 17:19:08 17.967 -66.839 9.0 4.3 Puerto Rico

Focal Mechanism

USGS/SLU Moment Tensor Solution ENS 2020/01/26 17:19:07:0 17.95 -66.83 20.0 4.3 Puerto Rico Stations used: GS.PR01 GS.PR03 GS.PR04 GS.PR05 GS.PR06 IU.SJG PR.AGPR PR.CELP PR.CRPR PR.ECPR PR.GCPR PR.HUMP PR.MLPR PR.OBIP PR.PRSN PR.UUPR Filtering commands used: cut o DIST/3.3 -40 o DIST/3.3 +50 rtr taper w 0.1 hp c 0.03 n 3 lp c 0.10 n 3 Best Fitting Double Couple Mo = 5.89e+21 dyne-cm Mw = 3.78 Z = 15 km Plane Strike Dip Rake NP1 159 85 170 NP2 250 80 5 Principal Axes: Axis Value Plunge Azimuth T 5.89e+21 11 114 N 0.00e+00 79 313 P -5.89e+21 4 205 Moment Tensor: (dyne-cm) Component Value Mxx -3.87e+21 Mxy -4.37e+21 Mxz -1.05e+20 Myy 3.69e+21 Myz 1.12e+21 Mzz 1.76e+20 -------------- ####------------------ #######--------------------- #########--------------------- ############---------------------- #############----------------------- ###############----------------------- ################------------------###### #################---------############## ###################--##################### ################---####################### ############--------###################### ########-------------##################### ####----------------#################### #--------------------############## ## ---------------------############# T # ---------------------############ ---------------------############# -------------------########### ---- ------------######### - P -------------##### -------------- Global CMT Convention Moment Tensor: R T P 1.76e+20 -1.05e+20 -1.12e+21 -1.05e+20 -3.87e+21 4.37e+21 -1.12e+21 4.37e+21 3.69e+21 Details of the solution is found at http://www.eas.slu.edu/eqc/eqc_mt/MECH.NA/20200126171907/index.html Details of the solution is found at http://www.eas.slu.edu/eqc/eqc_mt/MECH.NA/20200126171907/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 = 250
      DIP = 80
     RAKE = 5
       MW = 3.78
       HS = 15.0

The NDK file is 20200126171907.ndk The waveform inversion is preferred.

Moment Tensor Comparison

The following compares this source inversion to others

SLU SLUFM

USGS/SLU Moment Tensor Solution ENS 2020/01/26 17:19:07:0 17.95 -66.83 20.0 4.3 Puerto Rico Stations used: GS.PR01 GS.PR03 GS.PR04 GS.PR05 GS.PR06 IU.SJG PR.AGPR PR.CELP PR.CRPR PR.ECPR PR.GCPR PR.HUMP PR.MLPR PR.OBIP PR.PRSN PR.UUPR Filtering commands used: cut o DIST/3.3 -40 o DIST/3.3 +50 rtr taper w 0.1 hp c 0.03 n 3 lp c 0.10 n 3 Best Fitting Double Couple Mo = 5.89e+21 dyne-cm Mw = 3.78 Z = 15 km Plane Strike Dip Rake NP1 159 85 170 NP2 250 80 5 Principal Axes: Axis Value Plunge Azimuth T 5.89e+21 11 114 N 0.00e+00 79 313 P -5.89e+21 4 205 Moment Tensor: (dyne-cm) Component Value Mxx -3.87e+21 Mxy -4.37e+21 Mxz -1.05e+20 Myy 3.69e+21 Myz 1.12e+21 Mzz 1.76e+20 -------------- ####------------------ #######--------------------- #########--------------------- ############---------------------- #############----------------------- ###############----------------------- ################------------------###### #################---------############## ###################--##################### ################---####################### ############--------###################### ########-------------##################### ####----------------#################### #--------------------############## ## ---------------------############# T # ---------------------############ ---------------------############# -------------------########### ---- ------------######### - P -------------##### -------------- Global CMT Convention Moment Tensor: R T P 1.76e+20 -1.05e+20 -1.12e+21 -1.05e+20 -3.87e+21 4.37e+21 -1.12e+21 4.37e+21 3.69e+21 Details of the solution is found at http://www.eas.slu.edu/eqc/eqc_mt/MECH.NA/20200126171907/index.html Details of the solution is found at http://www.eas.slu.edu/eqc/eqc_mt/MECH.NA/20200126171907/index.html USGS/SLU Moment Tensor Solution ENS 2020/01/26 17:19:08:0 17.97 -66.84 9.0 4.3 Puerto Rico Stations used: GS.PR01 GS.PR03 GS.PR04 GS.PR05 GS.PR06 IU.SJG PR.AGPR PR.CELP PR.CRPR PR.ECPR PR.GCPR PR.HUMP PR.MLPR PR.OBIP PR.PRSN PR.UUPR Filtering commands used: cut o DIST/3.3 -40 o DIST/3.3 +50 rtr taper w 0.1 hp c 0.03 n 3 lp c 0.10 n 3 Best Fitting Double Couple Mo = 5.89e+21 dyne-cm Mw = 3.78 Z = 15 km Plane Strike Dip Rake NP1 159 85 170 NP2 250 80 5 Principal Axes: Axis Value Plunge Azimuth T 5.89e+21 11 114 N 0.00e+00 79 313 P -5.89e+21 4 205 Moment Tensor: (dyne-cm) Component Value Mxx -3.87e+21 Mxy -4.37e+21 Mxz -1.05e+20 Myy 3.69e+21 Myz 1.12e+21 Mzz 1.76e+20 -------------- ####------------------ #######--------------------- #########--------------------- ############---------------------- #############----------------------- ###############----------------------- ################------------------###### #################---------############## ###################--##################### ################---####################### ############--------###################### ########-------------##################### ####----------------#################### #--------------------############## ## ---------------------############# T # ---------------------############ ---------------------############# -------------------########### ---- ------------######### - P -------------##### -------------- Global CMT Convention Moment Tensor: R T P 1.76e+20 -1.05e+20 -1.12e+21 -1.05e+20 -3.87e+21 4.37e+21 -1.12e+21 4.37e+21 3.69e+21

First motions and takeoff angles from an elocate run.

Magnitudes

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 -40 o DIST/3.3 +50
rtr
taper w 0.1
hp c 0.03 n 3 
lp c 0.10 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   255    60    -5   3.19 0.2391
WVFGRD96    2.0   255    65     5   3.36 0.3666
WVFGRD96    3.0   255    65    10   3.43 0.4440
WVFGRD96    4.0   255    70    10   3.47 0.5011
WVFGRD96    5.0   255    70    20   3.52 0.5475
WVFGRD96    6.0   250    75    15   3.55 0.5893
WVFGRD96    7.0   250    75    10   3.58 0.6272
WVFGRD96    8.0   250    75    10   3.63 0.6622
WVFGRD96    9.0   250    75     5   3.65 0.6866
WVFGRD96   10.0   250    80     5   3.68 0.7072
WVFGRD96   11.0   250    80     5   3.70 0.7237
WVFGRD96   12.0   250    80     5   3.72 0.7349
WVFGRD96   13.0   250    80     5   3.74 0.7436
WVFGRD96   14.0   250    80     5   3.76 0.7482
WVFGRD96   15.0   250    80     5   3.78 0.7498
WVFGRD96   16.0   250    75     5   3.78 0.7493
WVFGRD96   17.0   250    75     5   3.80 0.7465
WVFGRD96   18.0   250    75     5   3.81 0.7421
WVFGRD96   19.0   250    75     5   3.83 0.7359
WVFGRD96   20.0   250    75     5   3.84 0.7280
WVFGRD96   21.0   255    70     5   3.85 0.7200
WVFGRD96   22.0   255    70     5   3.86 0.7112
WVFGRD96   23.0   255    70     5   3.87 0.7019
WVFGRD96   24.0   255    70     5   3.88 0.6924
WVFGRD96   25.0   255    70    10   3.88 0.6820
WVFGRD96   26.0   255    70    10   3.89 0.6715
WVFGRD96   27.0   255    70    10   3.90 0.6595
WVFGRD96   28.0   255    65    10   3.90 0.6478
WVFGRD96   29.0   255    65    10   3.90 0.6350

The best solution is

WVFGRD96   15.0   250    80     5   3.78 0.7498

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 -40 o DIST/3.3 +50
rtr
taper w 0.1
hp c 0.03 n 3 
lp c 0.10 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:

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)

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 Bureau of Mines, UC Berkely, Caltech, UC San Diego, Saint Louis University, University of Memphis, Lamont Doherty Earth Observatory, the Oklahoma Geological Survey, TexNet, the Iris stations, the Transportable Array of EarthScope and other networks.

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 Sun Jan 26 12:11:31 CST 2020