3.1. FullSWOF-ZG Validation Results of Curb Inlet Efficiency
For the 20 modeling cases conducted for the type D inlet, geometry (
S0,
Sx, and
Lci) and flow (
Qin and
T) parameters have been listed in
Table 2, and the same for the experimental conditions [
7,
21], which cover five longitudinal slopes (0.004–0.06), two cross slopes (0.0208 and 0.0407), 17 spreads (1.05–4.27 m), and 19 upstream inflows (0.0285–0.2597 m
3/s).
Table 2 shows that simulated intercepted flows (
Qcis) and inlet efficiencies (
Ecis) matched well with the observed results (
Qcio and
Ecio) from the laboratory experiments conducted by Hammonds and Holley [
7]. The coefficient of determination (
R2) of the linear relationship between simulated and observed
Eci is 0.99. The differences (Δ
E in
Table 2) of simulated and observed
Eci ranged from −2.28% to 4.21% with average ± standard deviation as 1.10% ± 1.67%. The percent differences (
PDE) of simulated and observed
Eci ranged from −3.15% to 5.17% with average ± standard deviation as 1.57% ± 2.29%. Therefore, the FullSWOF-ZG program can accurately simulate the overland flow through the road surface, gutter, local depressions (transition), and the flow interception over Type D curb inlets, and predict the curb inlet interception efficiency well.
The simulation results in
Table 2 were first developed using the cell size of 0.076 m (0.25 ft) for square computational grids. Three other cell sizes (0.05 m, 0.025 m, and 0.01 m) were then used for 10 modeling cases of undepressed inlets (O10X10L1–O10X10L10 in
Table 1) to conduct the cell size sensitivity analysis on a ThinkStation Desktop computer with central processing unit (CPU) type of Intel(R) Xeon (R) E3-1241 v3 3.5 GHz. For these three cell sizes, the total number of cells in the simulation domain (12 × 6.7 m) was 32,160, 128,640, and 804,000, respectively. For the 10 cases with a cell size of 0.05 m, the simulation time ranged from 0.15 h to 0.17 h with an average simulation time equal to 0.15 h. For the 10 cases with a cell size of 0.025 m, the simulation time ranged from 1.23 h to 1.43 h with an average simulation time equal to 1.27 h. For the 10 cases with a cell size of 0.01 m, the simulation time ranged from 26.3 h to 26.4 h. The cell size of 0.025 m (~1 inch) was chosen as the simulation cell size for simulations of all other modeling cases in this study based on the balance of the model accuracy in predicting
Qci and
Eci and the simulation time for the 10 test cases above.
3.2. Validation Results of 100% Intercepted Curb Inlet Length
The simulated water surface profile along the curb inlet was outputted and used by a MATLAB code to determine the 100% interception curb inlet length
LT.
Figure 2a shows six examples of the simulated water surface profile along the curb for six selected
LT validation cases (WS11, 23, 34, 47, 56, and 73) out of 80 experiment tests (WS1–WS80) conducted by Wesley [
19]. Because the curb inlet opening starts at 9.75 m, the water depth drops sharply at the first 0.2 m of the curb inlet opening and then decreases slowly and linearly along the curb inlet. Finally, the water depth becomes very small (a thin layer of water) across the remaining inlet length. These water surface profiles along the curb inlet show similar variations with distance as reported by other research studies, such as Schalla [
16], Hodges et al. [
31], and Muhammad [
13], but are significantly different from the linear decrease assumption made and used by Izzard [
8] to develop the
LT equation.
Five depth limits (0.05 mm, 0.1 mm, 0.2 mm, 0.3 mm, and 0.5 mm) were tested to determine the end point of the 100% interception curb inlet length. The location of water depth, equal to the depth limit minus the curb inlet start location, was regarded as the 100% interception curb inlet length. The green solid vertical lines in
Figure 2a show the location of the water depth equal to the depth limit of 0.2 mm for these six example cases. The simulated curb inlet lengths of total interception for all 80 modeling cases of Wesley’s tests were determined using the five water depth limits and compared to
LT observed and determined in laboratory tests (
Figure 2b). The final water depth limit was chosen when the root-mean-square error (RMSE) and mean absolute percentage error (MAPE) of simulated and observed curb inlet lengths of total interception were the smallest. Simulated
LT values for the 80 cases/tests ranged from 1.30 m (4.3 ft) to 5.33 m (17.5 ft).
Figure 2b shows that the simulated
LT best matched with observed data when the depth limit for determining
LT was 0.2 mm. The RMSEs for the simulated
LT results with depth limits equal to 0.05, 0.1, 0.2, 0.3, 0.5 mm were 0.30 m, 0.28 m, 0.27 m, 0.29 m, 0.31 m, and 0.34 m, respectively. The corresponding MAPEs for the five depth limits are 7.32%, 6.46%, 6.04%, 6.08%, 6.34%, and 6.80%, respectively. Since the smallest RMSE and MAPE were for the depth limit of 0.2 mm, therefore, the water depth limit 0.2 mm was used for the one thousand modeling cases (O1X1Q1–O10X10Q10) to determine the 100% interception curb inlet lengths summarized in
Section 3.3.
Figure 3 shows the comparison of the observed 100% interception curb inlet lengths simulated by the FullSWOF-ZG model and calculated
LT results by three existing methods for the 80 Wesley’s lab tests. The RMSE values between observed and calculated
LT from HEC-22 (2009), Izzard (1950), and Muhammad (2018) are 0.56 m, 1.77 m, and 0.45 m, respectively. The corresponding MAPE values are 12.9%, 43.3%, and 7.9%, respectively. The sequence from the smallest to largest RMSE and MAPE values for simulated and calculated
LT results are Simulated < Muhammad < HEC-22 < Izzard. Izzard’s equation generally overestimates
LT for all validation cases.
3.3. Simulated Curb Inlet Lengths of 100% Interception
After
LT was determined for the 1000 modeling cases using FullSWOF-ZG, a generalized power relation, Equation (7) was chosen to develop the regression equation for
LT as a function of four input parameters (
Qin,
S0,
n, and
Sx).
Table 1 also shows
LT determined for 10 example cases (O
mX
mQ
m,
m = 1, 2, …, 10) using FullSWOF-ZG. In Equation (7) the Manning’s value
n and cross slope
Sx were grouped as one combined variable, the same as the HEC-22 Equation (3).
where
LT is the curb inlet length in m for 100% interception;
Sx and
S0 are the cross slope and longitudinal slopes of the road/street (
Table 1),
Qin is the upstream inflow rate from the road/street surface to the curb inlet in m
3/s (0.006–0.024,
Table 1), and
n (-) is Manning’s roughness of the road surface.
The variation inflation factors (VIF) among three input variables (
Qin,
S0, and
nSx) were calculated with MATLAB before developing the equation. The VIFs among the three variables are all equal to 1. This means the predictors are more related to the target variable
LT than they are to each other [
32], and the multicollinearity of three variables are not significant. The coefficient
k and exponents (
a,
b, and
c) were estimated using the multiple linear regression (MLR) method after the log transformation of Equation (7), and the resulting regression equation of
LT was:
The 95% confidence intervals for the coefficient k and exponents a, b, and c are [0.372, 0.404], [0.368, 0.376], [0.0977, 0.103], and [0.559, 0.568] with p-value < 0.0001, respectively. If LT is in feet and Qin is in ft3/s for English or US customary units, the coefficient k would be 0.337. Comparing Equation (8) with HEC-22’s LT Equation (3), the exponent of S0 in Equation (8) is 0.1 (1/3 of 0.3 in Equation (3)), and the coefficient is about a half. Muhammad’s LT Equation (5) made the coefficient to be much smaller (~1/8 of 0.817 in HEC-22), but other exponents are similar, in addition to having different exponents for n and Sx.
Figure 4a shows the comparison of fitted
LT calculated using Equation (8), and simulated
LT. The
R2 and RMSE between fitted and simulated
LT are 0.99 (
Figure 4a) and 0.13 m, respectively. The MAPE between fitted and simulated
LT is 2.34% for all 1000 cases. It shows the fitted
LT or predicted by the regression equation matched well with the simulated
LT when
LT < 5 m, while the difference between simulated and predicted
LT becomes larger when
LT > 5 m. The ratio (
Rlt) of fitted
LT calculated using Equation (8) and simulated
LT was computed for all 1000 modeling cases; then, the mean
Rlt and standard deviation for each 100 cases with the same
S0 were also calculated and plotted in
Figure 5. The ratio
Rlt ranged from 0.89 to 1.06 (maximum of 11% underestimate and 6% overestimate), and the 915 fitted
LT values were within 5% from simulated
LT (0.95 <
Rlt ≤ 1.05) for Equation (8).
Figure 4b shows a comparison of predicted
LT results with Izzard (1950), HEC-22 (2009), and Muhammad (2018) methods to the simulated results, and the corresponding predicted
LT in m has ranges of [1.12, 8.60], [0.78, 6.36], and [0.63, 6.27], respectively. The predicted
LT for all three methods had strongly linear correlations with simulated
LT with
R2 of 0.91–0.97. The MAPEs between predicted from HEC-22 (2009), Izzard (1950), and Muhammad (2018) and simulated
LT for all 1000 cases were 22.4%, 14.0%, and 32.3%, respectively; the corresponding RMSEs were 0.13 m, 0.22 m, and 1.01 m. The HEC-22 and Muhammad methods underestimate
LT with
Rlt ranging from 0.48 to 0.92 (0.78 ± 0.10 for average and standard deviation) and from 0.39 to 0.84 (0.68 ± 0.09), respectively. The
Rlt range for Izzard method was [0.70, 1.28] with an average and standard deviation of 1.08 and 0.13. For the Izzard method, 771 cases overestimated the simulated
LT.
Figure 5 shows the average plus/minus the standard deviation of
Rlt for Equation (8), Izzard (1950), HEC-22 (2009), and Muhammad (2018) with respect to different
S0 values. All mean
Rlt ratios were within the range [0.95, 1.05] with small standard deviations (0.02–0.03) for fitted Equation (8), which indicate that the Equation (8) matches very well with simulated
LT for all
S0 conditions. For HEC-22 and Muhammad methods,
Rlt < 0.95 for all
S0 situations and the Muhammad method has a larger standard deviation (0.05–0.07), which means the HEC-22 and Muhammad methods underestimate
LT in a greater extent under smaller
S0 situations. For the Izzard method, most of
Rlt > 1 (overestimates
LT) when
S0 ≥ 0.3%, and it underestimates
LT when
S0 < 0.3%. For three previous methods, the mean
Rlt strongly correlates with
S0 as a power function with
R2 > 0.97 (
Figure 5):
Rlt increases with the increase of
S0.
3.4. 100% Intercepted Gutter Flow for Drainage and Road Bioretention Design
The simulated
LT ranged from 1.61 to 7.56 m for the 1000 modeling cases (
Figure 4a). In urban drainage design, the inlet opening lengths for various types of curb inlets standardized by municipalities and transportation agencies have only a few preset/pre-cast/manufactured lengths; for example, Texas Type C and Type D curb inlets [
7] and TxDOT precast curb inlet outside roadway (PCO) on-grade curb inlets [
31] have three opening lengths of 1.52 m (5 ft), 3.05 m (10 ft), and 4.57 m (15 ft). When the calculated curb inlet length for 100% interception is large under design gutter flow, none of the very large opening curb inlets are actually used, but continuously depressed gutter or locally depressed inlets with necessary transient lengths are typically designed and built. Therefore, Equation (8) from the current study, Equation (1) from Izzard (1950), Equation (3) from HEC-22 (2009), and Equation (5) from Muhammad (2018) were rearranged to determine the gutter flow for 100% interception (
Qg100) when the curb inlet length is given.
All the above equations are for the International System of Units (SI) where Lci is in m and Qg100 is m3/s. Determining Qg100 helps us to reevaluate these LT equations. For urban drainage design, design discharge for the gutter was calculated first based on the catchment area, runoff coefficients of land use, and design rainfall intensity; then, the distance between two curb inlets and the curb inlet opening were calculated and selected/specified for the design.
Figure 6 shows the comparison of predicted
Qg100 from Equations (10)–(12) and from Equation (9) for undepressed curb inlets with
Lci = 5 ft (1.524 m). Fourteen
S0 values were used for
Figure 6 and from 0.003 (0.3%) to 0.04 (4%), and two small
S0 (0.001 and 0.002) in
Table 1 were not used (HEC-22 recommends
S0 > 0.3%), and six larger
S0 (0.015, 0.03, 0.025, 0.03, 0.035, and 0.04) were added to represent the steep-slope roads for urban drainage and road bioretention curb inlet design. The 14
S0 and 10
Sx (
Table 1, 1.5–6%) formed 140 slope combinations that were used to compare/evaluate the above
Qg100 equations in
Figure 6. Even the overall
R2 for linear correlations of
Qg100 predicted from three previous studies and the newly developed Equation (9) are greater than 0.80, where
Qg100 predicted by HEC-22 (2009) and Muhammad (2018) is much larger than
Qg100 predicted by Equation (9). Muhammad’s equation has the largest mean absolute percent deviation (MAPD), equal to 180.5%, which always overestimates
Qg100 (
Figure 6), in comparison to
Qg100 from the current study. The MAPD for Izzard (1950) and HEC-22 (2009) are 25.8% and 69.1%, respectively.
Hodges et al. [
31] compared
Qg100 predicted using HEC-22 equation and their experimental measurements. When
Sx was fixed at 6% and
S0 changed from 4% to 0.1%, the
Qg100 predicted using the HEC-22 equation increased about 6 times, but experimental measurements only increased less than 1.6 times. The purple line on
Figure 6b shows the comparison of HEC-22 and Equation (9) predicted
Qg100 results when
Sx = 0.06 (6%). When
S0 decreased from 4% to 0.3% at
Sx = 6%,
Qg100 calculated using HEC-22 increased 6.4 times but
Qg100 from Equation (9) only increased two times, which is similar to results from the physical model by Hodges et al. [
31]. The smaller exponent 0.269 for
S0 in Equation (9) for the current study seems to give a better prediction on
Qg100 compared to HEC-22 Equation (11).
In
Figure 6b, 10 red filled squares gave
Qg100 predicted from HEC-22 for
S0 = 0.3%, and
Sx increased from 1.5% to 6%, and
Qg100 increased from 1.8 L/s to 13.6 L/s that was, on average, 2.83 times larger than
Qg100 (0.62–5.1 L/s) from Equation (9). At
S0 = 0.3%, the ratio of
Qg100 predicted from HEC-22 to Equation (9) ranged from 2.69 to 3.03 with a standard deviation from the mean of 0.11, which graphically shows as a perfect linear relation of these red filled squares on
Figure 6b. This strong linear correlation of
Qg100 predicted from three previous studies versus Equation (9) exists for all other
S0 when
Sx is changed. The ratio of
Qg100 predicted from HEC-22 (2009) versus Equation (9) ranges from 0.85 to 3.03, and has a strong correlation with the longitudinal slope
S0: a power function
Qg100-HEC-22/
Qg100-Equation-9 = 0.213
S0−0.445 (
R2 = 0.99). Actually, the power function can be approximately derived by dividing Equation (11) to Equation (9). The power function clearly indicates that over-prediction occurs in smaller
S0 because of the negative exponent −0.445; for example,
S0 = 0.3%, as shown by the red filled squares. The blue filled squares on
Figure 6 show results for 60 cases with
S0 > 1% and
Sx from 1.5% to 4%. From the power function, when
S0 is larger, the ratio of
Qg100 is smaller, as is also clearly shown in
Figure 6 by the blue filled squares for all three methods.
Figure 6b shows that the predicted
Qg100 from HEC-22 matched very well with the ones predicted from Equation (9) when
S0 > 1%. This means both HEC-22 and the newly developed Equation (9) do a very good job to predict
Qg100 (or
LT using Equation 8) when
S0 > 1%. HEC-22’s Equation (3) for
LT and rearranged Equation (11) for
Qg100 have exponents for slopes
S0 and
Sx that were adjusted from Izzard’s Equation (1) using limited available experiments, but HEC-22 did not document clearly what specific experimental data were used, which could be for experiments
S0 > 1%. The over-prediction of HEC-22 on
Qg100 actually only occurs at lower longitudinal slopes; this could be because the HEC-22 equation was not adjusted with experimental data of small
S0. The ratio of
Qg100 predicted from HEC-22 (2009) versus Equation (9) also seems to correlate with the ratio
Sx/
S0 and becomes larger (over-prediction) when the ratio
Sx/
S0 increases. The power function of the
Qg100 ratio versus the ratio
Sx/
S0 has a determination coefficient of 0.69, which is much weaker than the correlation with
S0 only (
R2 = 0.99).
Hodges et al. [
31] also show that, when the curb length
Lci = 10 ft,
Sx was fixed at 6%, and
S0 changed from 4% to 0.1%,
Qg100 calculated using HEC-22 equation over-predicts by an average factor of 1.51 when compared to measured
Qg100 from their physical model. The ratio of
Qg100 predicted from HEC-22 (2009) versus measurements actually ranges from 0.81 to 3.0, and the ratio of
Qg100 predicted from HEC-22 versus Equation (9) also ranges from 0.85 to 2.37 (
Figure 6), and these two results are very similar. The comparison of predicted 100% intercepted gutter flow with Equations (10)–(12) to Equation (9) for curb length
Lci = 10 ft (3.048 m) and
Lci = 15 ft (4.572 m) also gives similar results discussed above for
Lci = 5 ft (1.524 m) cases, and are therefore not repeated here.
3.5. Simulated Curb Inlet Efficiency and Evaluation Equation
Table 1 shows
Eci determined for 10 example cases (O
mX
mL
m,
m = 1, 2, …, 10), which range from 15.3–75.7%.
Eci was calculated as the curb inlet outflow divided by the upstream inflow (
Figure 1) when the flow through the curb inlet reaches the equilibrium—in other words, the
Eci change is less than 0.0005. For the second set of 1000 modeling cases (O1X1L1 to O10X10L1) of 10 different
Lci values (
Table 1), the mean and standard deviations of simulated
Eci at the same
Lci were calculated. The mean
Eci increased from 12.8% to 84.2%, and the corresponding standard deviation increased from 5.2% to 11.8% when
Lci increased from 0.15 m to 1.50 m. This means inlets in the Philadelphia area (the survey conducted by Stoolmiller et al. [
5]) could intercept different amounts of stormwater runoff to road bioretention facilities, and some of them were under-designed and had flooding risks on the road.
The format of Equation (6) was used to develop a new relationship between
Eci and
Lci/
LT using 1000 simulated
Eci for 10 different
Lci when
Qin was a constant of 10 L/s. Even
Eci has a strong correlation with
Lci (
R2 = 0.86 for a power function), but
Lci/
LT is used in Equation (13) so that it can be applied to other flow rates
Qin from upstream road or watershed, since
LT (Equation (8)) links with and has the impact of the input parameters
S0,
Sx,
Qin, and
n.
The exponent
was determined based on the simulated
Eci results of 1000 cases with the MLR method. The 95% confidence intervals for the exponents
is [2.408, 2.4358] with
p-value < 0.0001.
Figure 7a shows how the comparison of fitted and simulated
Eci; and fitted
Eci matches well with the simulated
Eci with
R2 = 0.98.
Figure 7b shows
Eci versus
Lci/
LT from the current study (fitted Equation 13), Izzard (1950), HEC-22 (2009), and Muhammad (2018). Fitted Equation (13) is almost the same as Izzard’s Equation (2) since
= 2.5, but the HEC-22 equation gives lower
Eci.
Eci predicted from Muhammad’s equation has a different distribution (
Figure 7b): different
Eci for the same
Lci/
LT when
Sx is different, since the exponent
is not a constant but a function of
Sx.
Figure 8 shows the comparison between predicted
Eci from Izzard (1950), HEC-22 (2009), and Muhammad (2018) method and fitted
Eci from newly developed Equations (8) and (13) for 10,000 design cases that are all combinations for 10
S0, 10
Sx, 10
Qin, and 10
Lci listed in
Table 1. The corresponding
LT equation for each method was applied first before
Lci/
LT, and then
Eci were calculated. When applying
Eci equations,
Eci was assumed to be 100% when
Lci is greater than
LT or
Lci/
LT > 1. Among all 10,000 cases, there are 21, 228, and 523 cases with
Lci/
LT > 1 for Izzard, HEC-22, and the Muhammad method when the predicted
LT is smaller than
Lci.
The
R2, RMSE, and MAPD between predicted
Eci for Izzard (1950) method and newly developed equations (Equations (8) and (13)) are 0.96, 4.8%, and 8.8%, respectively. The
R2, RMSE, and MAPD of predicted
Eci between the HEC-22 (2009) method and newly developed equations are 0.96, 5.9%, and 9.4%, respectively. The
R2, RMSE, and MAPD of predicted
Eci between Muhammad’s (2018) method and newly developed equations are 0.92, 8.1%, and 12.9%, respectively. This indicates that for the 10,000 undepressed curb inlet cases from all
S0,
Sx,
Qin, and
Lci combinations, when
LT and
Eci equations for each method are applied together to determine the inlet efficiency, the Izzard (1950), HEC-22 (2009), and Muhammad (2018) methods produced similar results, in comparison to
Eci from newly developed equations for
LT and
Eci. The ratio (
Rci) of predicted and fitted
Eci was computed and summarized to compare these four methods. For the Izzard (1950) method, the ratio
Rci ranged from 0.81 to 1.32 (maximum of 19% underestimate and 32% overestimate in comparison to fitted
Eci), and 2921 cases out of 10,000 cases were within 5% from simulated
Eci (0.95 ≤
Rci ≤ 1.05). For the HEC-22 (2009) method, the ratio
Rci ranged from 0.79 to 1.39 (maximum of 21% underestimate and 39% overestimate), and 3251 cases were within 5% from simulated
Eci (0.95 ≤
Rci ≤ 1.05). For the Muhammad (2018) equation, the ratio
Rci ranged from 0.80 to 1.74 (maximum of 20% underestimate and 74% overestimate), and 2516 cases were within 5% from simulated
Eci (0.95 ≤
Rci ≤ 1.05). There were 3160, 4753, and 8246 cases out of 10,000 cases overestimated
Eci (
Rci > 1.0) for the Izzard (1950), HEC-22 (2009), and Muhammad (2018) methods in comparison to
Eci from Equation (13). The HEC-22 underestimated
LT for most of the cases (
Figure 4) and then made
Lci/
LT larger. There were still 4757 cases overestimating
Eci even though the
Lci/
LT exponent for HEC-22’s
Eci Equation (4) was smaller than the exponent in the proposed Equation (13) and Izzard’s Equation (2).
Figure 8 shows that the Izzard’s method and newly developed equations gave the most similar
Eci predictions, and that the HEC-22 method gave the next most similar predictions on
Eci.