The results are presented following the two pathways in
Figure 2. The first path provides the results for the RDSM determined directly from the total damage energy output. The second path presents the mechanism RDSM formulations and characterization performed using the individual damage mechanism energy outputs. A third section compares the two methods of RDSM formulation. RDSM formulation for both pathways was based on the 1555 FE results obtained from the source model and sampled with all 41 parameters. As shown in
Figure 7, the total energy varies throughout the parameter space as do the contributions of the damage mechanisms. It should be noted that
DI contributed up to 7.6% for some parameter combinations comprising a small subspace of the entire parameter space and confirming the importance of characterizing the damage mechanisms separately to ensure adequate sampling in small but significant subspaces. (A subspace is defined as a distinct region within the full parameter space.) Overall,
PM dominated the parameter space. The next two highest energy contributors were
PL and
DC.
3.1. Direct RDSM Formulation
A surrogate model with all 41 input parameters as variables was generated using the FE source model dataset. The output layer consisted of a single output, the
TS energy absorption. The dataset consisted of 1555 data points, and 25 of these points were randomly selected to create a validation set. The remaining 1535 data points were split into testing and training data with a 10/90 split. KerasRegressor with two hidden layers of 60 and 80 nodes required the use of an Adam optimizer, a normal initializer, and a ReLU activator. The learning rate was set to 0.001. The surrogate model resulted in a mean absolute error (MAE) of 3.45%. The accuracy of the resulting
TS surrogate model is illustrated in
Figure 8, which presents a 45° plot of the 25 randomly saved validation data points. The plot shows the predicted results from the
TS surrogate model versus the values calculated by the FE source model. Predictions fall within 5% error of the actual with only three data points outside of this bound. These three outliers fell within 10% of the calculated FE results. Given the complexity of the parameter space and the limited data sampling, this accuracy was considered adequate to avoid overfitting the model with additional training. It should be highlighted that development of the surrogate model was user- and time-intensive due to the number of parameters.
GSA to calculate Sobol’ indices was performed using the
TS surrogate model to inform parameter space reduction. The first-order and total-order Sobol’ indices of all 41 input parameters were calculated with regards to the
TS parameter space (
Figure 9). Adequate convergence was achieved with 10,000 samples as results with 200,000 samples exhibited no deviations in the controlling parameters or their minimal interactions. The top four most influential parameters were
A,
E,
XS, and
Aln. Three of the four most influential parameters (
A,
E, and
Aln) represent
PM, the most dominant damage mechanism. The strength coefficient,
B, which is the other parameter representing
PM, is within the eight most influential parameters. Shear properties of the resin,
XS,
P, and
GII were in the top six most influential parameters. Minimal interaction was indicated between the dominant parameters when comparing first-order and total-order indices. Large drops in the index values are evident after the first- and fourth-highest contributors.
Sobol’ indices’ calculation was manually intensive and time-consuming. Therefore, FDR logworth was performed to explore its potential as a screening tool to reduce the parameter space prior to surrogate modeling and GSA.
Table 6 compares the total-order index from Sobol’ indices to the FDR logworth values. Both methods identically ordered the most influential parameters and captured the drops after the first and fourth dominant parameters. FDR logworth provided comparable information regarding the importance of the parameters at a significantly reduced computational cost. As such, FDR logworth was employed for parameter space reduction prior to mechanism RDSM formulation.
UQ was conducted on the most influential parameters to determine which parameters to include in the RDSM. Beginning with only the most dominant parameter,
A, the surrogate model was queried by varying only the parameter(s) under consideration while the remaining parameters were held constant at their mean values. Next, the top two parameters were varied and so on until minimal error with the inclusion of the next parameter as a variable was achieved. Convergence dictated that 5000 data points were needed for UQ. Negligible change in the mean
TS prediction was observed when only the most dominant parameter
A was included in the RDSM (
Table 7). As the standard deviation exhibited notable improvements until the addition of the fifth most influential parameter, the top four parameters were included in the
TS RDSM which was generated as part of the UQ.
The RDSM formulated with the top four influential parameters as variables was used to map the
TS parameter space (
Figure 10). The 2D plots along the diagonal map each of the four parameters against the
TS damage energy. As predicted by GSA, minimal interaction is indicated by the near linear gradations in all of the plots.
3.2. Mechanism RDSM Formulation and Characterization
Based on the previous results, FDR logworth was used as a screening tool to reduce the number of parameters prior to formulation of the surrogate models for each damage mechanism. This parameter reduction enabled an initial formulation of the mechanism RDSMs based on a reduced parameter set, eliminating the need to create a surrogate model based on all 41 parameters. The FDR logwoth measures for each damage mechanism are provided in
Table 8. An FDR logworth value of 1.3 (
p-value of 0.05) was considered potentially significant and included in the initial RDSM formulation. As seen in
Table 8, there are considerable drop-offs in the FDR logworth values after the first few parameters for each damage mechanism. Additional investigation demonstrated that only the parameters before this drop significantly influenced RDSM accuracy. As a result, at most three parameters per damage mechanism were included in the mechanism RDSM formulations. This substantial reduction in variables based on FDR logworth screening decreased RDSM formulation time to the extent that this approach could be readily and rapidly applied to existing datasets. The reduced parameter space for each of the damage mechanisms is highlighted in
Table 8.
In general, mechanism RDSMs exhibited higher MAEs than the
TS RDSM (
Table 9). Parameter sampling was uniform across the entire parameter space; however, individual mechanism contributions and their gradients varied significantly throughout the parameter space (as will be demonstrated). For improved RDSM accuracy, adequate data are needed within each mechanism subspace (the region within the parameter space where a damage mechanism significantly contributes). This issue was highlighted in the initial attempt at RDSM formulation for the
DI subspace, which comprised a much smaller region within the parameter space than the other mechanisms. As will be discussed, the
DI damage energy was zero or near zero within most of the parameter space, with a very limited subspace in which
DI significantly contributed to the total damage energy. This scenario hindered surrogate model generation, even with a reduced number of parameters, as the formulation process skewed to the data with zero contribution. Thus, the ANN fit the surrogate model to the much larger non-contributing region of the parameter space, thus inadequately capturing
DI contributions within the subspace of significant damage energy. As such, it was not possible to formulate a RDSM with the available dataset. Additional sampling and FE analysis with the source model using only the most influential
DI parameters according to the FDR logworth results was required to provide adequate output data in the
DI subspace to then formulate a RDSM.
The mechanism RDSMs were constructed with the same surrogate modeling process as the
TS model, as detailed in
Section 3.1. The primary difference in the mechanism RDSM formulation was that parameter reduction was performed prior to surrogate modeling. The
PM,
PL, and
DL parameter spaces were reduced to three input parameters and one output, while the
DC parameter space was reduced to two input parameters and one output. The MAE for each of the mechanism RDSMs is provided in
Table 9. The
PM RDSM exhibited the lowest error, because this damage mechanism was dominant across the entire parameter space, and thus more uniformly sampled than the other mechanisms. The collection of additional data to improve the
DL RDSM was discussed; however, it was not performed as the summed RDSM error was comparable to that of the
TS RDSM.
To characterize the damage mechanism behaviors, Sobol’ indices were calculated using data generated from the mechanism RDSMs.
Figure 11 shows parameter interactions for all mechanisms except
PM.
Figure 11a for
PL illustrates some interactions between
E1800,
XS, and
X1800, and
Figure 11b shows interaction between
XS and
E1800 in the
DL subspace, while
X7781 is independent. Given that
XS is dominant in two subspaces, it is not surprising that it was one of the top four influential parameters in
TS. The
DC subspace (
Figure 11c) shows that the two dominant parameters,
E1800 and
X1800, are interacting and that
E1800 has a significantly stronger influence on the delamination. Lastly, the
PM subspace (
Figure 11d) shows no parameter interactions with
A as the most dominant parameter followed by
E and
Aln, consistent with the GSA results for
TS.
The 3D contour graphs were generated for each mechanism to identify subspace locations and to understand parameter interactions (
Figure 12 and
Figure 13). Each mechanism RDSM was used to generate a 3D mesh grid consisting of 9261 datasets to uniformly and systematically capture the mechanism subspace. If the mechanism had a third dominant parameter, it was set at its minimum value when comparing the two other parameters.
PL (
Figure 12a) exhibits two distinct regions of low and high shear plasticity energy. The lower region is dominated by low values of
E1800 and
XS. The higher energy region corresponds to high values of
E1800 and
XS and low values of
X1800.
DL (
Figure 12b) highlights that the intralaminar fracture of the composite overlay is controlled by the shear strength of the resin matrix,
XS. This is noted by the large change in energy along its axis compared to the other two parameters,
X7781 and
E1800. A higher
XS requires a larger amount of energy for the damage to propagate through the laminae layers. This is mirrored with the tensile strength of the Hexcel 7781 layer, the outside ply, and
E1800 corresponding to the remaining interior layers carrying the stress after the outer plies fail.
Figure 12c for the
PM subspace illustrates that
A is the dominant parameter with no interaction between the parameters. The metal substrate absorbs more energy when it is a stiffer less formable metal, providing it does not fracture. Increasing the yield stress and Young’s Modulus and decreasing the metal’s formability (
Aln) will result in less deformation, allowing for the metal to absorb more energy before the outer composite overlay plies fail.
Figure 13 shows that in the
DC subspace, the delamination between the plies is controlled by the interior E-LT 1800 plies. As the stiffness of the plies is decreased, more deformation occurs leading to the resin carrying a larger stress. Increased delamination occurred with low
E1800 and high
X1800.
DI Subspace Reduced-Dimension Surrogate Modeling and Characterization
As previously stated, the initial RDSM formulation for the
DI subspace was not successful. Given the high distribution of the data as zero damage contribution, further FDR logworth was performed (
Table 10) to separate the engaged (contributes 3% or more to total damage) and nonengaged (zero or <3%) regions. From these results, 12 parameters from the engaged group were selected for additional data generation to better sample the subspace where
DI is active. While only three parameters were located above the drop applied previously, given the uncertainty in identifying the engaged subspace, the additional nine parameters were included in the sampling. Data acquisition followed the same procedure as that of the original data generation, except that only the 12 selected parameters were varied, while the remainder of the variables were held constant at their mean values. To expedite the data collection process, HPC was used to generate 3277 data points. The explicit FE source model required around 120 min per analysis to run locally but was reduced to 38 min on HPC systems. The dataset from the new sampling still resulted in many zero or near-zero outputs that continued to challenge RDSM formulation. Therefore, the 3% limit was again applied (8 joules of
DI) and only the data above this value were included in the RDSM formulation (793 data points). The initial RDSM consisted of a surrogate model following the same framework presented in
Section 3.1. For this RDSM, the 41 input parameters were reduced to 12 input parameters, and the output consisted of one variable (
DI). The dataset consisted of 793 data points and utilized a 20/80 split for testing and training. A learning rate of 0.0015 was set for the model. A resulting feedforward surrogate with two layers of 16 neurons resulted in a MAE of 8.45%.
Both FDR logworth and GSA (Sobol’ indices) were performed with data generated from this RDSM (
Table 11). Both are in agreement for the top three dominant parameters,
P,
XS, and
GiII, with
GiII replacing
GII from the original analysis, exemplifying the importance of an adequate number of data points in the region under consideration. These top three influential parameters then comprised the final
DI mechanism RDSM.
Figure 14 shows the point cloud for these parameters from varying angles allowing for visualization of the significant interactions between the parameters. As the RDSM was formulated only for the engaged region, it was necessary to create a function based on the parameter ranges when
DI is active. This plane was bound by a set of coordinates (
P,
XS,
GiII): (0.4, 0, 0), (0, 0.5, 0), (0.85, 0.3, 1), and (0, 1, 1). If the data point fell on the left side of this plane, the RDSM reported a zero-energy value. If the data were on the right side, the
DI RDSM is included in the total energy analysis.
3.3. Comparison of the TS to the Summed Reduced-Dimension Surrogate Model
To evaluate the accuracy of the direct versus the summed approach, the final
TS RDSM was compared to the summed RDSM (the summation of the mechanism RDSMs). (A linear summation inherently captured interactions between the damage mechanisms as all output energies were obtained simultaneously from the source model simulations.) The
TS RDSM was constructed with only 4 of the 41 input parameters (
A,
E,
XS, and
Aln), while the summed mechanism RDSM included 9 of the 41 input parameters (
A,
E,
Aln,
X1800,
E1800,
X7781,
P,
XS, and
GiII). Both RDSMs were compared to the saved 25 data points from the initial FE predictions as well as an additional 200 data points generated separately for a total of 225 validation points (
Table 12). The MAE of the summed approach was 5.78%, comparable to the 5.45% of the direct approach. For the validation points in the
DI subspace, the summed RDSM outperformed the direct RDSM, with 4.63% and 5.51%, respectively.
Figure 15a,b present the 45° validation plots using all 225 points. This result highlights that the summed approach is comparable in accuracy to the direct approach. Additionally,
Figure 15c,d, showing the validation data in the engaged
DI subspace only, clearly demonstrate the prediction improvement due to additional sampling in the mechanism subspaces during summed RDSM formulation.