1. Introduction
Ensuring the seismic performance of nuclear power plants has attracted increased interest worldwide since the Fukushima nuclear incident. Recently, earthquakes with a magnitude higher than 5, such as the Gyeongju earthquake (2016) and the Pohang earthquake (2017), have raised interest in the seismic safety of the nuclear power plants in Korea. Nuclear power plants use various systems to produce and transport energy using nuclear reactors and use a large amount of piping to connect these systems and facilities. Accordingly, it is essential to ensure the seismic safety of these piping systems.
According to various experiments and studies [
1,
2,
3,
4,
5] conducted on nuclear piping, the primary cause of pipe damage due to earthquakes appeared to be low-frequency fatigue. The pipe elbows were vulnerable to seismic events. A shake table test was conducted to analyze the seismic behavior of nuclear power plant piping. A quantitative study was performed to define the actual failure (leakage) of the piping system [
6,
7,
8]. Recently, studies were conducted to define the degree of piping damage based on an energy dissipation concept [
9].
Studies are underway to apply seismic isolation systems to improve the seismic performance of nuclear power plants [
10,
11,
12,
13]. On the other hand, the seismic risk may increase due to the large relative displacement induced by a period shift by the seismic isolation [
14]. In particular, there is a high risk of damage to the crossover(interface)-piping connecting the isolated part to the non-isolated part. Under this background, a study was carried out to evaluate the seismic safety of the crossover-piping of a seismic isolated nuclear power plant [
15]. In addition, finite element analysis was performed to evaluate the seismic safety of the pipe system of the nuclear power plant [
16,
17].
Specifically, seismic fragility analysis of the piping system for an isolated nuclear power plant was performed. Seismic fragility analysis of the piping system connecting the isolated and non-isolated parts was performed by modifying the NRC (U.S. Nuclear Regulatory Commission)-BNL (Brookhaven National Laboratory) benchmark model [
18,
19]. The justification of seismic fragility analysis of crossover-piping was confirmed by applying a damage index based on the dissipation energy to express the actual failure quantitatively [
20].
On the other hand, the seismic safety of nuclear power plants is determined by performing a seismic probabilistic safety assessment. Therefore, seismic fragility analyses are performed on the structures, systems, and components of nuclear power plants, including piping systems. Seismic fragility analysis requires a statistical approach towards various random variables. Therefore, multiple seismic response analyses are performed. These seismic response analyses should account for the nonlinearity of the seismic behavior of the piping element. Nevertheless, the analysis must be performed under suitable numerical conditions because the seismic response analysis of the piping systems depends on various numerical conditions. Such an argument relies on the following study result. In the OECD (Organization for Economic Cooperation and Development)-NEA (Nuclear Energy Agency), the MECOS (Metallic Component Margins under High Seismic Load) benchmark, a round-robin test that performs finite element analysis based on test results, was conducted to identify an appropriate method to simulate dynamic and static nonlinear behavior for the piping of nuclear power plants accurately. As a result, the results of the eigenvalue analysis were not significantly different. In the case of nonlinear analysis, however, a large error occurred from the experimental results.
Through the results of the MECOS benchmark, it was difficult for finite element analysis to simulate the actual failure accurately based on the fatigue ratcheting of nuclear piping. Thus, it is necessary to check the uncertainty and variability due to the variables of the analysis conditions to analyze the seismic fragility of a nuclear power plant piping system. Typical numerical conditions that affect the results of the seismic response analysis of the piping system are a convergence condition and a mesh size in nonlinear analysis. In this study, the variable seismic performance of a piping system was investigated because of such numerical conditions. First, the finite element model was improved using experimental data. Based on the detailed analytical model representing the experimental results, the difference in the seismic response analysis results of piping according to the mesh size was analyzed comparatively. Finally, the variability in the seismic fragility curve of the piping according to the convergence conditions was confirmed.
2. Derivation of Damage Index of Piping through Experiments
In general, the piping system connecting the two support points was composed of a straight pipe, branch pipe, and elbow. The elbow of the nuclear power plant piping system caused a leak through penetration cracks induced by fatigue failure accompanied by ratchets due to repeated excessive loads. The damage index of the piping is required to perform the seismic fragility analysis of the piping system. The damage index of the piping system was evaluated using extreme nonlinear analyses based on the results of the low cycle fatigue test for a 3-inch pipe elbow.
2.1. In-Plane Cyclic Loading Tests of 3-Inch Elbow Element
ASME/ANSI 3-inch standard piping was used to minimize the manufacturing errors and material uncertainty. A straight pipe of sufficient length of three times (270 mm) or more in diameter was attached to the elbow by welding to allow plastic behavior in the pipe elbow. As shown in
Figure 1 and
Figure 2, it was processed to implement a pin connection at both ends of the specimen and combined with a universal testing machine UTM (Universal Testing Machine).
The repeated displacement test for a constant amplitude was performed on the elbow element, as shown in
Table 1. A pressure of 3 MPa was applied to all samples, and a repeated force was applied for displacements of ±20 mm to ±100 mm, so sufficient nonlinear behaviors could be captured until leakage occurred. The weakest point of the pipe was the crown and the center of the elbow. A previous study reported that the strain in the hoop direction has a significant effect on damage [
2]. Therefore, the strain in the crown region was measured using a strain gauge and a vision-based system based on image signal processing. In this study, the fracture mode of the pipe is defined as a leak caused by cracking. A repeated force test was performed until cracking occurred.
Figure 3 shows the composition of the piping element test, including the crack and leak in the pipe elbow.
Table 2 lists the results of repeated force experiments in which cracking occurred.
2.2. Quantitative Failure Criteria Based on the Strain-Stress Relation
In this study, the failure criterion of the piping was defined using Equation (1) which applies the stress–strain relation reported by Bannon. In Equation (1),
ϵy and
σy are the yield strain and yield stress, respectively;
ϵi and
Ei are the strain and dissipation energy of the N
th cycle, respectively. The constants c and d are 0.3 and 3.5, respectively [
20].
The hoop directional stress and strain were calculated using finite element analysis, as shown in
Figure 4, and the damage was evaluated from the dissipated energy.
Cracks in the pipe elbow occurred on the inner surface of the crown and grew axially. Hoop strain was dominant. Hence, the hoop strain was used to define the failure of the pipe elbow. The numerical analysis model of the piping was constructed using shell elements. The mesh size was composed of 10–16 elements and 45–60 elements in the longitudinal and circumferential directions, respectively, and analysis was conducted under the same conditions as the test.
Figure 5 compares the response of the ±60 mm test case. In the case of the force–displacement relation, the analysis results and test results showed good agreement. The damage index was calculated using Equation (1) from finite element analysis, and the average of the damage index was 35.25, as shown in
Figure 6.
3. Seismic Performance of Piping Systems According to the Numerical Analysis Conditions
3.1. Finite Element Analysis Model and Seismic Response Analysis of a Piping System
Seismic response analysis was performed on piping installed in the containment building to which the seismic isolation system had been applied. The NRC-BNL benchmark model [
18] was used for the pipe model, and an isolator was applied to the lower part of the containment structure. The containment structure and piping were connected, as shown in
Figure 7.
Table 3 shows the boundary conditions for isolated containment structures and piping systems. The seismic isolation device was assumed to behave linearly, and the natural frequency of the isolated structures was designed to be 0.5 Hz. Carbon steel of ASME (B36.10 M, SA106, Grade b, SCH 40) was used, and the material properties are shown in
Table 4 [
21]. The outer diameter of the pipe was 323.85 mm, the thickness was 9.525 mm, and the radius of the curved pipe was 457.2 mm. The damping ratio was assumed to be 4% (Rayleigh damping), referring to the damping ratio of the SSE (Safe Shutdown Earthquake)-based piping systems in Regulatory Guide 1.61 [
22]. The responses of the structure and piping were derived by performing seismic response analysis unidirectionally (Z-axis).
The five earthquake input motions that satisfy the requirements of ASCE 43-05 and the response spectrum of Regulatory Guide 1.60 were generated [
23].
Figure 8 shows the target response spectrum for the horizontal unidirectional direction (Z direction) and the response spectrum for the generated input earthquake.
Table 5 lists the information on the seed earthquake.
Detailed finite element analysis of the piping was performed from the seismic response analysis results of the model, in which the structure and piping were connected. Shell elements express the elliptic deformation and distortion behavior in the detailed finite element analysis of piping. The displacement response was derived from the location where the piping was installed in the structure and entered to the support of the piping system. The nonlinear seismic response analysis of the piping system was performed in the following order: (1) First, the design internal pressure was applied, and (2) seismic response analyses (direct integration method) were performed while maintaining the stress due to the internal pressure.
The pressure applied inside the piping was calculated using Equation (2), which is represented in the Boiler & Pressure Vessel Code of ASME (American Society of Mechanical Engineers):
where
σdesign is a design stress intensity value;
Ip is the design internal pressure;
t is the thickness of the pipe;
d is the diameter of the pipe.
The design stress intensity value was 110 MPa, and the internal pressure was 6.31 MPa, and were applied to the pipe system, referring to the Boiler & Pressure code.
Figure 9 presents the natural frequency and mode shape of the piping. The natural frequencies of the primary and secondary modes were 4.965 Hz and 9.196 Hz, respectively.
3.2. Effect of Number of the Mesh (Mesh Size) for Piping System
The piping system was modeled as a shell to examine the changes in the stress and strain of the pipe according to the change in mesh size. Such a numerical model was verified by a comparison with the test results in
Section 2.2. The weak part of the piping is the elbow part. Therefore, the number of elements in the longitudinal and circumferential directions of the shell elements of the pipe elbow was adjusted. As shown in
Figure 10, numerical analysis was performed by dividing the length direction and circumferential direction from 2 to 10 elements and 8 to 32 elements, respectively. All conditions except the number of elements for a pipe elbow were applied in the same way to check only the change in the stress and strain of the pipe according to the number of meshes (mesh size).
Point 1 in
Figure 10 was installed on the ground; the other locations were installed in the building. The positions constrained in the Z direction were points 3 and 7. The elbow crown between points 2 and 3 was identified as the most vulnerable. The stress and strain were derived, as shown in
Figure 11 and
Figure 12.
Table 6 and
Table 7 list the maximum values of strain and stress for the size of the mesh. As shown in
Figure 11, the change in the size of elements in the longitudinal direction confirmed that the response increased with increasing number of elements in the longitudinal direction. A test on the number of elements in the circumferential direction confirmed that the response increases with increasing number of elements, as shown in
Figure 12. The area where the stress is concentrated decreases with increasing number of elements, and the response tends to increase.
3.3. Effect of Convergence for Piping System
The seismic performance of piping according to the convergence conditions of nonlinear dynamic analysis was analyzed. The Newton-Raphson methodology was used as a convergence method for nonlinear dynamic analysis. In the piping system model, the number of meshes in the elbow was 8 in the longitudinal direction and 12 in the circumferential direction. Convergence “condition A” was performed with a forced convergence when repeated more than 16 times, and convergence “condition B” was performed with forced convergence when repeated more than 48 times. Nonlinear seismic response analysis compared the convergence “condition A” and convergence “condition B” to confirm the change in the result according to the convergence condition. The elbow crown between points 2 and 3 was identified as most vulnerable.
Figure 13 compares the strain and stress of convergence “condition A” and convergence “condition B” in the elbow crown caused by the Northridge earthquake. To compare the analysis results of convergence “condition A” and convergence “condition B”, the percentage difference was calculated using Equation (3), and the RMS (Root Mean Square) difference was calculated using Equation (4).
where
n is the number of analysis data;
A is the response analyzed by convergence “condition A”; and
B is the response analyzed by convergence “condition B”. The stress and strain of the piping were checked by varying the five input earthquakes and the PGA (Peak Ground Acceleration) level (1 g, 2 g, and 3 g).
Table 8 compares the stress and strain calculated through nonlinear dynamic analysis of the pipe. The average percentage difference in strain was 6.38%, and the RMS difference in strain was 0.006227. The average percentage difference was 25.58% in stress, and the RMS difference in stress was 153.61 N/mm
2. Even if the PGA was the same earthquake, the response varied according to the earthquake. If the input earthquake was the same, the difference in response increased with increasing size of the PGA. Therefore, the difference in response is dependent on the size of the PGA and input earthquake.
The seismic performance of piping under two different convergence conditions was analyzed. A seismic fragility curve was calculated to assess the seismic performance of the piping system, and the seismic fragility was determined using the procedure in
Figure 14. First, a piping system was selected to analyze the seismic fragility, and the most vulnerable part of the piping elements was identified. The finite element model was then updated for the numerical analysis using the cyclic loading test for the weak piping elements. The response of the piping installation position was derived from the experiments and the numerical analysis of the building. Finally, the seismic fragility curves were derived using the damage index that indicated the failure of the piping systems.
The seismic fragility curve of the piping was checked by varying the five input earthquakes and PGA levels (1 g, 2 g, and 3 g). The damage index was 35.25, which was calculated in
Section 2. The seismic fragility curve was represented by a lognormal distribution, which confirmed a difference between the results of convergence “condition A” and “condition B”, as shown in
Figure 15. Therefore, when deriving the seismic performance of piping through numerical analysis, differences occur in the results depending on the convergence conditions. The median value of the seismic fragility curve under convergence “condition A” and “condition B” was 2.8 g and 2.4 g, respectively, showing a difference of 0.4 g. Therefore, in this study, the seismic performance of the pipe was overestimated when the iteration is small for convergence.
4. Conclusions
This study examined the effect of evaluating the seismic performance of piping by varying the numerical analysis conditions, i.e., a mesh size and convergence conditions in the nonlinear dynamic analysis (seismic response analysis). Pipe damage was defined as leakage caused by penetrating cracking. A low cycle fatigue test of a 3-inch elbow was performed to quantify piping damage and verify the finite element model of piping. Dynamic tests were performed until piping leakage occurred under various conditions. A finite element model of piping was developed and verified with test results. The damage index of the leak point due to the penetrating cracks was calculated using Bannon’s method from the test and numerical analysis results of the piping.
A numerical model was constructed for the piping system installed in the isolated containment building, and seismic response analysis was performed by varying the number of meshes. The stress and strain were lower when the number of elements was small based on numerical analyses. The seismic performance of the piping was underestimated when a small number of elements were used. On the other hand, the strain and stress were overestimated when a large number of elements were used, but the difference was negligible compared to the dynamic test result. Therefore, evaluating the seismic performance of piping using a numerical model with a small size of elements results in a slight overestimation of the actual results.
The seismic performance of piping according to the convergence conditions of nonlinear dynamic analysis was analyzed. Convergence “condition A” was forced convergence when repeated more than 16 times, and convergence “condition B” was forced convergence when repeated more than 48 times. Seismic response analysis was performed with five input earthquakes and several PGA levels (1 g, 2 g, and 3 g) to evaluate the seismic fragility curve of the piping system. The seismic response was similar between convergence “condition A” and convergence “condition B”, but a difference occurred in the stress–strain curves of the two conditions. As the damage index of the pipe utilizes the stress–strain curve, a difference occurred in the seismic fragility curves of the two conditions. The seismic capacity of the pipe increased with decreasing number of iterations of the convergence condition. Therefore, when performing numerical analysis, the convergence condition needs to be checked. In particular, when considering the actual failure, i.e., leakage through a crack, convergence should be checked for a large input motion that could cause failure.
Overall, the seismic performance of the piping could differ according to the numerical conditions of the piping. Moreover, the seismic performance of the piping can be overestimated if the number of elements and convergence are insufficient. Therefore, an appropriate number of elements and convergence conditions are required when evaluating the seismic performance of a pipe using a numerical analysis technique.
Author Contributions
Formal analysis, B.J., D.H. and S.E.; Writing—original draft, S.C., B.J., D.H. and S.E.; Writing—review & editing, S.K. and S.E. All authors have read and agreed to the published version of the manuscript.
Funding
This research was funded by KETEP, grant number 20201510100010, and also this research was funded by NRF, grant number 2020R1G1A1007570.
Acknowledgments
This study was supported by the Korea Institute of Energy Technology Evaluation and Planning (KETEP) and the Ministry of Trade, Industry & Energy (MOTIE) of the Republic of Korea (No. 20201510100010). This work was also supported by the National Research Foundation of Korea (NRF) grant funded by the Korean government (No. 2020R1G1A1007570).
Conflicts of Interest
The authors declare no conflict of interest.
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Figure 1.
Test specimen and connection jig.
Figure 1.
Test specimen and connection jig.
Figure 2.
Test specimen on UTM.
Figure 2.
Test specimen on UTM.
Figure 3.
Cracks and leaks by in-plane cyclic loading test.
Figure 3.
Cracks and leaks by in-plane cyclic loading test.
Figure 4.
Finite element analysis model of the pipe specimens.
Figure 4.
Finite element analysis model of the pipe specimens.
Figure 5.
Comparison of the experimental and finite element analysis results: (a) comparison of the force–displacement response; (b) comparison of the strain response.
Figure 5.
Comparison of the experimental and finite element analysis results: (a) comparison of the force–displacement response; (b) comparison of the strain response.
Figure 6.
Damage index of a carbon steel pipe elbow.
Figure 6.
Damage index of a carbon steel pipe elbow.
Figure 7.
Isolated containment structure and piping system: (a) connection of the isolated structure and piping system; (b) isolated containment structure; (c) piping system.
Figure 7.
Isolated containment structure and piping system: (a) connection of the isolated structure and piping system; (b) isolated containment structure; (c) piping system.
Figure 8.
Response spectra of the generated input earthquakes and target response spectrum.
Figure 8.
Response spectra of the generated input earthquakes and target response spectrum.
Figure 9.
Natural frequency and mode shape of the piping system: (a) 1st mode; (b) 2nd mode.
Figure 9.
Natural frequency and mode shape of the piping system: (a) 1st mode; (b) 2nd mode.
Figure 10.
Pipe finite element model according to the number of elements.
Figure 10.
Pipe finite element model according to the number of elements.
Figure 11.
Comparison according to the change in the lengthwise element size: (a) stress; (b) strain.
Figure 11.
Comparison according to the change in the lengthwise element size: (a) stress; (b) strain.
Figure 12.
Comparison according to the change in the circumferential element size: (a) stress; (b) strain.
Figure 12.
Comparison according to the change in the circumferential element size: (a) stress; (b) strain.
Figure 13.
Comparison of the convergence “condition A” and convergence “condition B” analysis results (Northridge earthquake): (a) comparison of the stress (PGA level: 1 g); (b) comparison of the strain (PGA level: 1 g); (c) comparison of the stress (PGA level: 2 g); (d) comparison of the strain (PGA level: 2 g); (e) comparison of the stress (PGA level: 3 g); (f) comparison of the strain (PGA level: 3 g).
Figure 13.
Comparison of the convergence “condition A” and convergence “condition B” analysis results (Northridge earthquake): (a) comparison of the stress (PGA level: 1 g); (b) comparison of the strain (PGA level: 1 g); (c) comparison of the stress (PGA level: 2 g); (d) comparison of the strain (PGA level: 2 g); (e) comparison of the stress (PGA level: 3 g); (f) comparison of the strain (PGA level: 3 g).
Figure 14.
Procedure for calculating the seismic fragility curve of a piping system.
Figure 14.
Procedure for calculating the seismic fragility curve of a piping system.
Figure 15.
Seismic fragility curve of the piping system due to the convergence condition.
Figure 15.
Seismic fragility curve of the piping system due to the convergence condition.
Table 1.
Pipe element test cases.
Table 1.
Pipe element test cases.
Number of Specimens | 6 | 5 | 5 | 5 | 6 | 5 | 7 | 5 | 5 |
---|
Amplitude (mm) | ±20 | ±30 | ±40 | ±50 | ±60 | ±70 | ±80 | ±90 | ±100 |
Loading condition | Constant amplitude cyclic loading |
Pressure | 3 MPa |
Failure mode | Leakage by low-cycle fatigue |
Table 2.
Results of the pipe element test.
Table 2.
Results of the pipe element test.
Mode | Amplitude | Leakage Nth Cycle | Avg. Leakage Cycle |
---|
Cyclic mode | ±20 mm | 82, 108, 110, 87, 76, 98 | 94 |
Cyclic mode | ±30 mm | 45, 46, 29, 29, 38 | 37 |
Cyclic mode | ±40 mm | 17, 18, 18, 14, 15 | 16 |
Cyclic mode | ±50 mm | 11, 10, 11, 9, 12 | 11 |
Cyclic mode | ±60 mm | 6, 6, 8, 8, 8, 8 | 7 |
Cyclic mode | ±70 mm | 4, 5, 5, 4, 6 | 5 |
Cyclic mode | ±80 mm | 5, 4, 4, 5, 4, 4, 5 | 4 |
Cyclic mode | ±90 mm | 4, 4, 4, 4, 4 | 4 |
Cyclic mode | ±100 mm | 4, 3, 4, 4, 3 | 3 |
Table 3.
Boundary condition of the piping system.
Table 3.
Boundary condition of the piping system.
Support ID | Restraint Direction |
---|
1, 7 |
X, Y, Z, RX, RY, RZ
|
4, 5, 6 |
X, Y
|
3 |
X, Z
|
2 |
Y
|
Table 4.
Material properties of the piping system.
Table 4.
Material properties of the piping system.
Density (N/mm3) | E (Mpa) | Poisson’s Ratio | Damping (%) |
---|
7.85 × 109 | 203,509 | 0.3 | 4 |
Table 5.
Characteristic of the seed earthquake.
Table 5.
Characteristic of the seed earthquake.
No | Earthquake | Station | Inter/Intra | Mw | Distance (km) |
---|
1 | Northridge | PKC | Inter | 6.69 | 7.26 |
2 | Kobe | KIMA | Inter | 6.90 | 0.96 |
3 | Chi-Chi, Taiwan | TCU072 | Inter | 7.62 | 7.03 |
4 | Nahanni | S3 | Inter | 6.76 | 5.32 |
5 | Superstition Hills-02 | ICC | Inter | 6.54 | 18.2 |
Table 6.
Comparison of the maximum stress in the piping system.
Table 6.
Comparison of the maximum stress in the piping system.
| Circumferential Direction | 8 | 12 | 16 | 20 | 24 | 28 | 32 |
---|
Longitudinal Direction | |
---|
2 | 717.30 | 809.36 | 888.78 | 942.73 | 966.90 | 977.15 | 985.74 |
4 | 809.36 | 910.79 | 997.27 | 1016.80 | 1028.67 | 1047.93 | 1055.50 |
6 | 855.45 | 947.44 | 1008.06 | 1035.75 | 1050.84 | 1060.84 | 1070.18 |
8 | 863.42 | 941.10 | 1014.53 | 1049.26 | 1063.00 | 1072.79 | 1081.76 |
Table 7.
Comparison of maximum strain in the piping system.
Table 7.
Comparison of maximum strain in the piping system.
| Circumferential Direction
| 8 | 12 | 16 | 20 | 24 | 28 | 32 |
---|
Longitudinal Direction | |
---|
2 | 0.0825 | 0.1031 | 0.1294 | 0.1420 | 0.1495 | 0.1531 | 0.1561 |
4 | 0.1095 | 0.1343 | 0.1535 | 0.1630 | 0.1685 | 0.1716 | 0.1745 |
6 | 0.1169 | 0.1404 | 0.1594 | 0.1690 | 0.1746 | 0.1783 | 0.1817 |
8 | 0.1196 | 0.1398 | 0.1616 | 0.1727 | 0.1778 | 0.1814 | 0.1848 |
Table 8.
Difference in the stress and strain of piping according to the convergence conditions.
Table 8.
Difference in the stress and strain of piping according to the convergence conditions.
| Strain | Stress |
---|
Percent Difference (%) | RMS Difference (%) | Percent Difference (%) | RMS Difference (%) |
---|
Northridge_1 g | 1.43 | 0.002037 | 17.72 | 104.68 |
Northridge_2 g | 4.84 | 0.004589 | 30.69 | 155.18 |
Northridge_3 g | 11.14 | 0.008327 | 24.88 | 148.84 |
Kobe_1 g | 2.07 | 0.002687 | 21.25 | 113.54 |
Kobe_2 g | 8.08 | 0.006801 | 22.08 | 133.63 |
Kobe_3 g | 20.08 | 0.013299 | 31.91 | 173.64 |
Chi-Chi, Taiwan_1 g | 2.91 | 0.003632 | 23.71 | 154.42 |
Chi-Chi, Taiwan_2 g | 7.84 | 0.007553 | 28.41 | 191.15 |
Chi-Chi, Taiwan_3 g | 6.75 | 0.008519 | 28.33 | 203.48 |
Nahanni_1 g | 3.57 | 0.004282 | 20.37 | 112.74 |
Nahanni_2 g | 4.37 | 0.005704 | 22.43 | 134.46 |
Nahanni_3 g | 6.15 | 0.007987 | 24.23 | 149.98 |
Superstition Hills-02_1 g | 1.78 | 0.002779 | 26.99 | 153.28 |
Superstition Hills-02_2 g | 4.90 | 0.005614 | 26.65 | 169.50 |
Superstition Hills-02_3 g | 9.80 | 0.009599 | 34.10 | 205.60 |
mean | 6.38 | 0.006227 | 25.58 | 153.61 |
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