Radial gates are common structures in irrigation projects. This paper presents some theory-based equations for explicit estimation of the discharge from a radial gate under free and submerged flow conditions using energy and momentum (E-M) principles. The proposed equations were calibrated using extensive experimental data collected from the literature and this study for three types of radial gate under free and submerged flow conditions. The submergence threshold of radial gates is concluded, based on the concepts of hydraulic jump and the intersection of free and submerged head-discharge curves. The results indicated that the error in estimating the discharge increases under transition ( − 2.5 ≤ Sr% ≤ + 2.5), gate lip (1 < y0/w ≤ 2), and high submerged (yt/y0 ≥ 0.95) flow conditions. However, in these flow limit conditions, the discharge error can be considerably decreased by adjusting the tailwater depth to flow depth just after the gate and using the energy equation for the sections before and after the gate. The efficiency of the proposed methods was evaluated based on the data series from field measurements of radial gates in 29 check structures at irrigation canals in the United States and Iran. The results showed that the discharge could be estimated using the proposed equations in field conditions with acceptable accuracy.

  • Development of an analytical solution for estimating the discharge of radial gates under free and submerged flow conditions.

  • Evaluation of different methods for discharge estimating of radial gates.

  • Evaluation of different methods for identifying the flow condition.

  • Development of some analytical equations for submergence threshold of radial gates based on the concept of the intersection of free and submerged flow curves.

c1, c2, c3, c4

Constant parameters (−)

a

Relative gate opening (a = w/y0) (–)

b

Gate width (m)

Cd

Discharge coefficient (−)

F

Approach Froude number (F = Q/(B.(gy03))) (−)

f

f = Q/(B.√(g.w3))

Ff

Calculated value of approach Froude number from Equation (9) (−)

g

Acceleration due to gravity (m/s2)

k

Calibration coefficient (−)

N

Number of tests (−)

Q

Discharge (m3/s)

R

Gate arm radius (m)

Sr

Submergence ratio (–)

Y

Trunnion-pin height (m)

yc

Critical depth ()(m)

yj

Thickness of the vena contracta (m)

y0

Upstream depth (m)

y2

Flow depth just after the gate (m)

y2L

Flow depth at the immediate section of the gate under transitional flow condition (m)

yt

Tailwater depth (m)

ytL

Maximum downstream depth for which the free flow condition occurs (m)

w

Gate opening (m)

α

Relative flow depth just after the gate (α = y2/y0) (−)

γ

Relative tailwater depth (γ = yt/y0) (−)

γ*

Relative tailwater depth under transitional flow conditions (γ* = ytL/y0) (−)

δ

Contraction coefficient (−)

Θ

Gate lip angle (radians)

Δ

Discriminant in Equation (12) (−)

Δ

Discriminant in Equation (18) (−)

It seems that the key factor in saving irrigation water is to adjust the adequate water supply in proportion to the needs of the product. This is possible by accurately measuring the flow discharge and controlling the water level in irrigation channels. Therefore, measuring water in irrigation canals is essential for precision irrigation management.

Radial gates are common check structures and are frequently used in irrigation networks. Figure 1 shows some typical applications of these structures installed in the Dez irrigation network, Khuzestan province, Iran. They are used to regulate the water level and flow discharge in irrigation canals. Figure 2 depicts the characteristics of flow through a radial gate under free and submerged flow conditions. The discharge (Q) is a function of upstream and downstream geometries such as canal width (B), flow depths both at the upstream (y0) and downstream of the gate (yt), flow condition either free, submerged or transition, and geometric characteristics of the gate, such as gate radius (R), gate width (b), trunnion-pin height (Y) and gate opening (w).

Figure 1

A typical application of radial gates in the Dez irrigation network, Khuzestan province, Iran: (a) parallel gates in the main canal (W1) of the west irrigation network (w1 = 60 cm, w2 = 0), Q = 51 m3/s; (b) parallel radial gates: Gate #1 is under the transition condition, whereas Gate #2 is under the free flow condition.

Figure 1

A typical application of radial gates in the Dez irrigation network, Khuzestan province, Iran: (a) parallel gates in the main canal (W1) of the west irrigation network (w1 = 60 cm, w2 = 0), Q = 51 m3/s; (b) parallel radial gates: Gate #1 is under the transition condition, whereas Gate #2 is under the free flow condition.

Close modal
Figure 2

Definition sketch for outflow from a radial gate: (a) free flow, (b) submerged flow.

Figure 2

Definition sketch for outflow from a radial gate: (a) free flow, (b) submerged flow.

Close modal

An accurate estimate of flow discharge under radial gates is a classic problem in hydraulic engineering. Many studies are available to formulate the discharge of radial gates under free and submerged flow conditions (Buyalski 1983; Clemmens et al. 2003; Wahl 2005, 2011; Shahrokhnia & Javan 2006; Clemmens & Wahl 2012; Zahedani et al. 2012; Bijankhan et al. 2013; Abdelhaleem 2017). The proposed discharge curves by Toch (1955) are applicable to sharp-edged gates with only three relative heights of trunnion pin (Y/R). Clemmens et al. (2003) and Wahl (2005) presented an implicit (iterative) solution for estimating radial gate discharge under submerged flow conditions. In the studies of Toch (1955), Clemmens et al. (2003), Shahrokhnia & Javan (2006) and Zahedani et al. (2012), the type of gate seal was not considered in flow discharge modelling, and for each kind of gate (hard rubber bar, sharp-edged, and music note), a separate equation is proposed. Moreover, the proposed equations by Shahrokhnia & Javan (2006) and Zahedani et al. (2012) have been derived for calculating the submerged flow rate based on the flow depth immediate downstream of the gate (y2), which may be subject to some complexities in measurement. In the studies of Buyalski (1983), Shahrokhnia & Javan (2006), Bijankhan et al. (2013), and Abdelhaleem (2017), the proposed discharge equations are regression-based, which could only be applicable for interpolation in the range of calibration and may result in considerable errors if extrapolation is needed.

A review of the reported works concerning flow measurement using radial gates shows that a general equation (with acceptable accuracy, simplicity in form, including all flow characteristics and gate dimensions) is lacking to determine the flow discharge of radial gates. Moreover, there are limited studies available regarding the distinguishing condition curve of radial gates. Bijankhan et al. (2011) reported three-fold errors in estimating discharge due to a lack of knowledge about the flow conditions. Since most of the previous approaches are based on the momentum equilibrium downstream of the gate and take benefit from the trial-and-error method, Bijankhan et al. (2011) suggested a new approach to identify the flow condition using the intersection of rating curves under free and submerged conditions. However, this implicit approach needs trial-and-error procedures. Also, under the transition zone, the flow depth immediately after the gate was assumed constant (y2L = 1.035 × yj) for all combinations of gate seal type and gate lip angle, requiring more clarifications.

Radial gates may be designed in parallel across the downstream channels (Figure 1(a)). In this situation, some gates may be open, while others are closed (Figure 1(b)). Due to the difference in the gate openings, some gates may be free or submerged while others operate under transition flow conditions. Abdelhaleem (2016) used dimensional analysis to apply the incomplete self-similarity concept to estimate the discharge of submerged parallel radial gates. He introduced some constant parameters in his work, which were calibrated based on the field measurements in three control structures in the Delta irrigation district in Egypt. However, most of the previous methods are experimentally calibrated for an individual radial gate. Consequently, more studies are needed to evaluate the capability of prior discharge estimation methods for parallel radial gates.

In this study, firstly, the energy equation was used between the upstream and immediate contracted section of the gate and combined with the momentum equation between the immediate downstream and the tail section of the gate, with some simplifying assumptions. Then, the empirical values of the constant parameters are presented based on the experimental data. The accuracy of the proposed method was assessed in determining the discharge under free and submerged flow conditions. Under the flow limit conditions, the capability of the proposed method was carefully considered, and a novel solution is presented to decrease the discharge estimation errors. The paper also compares the accuracy of the different methods in estimating the discharge of radial gates and flow conditions. The effects of gate lip angle and gate seal type on the distinguishing condition curve and the discharge of the radial gates have also been evaluated. Finally, the field application of the proposed equations has been considered.

The experimental data by Buyalski (1983) were used to calibrate the proposed equations related to outflow from the radial gates. Buyalski (1983) performed 2,657 experiments on three types of radial gates, namely hard rubber bar, sharp-edged, and music note. In his experiments, the gate width was kept constant at 711 mm, while the downstream channel width was 762 mm. Each gate was installed at three different trunnion-pin heights. The experiments were conducted under three different flow conditions, which he called free, submerged, and jump (assumed to be the transition zone) flow. Table 1 shows the range of Buyalski's (1983) experimental observations. In each case, 80% of the data sets were randomly selected to determine the constant parameters and the remaining 20% were used to validate the proposed equations.

Table 1

Range of non-dimensional parameters within the experiments from Buyalski (1983) and this study

Source of experimentsGate seal typeFlow conditionY/RNumber of testsΘ°Fay0/wyt/w
Buyalski (1983)  Hard rubber bar (Gate 1, 2, 3) Free 0.583, 0.657, 0.728 140 49.01, 53.72, 54.37, 58.26, 62.13, 64.03, 66.85, 69.40, 72.92, 74.79, 76.30, 81.46, 82.56, 83.11, 89.75, 89.83, 90.07 0.05–0.55 1.25–17.83 0.60–1.78 
Jump 38 0.08–0.57 1.17–12.28 0.59–3.08 
Submerged 1,657 0.004–0.50 1.03–18.04 0.96–17.77 
Sharp-edged gate (Gate 7, 8, 9) Free 159 0.05–0.51 1.31–18.19 0.72–1.31 
Jump 18 0.23–0.55 1.22–3.60 0.66–0.86 
Submerged 242 0.02–0.38 1.09–18.11 1.07–14.08 
Music note gate (Gate 4, 5, 6) Free 159 0.05–0.51 1.33–16.31 0.71–1.77 
Jump 0.28–0.53 1.27–2.77 0.66–0.76 
Submerged 237 0.03–0.45 1.09–17.85 1.06–13.53 
This study Sharp-edged gate Free 0.388, 0.728, 0.845 45 35.36, 36.40, 38.25, 40.02, 41.72, 43.0, 44.87, 45.65, 46.42, 47.94, 49.42, 50.87, 68.47, 69.66, 70.84, 72.02, 73.18 0.02–0.38 2.10–47.45 0.74–5.31 
Submerged 847 0.02–0.35 2.00–52.44 1.68–19.89 
Gate lip flow 99 0.08–0.49 1.02–1.99 0.87–1.92 
Transition flow 55 0.03–0.37 1.60–40.55 2.09–10.41 
Source of experimentsGate seal typeFlow conditionY/RNumber of testsΘ°Fay0/wyt/w
Buyalski (1983)  Hard rubber bar (Gate 1, 2, 3) Free 0.583, 0.657, 0.728 140 49.01, 53.72, 54.37, 58.26, 62.13, 64.03, 66.85, 69.40, 72.92, 74.79, 76.30, 81.46, 82.56, 83.11, 89.75, 89.83, 90.07 0.05–0.55 1.25–17.83 0.60–1.78 
Jump 38 0.08–0.57 1.17–12.28 0.59–3.08 
Submerged 1,657 0.004–0.50 1.03–18.04 0.96–17.77 
Sharp-edged gate (Gate 7, 8, 9) Free 159 0.05–0.51 1.31–18.19 0.72–1.31 
Jump 18 0.23–0.55 1.22–3.60 0.66–0.86 
Submerged 242 0.02–0.38 1.09–18.11 1.07–14.08 
Music note gate (Gate 4, 5, 6) Free 159 0.05–0.51 1.33–16.31 0.71–1.77 
Jump 0.28–0.53 1.27–2.77 0.66–0.76 
Submerged 237 0.03–0.45 1.09–17.85 1.06–13.53 
This study Sharp-edged gate Free 0.388, 0.728, 0.845 45 35.36, 36.40, 38.25, 40.02, 41.72, 43.0, 44.87, 45.65, 46.42, 47.94, 49.42, 50.87, 68.47, 69.66, 70.84, 72.02, 73.18 0.02–0.38 2.10–47.45 0.74–5.31 
Submerged 847 0.02–0.35 2.00–52.44 1.68–19.89 
Gate lip flow 99 0.08–0.49 1.02–1.99 0.87–1.92 
Transition flow 55 0.03–0.37 1.60–40.55 2.09–10.41 

aFroude number F = Q/(B.√(gy03)).

Since Buyalski (1983) performed his experiments for limited Y/R ratio values, additional tests have been conducted to extend the range of Buyalski's (1983) data domain. These experiments were performed in a long Plexiglas flume located at the hydraulic laboratory of the Irrigation and Reclamation Engineering Department, University of Tehran. The flume had a width of 0.973 m, and was 1.2 m in height and 18 m in length. All tests were conducted on a sharp-edged gate. The gate arm radius and width were 1.0 m and 0.972 m, respectively. An adjustable Lopac gate was used to regulate the tailwater depth. The upstream water depth (y0) and downstream water depth (yt) were measured using two gauges, with an accuracy of 0.1 mm, at 1.5 m upstream and 9.0 m downstream of the gate seal position, respectively. At this downstream distance, the flow was fully developed. During the experiments, the flow depth just after the gate (y2) was measured. The discharge was measured by an electromagnetic flow-meter, which was installed in the feeding pipe. In total, 1,046 tests were performed on a wide range of flow conditions, gate lip angles, Y/R ratios, approach Froude numbers (F), and relative upstream and downstream depths (y0/w and yt/w).

Table 1 compares the ranges of Buyalski's (1983) data and those of this study. The data from this study covers the upper and lower ranges for the ratio of Y/R (0.388 Y/R 0.845). Some data were collected in the lower range of the gate lip angle (35.36° θ < 49.01°). Figure 3 compares the range of discharge coefficients (Cd = Q/(B.w√(2 g.y0)) determined from Buyalski (1983) and additional experimental data at equal values of θ and Y/R. As noted from the figure, the data of the present study are located in the lower range of f = Q/(B.(g.w3)) and y0/w. Consequently, the data of this study extend the range of Buyalski's (1983) experiments to the sharp-edged gates.

Figure 3

Comparison between the range of experimental data from this study with Buyalski (1983) for the sharp-edged gate (θ ∼ 49°, Y/R = 0.728).

Figure 3

Comparison between the range of experimental data from this study with Buyalski (1983) for the sharp-edged gate (θ ∼ 49°, Y/R = 0.728).

Close modal

Under the orifice flow regime, three hydraulic flow conditions (free, transition, and submerged) can be observed at a gate located in an open channel. However, the discharge error estimation may be increased under three flow conditions, so-called flow limit conditions, as the following (Figure 4): (a) the transition between the orifice and non-orifice flow regimes, which is named the gate lip flow (1 y0/w 2) in which the downstream water depth firstly hits the gate lip, (b) the transition between free and submerged flows ((−2.5% Sr +2.5%), where Sr is the submergence ratio = 100 × (ytytL)/ytL, and ytL is the transitional value of the tailwater depth) in which the downstream water fluctuations due to the hydraulic jump will be transmitted to the gate lip, and (c) high submerged flow (yt/y0 ≥ 0.95).

Figure 4

Classification of flow limit conditions for discharge through the radial gates: (a) gate lip flow (1 y0/w 2), (b) transition between free and submerged flow (−2.5% Sr +2.5%), (c) high submerged flow (yt/y0 0.95).

Figure 4

Classification of flow limit conditions for discharge through the radial gates: (a) gate lip flow (1 y0/w 2), (b) transition between free and submerged flow (−2.5% Sr +2.5%), (c) high submerged flow (yt/y0 0.95).

Close modal

Theoretical equation for discharge estimation of radial gates

Referring to Figure 2, for the submerged flow condition applying the energy equation for sections (1) and (2) would result in:
(1)
where y2 is the flow depth at section (2), and δ is the contraction coefficient as a function of gate lip angle and gate seal characteristics. Moreover, the application of the momentum equation between the immediate downstream and tail sections of the gate would read:
(2)
Introducing non-dimensional parameters of a = w/y0,α = y2/y0,γ = yt/y0, and F = Q/(Bgy03) would simplify Equations (1) and (2) as:
(3)
(4)

Equations (1) and (2) were based on the following assumptions:

  • (1)

    energy conservation between sections 1 and 2;

  • (2)

    momentum conservation between sections 2 and 3;

  • (3)

    presence of rectangular sections both upstream and downstream of the gate;

  • (4)

    equal width for upstream canal and gate;

  • (5)

    hydrostatic pressure distribution at sections 1, 2, and 3;

  • (6)

    uniform flow velocity distribution at the vena contracta section;

  • (7)

    zero roller velocity at the vena contracta section and uniform flow velocity distribution at the downstream section allowing the use of a power-law velocity distribution at this section (Castro-Orgaz et al. 2013); and

  • (8)

    the drag force between sections (2) and (3) is neglected.

Ignoring the effect of simplifying assumptions would cause some disagreements between the experimental observations and those determined by Equations (3) and (4). A calibration factor (k) was introduced in Equation (3) to compensate for these deviations. The value of k would be determined using all experimental data sets. Hence, Equation (3) would be changed as:
(5)
Due to the effects of simplifying assumptions, especially for energy loss, the discharges computed by Equation (5) will be more than the observed values. As a result, it is expected that k < 1. Substituting Equation (5) into Equation (4) can give a solution for α as:
(6)
Taking 0 <α < 1, one can conclude:
(7)
Based on Equations (5) and (6), one gets and hence . Therefore, according to mathematical principles, the positive sign of the square root in Equation (6) has to be taken for 0 <α < 1 and the final discharge equation of a radial gate under the submerged flow condition can be expressed as:
(8)
Under the free flow condition, αδ × α; therefore, the parameter F can be derived from Equation (5) as:
(9)

One fundamental assumption in the development of explicit solutions is an equal width of the gate and the downstream channel. This assumption limits the application of equations for the field cases in which the downstream channel may be wider than the gate. However, it is possible to provide explicit solutions when the gate and downstream channel widths are different.

As before mentioned, generally, the discharge of a radial gate is a function of y0, yt, w, b, R, Y, θ, and gate seal type. It can be seen that the last four parameters are not included in Equation (8). As a result, it is expected that these parameters affected the value of δ. Consequently, the contraction ratio is a function of flow conditions, physical and geometrical characteristics of the gate consisting of the gate seal type, and the ratio of the trunnion-pin height to its radius (i.e., , in which θ = cos−1[(Yw)/R]). By using the experimental data, it is possible to solve Equations (8) and (9) for the contraction coefficient respectively under free and submerged flow conditions. After determining the values of δ, the best regression relation was found as the following:
(10)

In this equation, the angle of θ is in radians. Table 2 shows the empirical values of constants as a function of the gate seal types and flow conditions, which were determined using Buyalski's (1983) data.

Table 2

Values of constant parameters based on the data from Buyalski (1983) 

Gate seal type
Parameterc1c2c3c4k
Free flow condition 
Hard rubber bar 0.029 11.440 844.671 0.643 0.940 
Sharp-edged 0.039 9.395 658.469 0.629 
Music note 0.016 11.116 845.469 0.633 
Submerged flow condition 
Hard rubber bar 0.023 11.707 845.419 0.685 0.940 
Sharp-edged 0.030 9.368 658.458 0.665 
Music note 0.009 10.930 845.485 0.672 
Gate seal type
Parameterc1c2c3c4k
Free flow condition 
Hard rubber bar 0.029 11.440 844.671 0.643 0.940 
Sharp-edged 0.039 9.395 658.469 0.629 
Music note 0.016 11.116 845.469 0.633 
Submerged flow condition 
Hard rubber bar 0.023 11.707 845.419 0.685 0.940 
Sharp-edged 0.030 9.368 658.458 0.665 
Music note 0.009 10.930 845.485 0.672 
Table 3 shows the values of Mean Absolute Relative Error (MARE) for discharge estimation by the proposed method, where Buyalski's (1983) data were used. The following equation was used for computing the MARE:
(11)
where n is the number of data points, and Qexp and Qcal are the experimental and calculated discharges, respectively. Table 3 indicates that under free flow, jump formation, and submerged flow conditions, the MARE values for discharge estimation of the hard rubber bar are 1.4%, 3.3%, 3.2%, respectively, and for the sharp-edged gates are 1.1%, 3.6%, 1.2%, respectively, and for the music note gates are 1.0%, 3.5%, 1.5%, respectively. Based on the experimental data under all flow conditions (free, jump, and submerged), the MARE for the three considered hard rubber bar, sharp-edged, and music note gates are 3.1%, 1.3%, and 1.3%, respectively. The relative error of the hard rubber bar gate increases up to 62% under high submergence flow (γ ≥ 0.9) and low discharge coefficient (Cd 0.26). It was also observed that the errors in discharge estimation do not significantly increase in the validation stage (20% of the data) than in the calibration stage (80% of the data).
Table 3

Evaluation of the proposed method for estimating the discharge based on Buyalski (1983)’s data

Gate seal typeMARE% (Free flow)
MARE% (Jump flow)
MARE% (Submerged flow)
MARE% (All flow conditions)Max RE% (All flow conditions)Percentage of correct flow condition
CalibrationValidationAll dataCalibrationValidationAll dataCalibrationValidationAll data
Hard rubber bar 1.36 1.53 1.41 3.52 2.71 3.35 3.34 3.27 3.21 3.07 62 98.74 
Sharp-edged 1.17 1.09 1.15 3.46 3.70 3.60 1.19 1.58 1.24 1.31 5.91 100 
Music note 1.07 0.98 1.05 3.04 4.66 3.50 1.51 1.29 1.46 1.34 7.52 100 
Gate seal typeMARE% (Free flow)
MARE% (Jump flow)
MARE% (Submerged flow)
MARE% (All flow conditions)Max RE% (All flow conditions)Percentage of correct flow condition
CalibrationValidationAll dataCalibrationValidationAll dataCalibrationValidationAll data
Hard rubber bar 1.36 1.53 1.41 3.52 2.71 3.35 3.34 3.27 3.21 3.07 62 98.74 
Sharp-edged 1.17 1.09 1.15 3.46 3.70 3.60 1.19 1.58 1.24 1.31 5.91 100 
Music note 1.07 0.98 1.05 3.04 4.66 3.50 1.51 1.29 1.46 1.34 7.52 100 

Buyalski's (1983) data were combined with observations of this study to extend the application of the proposed equations for estimating the contraction coefficient of the radial gates, where the values of c1, c2, c3, and c4 have been recalibrated for the sharp-edged gates.

Table 4 shows the values of the parameters as a function of flow conditions using Buyalski's (1983) data and the present study. Table 5 presents the accuracy of the proposed method with new calibrated constant parameters for the δ function under the different flow conditions.

Table 4

Values of constant parameters based on the data from Buyalski (1983) and the present study (sharp-edged gate)

Flow conditionc1c2c3c4k
Free 0.033 9.156 658.464 0.635 0.940 
Submerged 0.035 10.386 658.438 0.670 0.940 
Flow conditionc1c2c3c4k
Free 0.033 9.156 658.464 0.635 0.940 
Submerged 0.035 10.386 658.438 0.670 0.940 
Table 5

Evaluation of the proposed method for estimating the discharge based on the data from Buyalski (1983) and the present study (sharp-edged gate)

Source of dataMARE% (Free flow)MARE% (Jump flow)MARE% (Submerged flow)MARE% (All flow conditions)Max RE% (All flow conditions)Percentage of correct flow condition
Buyalski (1983)  1.18 3.68 1.88 1.70 9.39 100 
Source of dataMARE% (Free flow)MARE% (Gate lip flow)MARE% (Transition flow)aMARE% (Submerged flow)bMax RE% (All flow conditions)Percentage of correct flow conditionc
This study 2.32 8.16 2.19 3.07 35.70 97.03 
Source of dataMARE% (Free flow)MARE% (Jump flow)MARE% (Submerged flow)MARE% (All flow conditions)Max RE% (All flow conditions)Percentage of correct flow condition
Buyalski (1983)  1.18 3.68 1.88 1.70 9.39 100 
Source of dataMARE% (Free flow)MARE% (Gate lip flow)MARE% (Transition flow)aMARE% (Submerged flow)bMax RE% (All flow conditions)Percentage of correct flow conditionc
This study 2.32 8.16 2.19 3.07 35.70 97.03 

a52.7% from all data under transition zone not converged.

bWith large submerged flow data (γ ≥ 0.95).

cThe number of flow data under transition zone (Free ↔ Submerged) = 35.

Based on the data from Buyalski (1983) and the present study, the proposed method for sharp-edged gates showed MARE values of 1.4% and 2.8%, respectively, under free and submerged flow conditions (Table 5). However, the proposed equation with calibrated parameters only based on the data from Buyalski (1983) estimates discharge with MARE values of 1.1% and 1.2%, respectively, for the free and submerged flow conditions (Table 3). Consequently, it is recommended to use the constant parameters in Table 2 for the discharge estimation of sharp-edged gates with more accuracy under the limited range of Buyalski's (1983) data.

Flow limit conditions for discharge estimation of radial gates

Tables 3 and 5 show an increase in the MARE values for the discharge estimation of radial gates under jump flow conditions. Figure 5 presents the variation of MARE in the discharge estimation of radial gates using the proposed method with y0/w and yt/y0. By increasing the ratio of yt/y0, the discharge of the radial gate decreases, and the values of MARE computed by the proposed method considerably increase. As shown in Figure 5(a), the MARE for discharge estimation of the hard rubber bar gate is about 2.5% for the ratio of yt/y0< 0.95 (and Cd > 0.26). However, the MARE increases by approximately 3.5% for 0.95 <yt/y0< 0.99 (mean value of the discharge coefficient is about 0.16). Under high submergence i.e., 0.99 yt/y0< 1.0), the mean value of the discharge coefficient tends to be about 0.07, which results in a significant increase in MARE up to 11.7%. It was also observed that the discharge estimation of radial gates is associated with more error when the upstream depth drops relative to the gate opening (Figure 5(b)). For the range of y0/w > 2, the value of MARE is less than 4.25%. However, for gate lip flow (i.e., 1 <y0/w 2), the MARE increases to 6.3%, which corresponds to the transition zone between the orifice and non-orifice flow conditions.

Figure 5

(a) Variation of MARE with the ratio of yt/y0 based on the data for hard rubber bar; (b) variation of MARE with the ratio of y0/w based on the data for the sharp-edged gate.

Figure 5

(a) Variation of MARE with the ratio of yt/y0 based on the data for hard rubber bar; (b) variation of MARE with the ratio of y0/w based on the data for the sharp-edged gate.

Close modal

Figure 6 compares the measured and calculated discharge of sharp-edged gates from the proposed method under three different flow limit conditions. It can be seen that the amounts of MARE for high submerged flow, transition flow, and gate lip flow are 15.5%, 6.2%, and 30.1%, respectively (Figure 6(a), 6(c) and 6(e)).

Figure 6

Effect of using the measured values of y2 to decrease error in discharge estimation for three flow limit conditions: (a) high submerged flow (before modification), (b) high submerged flow (after modification), (c) transition flow (before modification), (d) transition flow (after modification), (e) gate lip flow (before modification) and (f) gate lip flow (after modification).

Figure 6

Effect of using the measured values of y2 to decrease error in discharge estimation for three flow limit conditions: (a) high submerged flow (before modification), (b) high submerged flow (after modification), (c) transition flow (before modification), (d) transition flow (after modification), (e) gate lip flow (before modification) and (f) gate lip flow (after modification).

Close modal

The value of MARE in discharge estimation at the three above-mentioned zones can be further reduced by using the energy principle between the upstream and downstream of the gate (using Equation (5)) and measured y2 values. This method significantly decreases the MARE amount for discharge estimation of radial gates under high submerged flow, transition flow, and gate lip flow with about 10.6%, 2.2%, and 8.2%, respectively (Figure 6(b), 6(d) and 6(f)). As a result, it is expected that a systematic error in reading the tailwater depth during the experimental observations is of significant importance in increasing the value of MARE for discharge estimation from Equation (8), especially under high submergence. Consequently, it is recommended that a gauge is installed after the gate for direct measurement of y2. Under the high submerged and gate lip flows, the water level after the gate has no turbulence, making possible the direct measurement of y2 (Figure 4(a) and 4(c)). However, there are some difficulties for direct measurement of y2 due to the gate's turbulence under the transition flow condition (Figure 4(b)). As a result, it is recommended to avoid adjusting the gates under the transition zone for field applications to reduce the discharge estimation error.

Effect of gate seal type and gate lip angle on discharge

Figure 7 shows the effects of gate seal type, gate lip angle (θ), and Y/R ratio on the discharge coefficient of radial gates. The discharge coefficient (Cd = Q/(b.w√(2g.y0)) was obtained from Equations (5) and (8) using the functional relationship between F and Cd as Cd = F/(a.√2). Figure 7 shows that the discharge coefficient decreases as θ increases or the ratio of Y/R decreases. This result is in agreement with Salmasi et al.’s (2020) observations, which showed that the gate angle causes the discharge coefficient to increase. The sluice gates are a particular type of radial gates, where R → ∞ and θπ/2. Consequently, under certain conditions, the outflow from a radial gate is more significant than that passing through a sluice gate. It is also notable that the hard rubber bar gate conveys a higher discharge than the sharp-edged and the music note gates. Additionally, the music note gates transport more discharge than the sluice gates.

Figure 7

(a) Effect of gate lip angle on discharge coefficient, (b) effect of gate seal type on discharge coefficient.

Figure 7

(a) Effect of gate lip angle on discharge coefficient, (b) effect of gate seal type on discharge coefficient.

Close modal

Evaluation of different methods for discharge estimating of radial gates

Most of the previous methods have been calibrated based on Buyalski's (1983) data. In this study, the graphical process of Toch (1955), because of multiple interpolations, is avoided. Also, Buyalski's (1983) method was eliminated because of the complex set of equations.

Tables 6 and 7 compare the capability of different methods for discharge estimation of radial gates for free and submerged flow conditions, respectively. The results were obtained based on Buyalski's (1983) experimental data on the three types of radial gates. It should be mentioned that the proposed method of the present study leads to the least error for all flow conditions with the three types of radial gates. Generally, energy–momentum methods (Clemmens et al. 2003; Wahl 2005, and WinGate by Clemmens & Wahl 2012 and the present study) give a more accurate estimation of discharge than those of the regression-based methods (Shahrokhnia & Javan 2006; Zahedani et al. 2012; Bijankhan et al. 2013). Zahedani et al.’s (2012) approach provides the least accuracy in discharge estimation. On the other hand, Wahl's (2005) equation is more accurate than previous methods due to considering the effect of gate seal type.

Table 6

Evaluation of proposed methods for discharge estimation under the free flow condition

Gate seal typeMethodPercentage of ±2.5% errorPercentage of ±5% errorPercentage of ±10% errorMARE%Max ARE%
Hard rubber bar Clemmens et al. (2003)  39.9 68.5 99.4 3.8 10.1 
Wahl (2005)  42.1 95.5 99.4 2.8 10.2 
Shahrokhnia & Javan (2006)  19.7 50.6 70.2 6.9 25.7 
Bijankhan et al. (2013)  37.6 65.2 93.3 4.1 12.7 
Zahedani et al. (2012)  12.9 29.8 59.0 9.6 37.1 
WinGate 62.4 93.3 99.4 2.3 10.6 
This study 78.1 92.7 98.3 1.8 17.5 
Music note gate Clemmens et al. (2003)  35.5 84.3 100 3.2 6.3 
Wahl (2005)  73.5 100 100 1.7 4.8 
Shahrokhnia & Javan (2006)  0.0 0.0 22.9 12.8 20.3 
Bijankhan et al. (2013)  69.9 94.0 100 1.93 6.8 
Zahedani et al. (2012)  15.7 31.3 56.0 12.6 44.9 
WinGate 85.5 95.8 98.8 1.5 13.1 
This study 92.8 100 100 1.2 4.9 
Sharp-edged gate Clemmens et al. (2003)Wahl (2005)  80.2 96.0 97.7 1.8 14.5 
Shahrokhnia & Javan (2006)  0.6 7.34 50.3 10.7 19.8 
Bijankhan et al. (2013)  65.5 91.0 100 2.0 6.5 
Zahedani et al. (2012)  14.1 28.8 57.6 11.7 46.0 
WinGate 92.1 97.7 99.4 1.3 10.1 
This study 89.3 96.6 100 1.4 5.9 
Gate seal typeMethodPercentage of ±2.5% errorPercentage of ±5% errorPercentage of ±10% errorMARE%Max ARE%
Hard rubber bar Clemmens et al. (2003)  39.9 68.5 99.4 3.8 10.1 
Wahl (2005)  42.1 95.5 99.4 2.8 10.2 
Shahrokhnia & Javan (2006)  19.7 50.6 70.2 6.9 25.7 
Bijankhan et al. (2013)  37.6 65.2 93.3 4.1 12.7 
Zahedani et al. (2012)  12.9 29.8 59.0 9.6 37.1 
WinGate 62.4 93.3 99.4 2.3 10.6 
This study 78.1 92.7 98.3 1.8 17.5 
Music note gate Clemmens et al. (2003)  35.5 84.3 100 3.2 6.3 
Wahl (2005)  73.5 100 100 1.7 4.8 
Shahrokhnia & Javan (2006)  0.0 0.0 22.9 12.8 20.3 
Bijankhan et al. (2013)  69.9 94.0 100 1.93 6.8 
Zahedani et al. (2012)  15.7 31.3 56.0 12.6 44.9 
WinGate 85.5 95.8 98.8 1.5 13.1 
This study 92.8 100 100 1.2 4.9 
Sharp-edged gate Clemmens et al. (2003)Wahl (2005)  80.2 96.0 97.7 1.8 14.5 
Shahrokhnia & Javan (2006)  0.6 7.34 50.3 10.7 19.8 
Bijankhan et al. (2013)  65.5 91.0 100 2.0 6.5 
Zahedani et al. (2012)  14.1 28.8 57.6 11.7 46.0 
WinGate 92.1 97.7 99.4 1.3 10.1 
This study 89.3 96.6 100 1.4 5.9 
Table 7

Evaluation of proposed methods for discharge estimation under submerged flow condition

Gate seal typeMethodPercentage of convergencePercentage of ±2.5% errorPercentage of ±5% errorPercentage of ±10% errorMARE%Max ARE%
Hard rubber bar Clemmens et al. (2003)  86.1 9.1 20.5 49.8 12.1 87.2 
Wahl (2005)  95.5 31.2 58.8 81.3 5.9 73.2 
Shahrokhnia & Javan (2006)  100 17.3 35.7 68.6 8.2 49.1 
Bijankhan et al. (2013)  87.2 26.5 45.6 66.8 8.1 91.1 
WinGate 99.9 46.4 74.3 92.1 4.6 84.5 
This study 98.9 66.5 84.4 93.2 3.2 62.0 
Music note gate Clemmens et al. (2003)  95.8 31.6 54.4 71.7 9.4 61.9 
Wahl (2005)  100 49.8 79.3 95.4 3.3 21.9 
Shahrokhnia & Javan (2006)  100 13.5 30.4 56.5 8.7 20.1 
Bijankhan et al. (2013)  86.9 43.9 69.2 83.5 3.3 25.4 
WinGate 100 56.1 87.3 98.3 2.8 18.3 
This study 100 82.3 97.5 100 1.5 7.5 
Sharp-edged gate Clemmens et al. (2003)  94.6 37.3 61.4 73.9 8.1 63.0 
Wahl (2005)  100 55.2 83.4 95.4 3.1 20.9 
Shahrokhnia & Javan (2006)  100 15.3 34.4 64.7 7.6 19.9 
Bijankhan et al. (2013)  87.1 45.2 69.7 83.0 3.4 35.7 
WinGate 100 48.1 77.6 96.3 3.4 21.3 
This study 100 89.2 99.2 100 1.2 5.4 
Gate seal typeMethodPercentage of convergencePercentage of ±2.5% errorPercentage of ±5% errorPercentage of ±10% errorMARE%Max ARE%
Hard rubber bar Clemmens et al. (2003)  86.1 9.1 20.5 49.8 12.1 87.2 
Wahl (2005)  95.5 31.2 58.8 81.3 5.9 73.2 
Shahrokhnia & Javan (2006)  100 17.3 35.7 68.6 8.2 49.1 
Bijankhan et al. (2013)  87.2 26.5 45.6 66.8 8.1 91.1 
WinGate 99.9 46.4 74.3 92.1 4.6 84.5 
This study 98.9 66.5 84.4 93.2 3.2 62.0 
Music note gate Clemmens et al. (2003)  95.8 31.6 54.4 71.7 9.4 61.9 
Wahl (2005)  100 49.8 79.3 95.4 3.3 21.9 
Shahrokhnia & Javan (2006)  100 13.5 30.4 56.5 8.7 20.1 
Bijankhan et al. (2013)  86.9 43.9 69.2 83.5 3.3 25.4 
WinGate 100 56.1 87.3 98.3 2.8 18.3 
This study 100 82.3 97.5 100 1.5 7.5 
Sharp-edged gate Clemmens et al. (2003)  94.6 37.3 61.4 73.9 8.1 63.0 
Wahl (2005)  100 55.2 83.4 95.4 3.1 20.9 
Shahrokhnia & Javan (2006)  100 15.3 34.4 64.7 7.6 19.9 
Bijankhan et al. (2013)  87.1 45.2 69.7 83.0 3.4 35.7 
WinGate 100 48.1 77.6 96.3 3.4 21.3 
This study 100 89.2 99.2 100 1.2 5.4 

Under submerged flow conditions, particularly in the low submergence case, the methods which are based on the energy–momentum equations may not provide a convergent solution. Table 7 shows that the proposed method in this research and WinGate software has the maximum convergence level over those offered by Clemmens et al. (2003) and Wahl (2005).

Among the previous methods, WinGate software provides a more reliable discharge estimation for the three types of radial gates. Accordingly, WinGate software is recommended as a superior tool compared with the other previous methods.

Table 8 shows that the MARE values for WinGate software, as the selected method in the previous section, are 5.6% and 4.6%, respectively, for free and submerged flow conditions. The MARE for WinGate software at high submerged, transition, and gate lip flows increases respectively to about 16.8%, 5.2%, and 13.5%. Consequently, the WinGate software needs to be calibrated for a wide range of Y/R and θ. Hence, the proposed method in this research is recommended for the discharge estimation of sharp-edged gates in a wider range.

Table 8

Evaluation of proposed methods for discharge estimation of sharp-edged gates based on the data from this study

Flow conditionFreeSubmergedLarge submergedTransition between free and submergedGate lipPercentage of convergence
MethodSr% < −2.5%γ < 0.95, y0/w > 2, Sr% > 2.5%γ ≥ 0.95, y0/w > 2, Sr% > 2.5%flow y0/w > 2, −2.5% < Sr% < 2.5%flow y0/w ≤ 2
Clemmens et al. (2003)  3.03 5.52 19.54 6.97 31.59 97.13 
Wahl (2005)  3.03 6.87 20.34 8.31 31.45 100 
WinGate 5.64 4.56 16.84 5.16 13.50 100 
This study 2.32 2.62 15.532 (10.363a6.159 (2.195a) Jump free: 8.29 (3.86a) Jump subm: 2.59 (1.77a30.1 (8.164) 100 
Flow conditionFreeSubmergedLarge submergedTransition between free and submergedGate lipPercentage of convergence
MethodSr% < −2.5%γ < 0.95, y0/w > 2, Sr% > 2.5%γ ≥ 0.95, y0/w > 2, Sr% > 2.5%flow y0/w > 2, −2.5% < Sr% < 2.5%flow y0/w ≤ 2
Clemmens et al. (2003)  3.03 5.52 19.54 6.97 31.59 97.13 
Wahl (2005)  3.03 6.87 20.34 8.31 31.45 100 
WinGate 5.64 4.56 16.84 5.16 13.50 100 
This study 2.32 2.62 15.532 (10.363a6.159 (2.195a) Jump free: 8.29 (3.86a) Jump subm: 2.59 (1.77a30.1 (8.164) 100 

aAfter modifications.

Theoretical equation for distinguishing condition of radial gates

Predicting flow conditions plays an important role that needs clear explanation under free and submerged conditions. When the flow depths in section (2) and an immediate section of the gate (y2) become equal to the flow depth in a contracted section (i.e., y2δw or αδ × α), the flow falls at the submergence threshold. Denoting the relative flow depth at this state as γ* = ytL/y0, and introducing α = δ × a in Equations (3) and (4) and omitting F from these two equations, results in:
(12)
where,
(13)
and,
(14)
Defining the critical flow depth at the downstream section as together with Equations (9) and (14), it can be concluded that r1 = 2γc3 where γc = yc/y0. As a result: . On the other hand, with the subcritical flow at the downstream section (), p1 always is an ascending function of , and its minimum value is , which gives (p1(min) = 3yc3). Taking Δ in Equation (12) as , we would always have Δ< 0. Hence, there will be three roots for Equation (12):
(15)
(16)
(17)
where . Since p1, r1 > 0 and cosϕ< 0, it can be concluded that π/2 <ϕ<π, which gives: , . It is shown that cannot be physically an acceptable solution for relative submergence. On the other hand, and hence is the second solution for supercritical flow, which is not justifiable with the subcritical flow at the downstream section. Thus, would be the correct and only solution to guarantee the flow at the tail section from Equation (15). Therefore, Equation (15), together with the values of k and δ, could be used to determine the submergence threshold and hence the flow condition in the three types of radial gates.

Table 3 shows the percentage of precise flow estimation using Equation (15) and its comparison with the observations of Buyalski (1983). Table 3 demonstrates that Equation (15) correctly predicts the flow conditions for 98.7% of the measurements in the hard rubber bar gates, 100% of the measurements in the sharp-edged gates, and 100% of the measurements in the music note gates. According to the experimental observations in the present study, Equation (15) correctly estimates the flow conditions in most cases (97%) for the sharp-edged gates (Table 5). Therefore, it can be concluded that Equation (15) is efficient in predicting the flow conditions for all three types of radial gates.

Figure 8 shows the distribution of experimental pairs (yt/w, y0/w) relative to the distinguishing curve defined by Equation (15) using the combined data of Buyalski (1983) and the present study. It can be seen that, in most cases, the pairs of (yt/w, y0/w) corresponding to free and submerged flow conditions are located in the lower and upper zone of the distinguishing curve, respectively. Among the experiments on the sharp-edged gates at the present study, several observations are related to the transition zone, which is shown with blue points in Figure 8. These points are located approximately on the distinguishing curve.

Figure 8

Evaluation of proposed methods for identifying the flow conditions based on the data from Buyalski (1983) and the present study. Please refer to the online version of this paper to see this figure in colour: http://dx.doi.org/10.2166/ws.2021.071.

Figure 8

Evaluation of proposed methods for identifying the flow conditions based on the data from Buyalski (1983) and the present study. Please refer to the online version of this paper to see this figure in colour: http://dx.doi.org/10.2166/ws.2021.071.

Close modal

Effects of gate lip angle and gate seal type on the distinguishing curve

Figure 9 shows the effects of θ, Y/R, and gate seal type on the distinguishing curve. It can be seen that the gate with a more significant angle is more likely to become submerged. Hence, under certain conditions of the gate opening and upstream depth, radial gates are less likely to become submerged than sluice gates. Also, the hard rubber bar gate operates under free flow in wider ranges than the sharp-edged and music note gates.

Figure 9

Effects of (a) gate lip angle and (b) gate seal type on the distinguishing curve of radial gates.

Figure 9

Effects of (a) gate lip angle and (b) gate seal type on the distinguishing curve of radial gates.

Close modal

Evaluation of different methods for identifying the flow condition from radial gates

Table 9 compares the capability of different methods to predict the flow condition based on Buyalski's (1983) data and the present study (all data set). Based on Buyalski's (1983) data, the WinGate software provides a more accurate prediction of flow conditions than the other methods. Based on the data from the present study, Equation (15) correctly predicts the flow conditions in 97% of all cases. However, in this series of data, the WinGate software identifies the flow conditions with lower precision than the others. This is due to the limited range of Y/R, and θ was taken from Buyalski's (1983) data to calibrate the WinGate software. It can be seen that the method of Bijankhan et al. (2011) provides an accurate prediction of flow conditions. However, the method of Bijankhan et al. (2011) is implicit and uses a trial-and-error procedure to determine the tailwater depth under the transition zone.

Table 9

Evaluation of different methods for identifying the flow condition from radial gates

Source of experimental dataGate seal typeBijankhan et al. (2011) Bijankhan et al. (2013) WinGateEquation (15)
Buyalski (1983)  Hard rubber bar 94.60 90.30 98.80 98.75 
Music note 97.27 92.31 99.50 100 
Sharp edge 97.37 92.58 97.13 100 
Source of experimental dataFlow conditionBijankhan et al. (2011) Bijankhan et al. (2013) WinGateEquation (15)
This study (Sharp-edged gate) Free flow 100 100 79.07 97.67 
Submerged flow 97.73 92.05 83.75 99.32 
Low submerged flow 56.82 21.59 72.73 73.86 
Total data (1,011 tests)a 94.26 86.25 82.59 97.03 
Source of experimental dataGate seal typeBijankhan et al. (2011) Bijankhan et al. (2013) WinGateEquation (15)
Buyalski (1983)  Hard rubber bar 94.60 90.30 98.80 98.75 
Music note 97.27 92.31 99.50 100 
Sharp edge 97.37 92.58 97.13 100 
Source of experimental dataFlow conditionBijankhan et al. (2011) Bijankhan et al. (2013) WinGateEquation (15)
This study (Sharp-edged gate) Free flow 100 100 79.07 97.67 
Submerged flow 97.73 92.05 83.75 99.32 
Low submerged flow 56.82 21.59 72.73 73.86 
Total data (1,011 tests)a 94.26 86.25 82.59 97.03 

aThe number of flow data under transition zone (Free↔ Submerge) = 35.

Submergence threshold according to the intersection of flow rating curves

Under certain geometric conditions of the canal, radial gate, and specific value of the gate opening, the maximum flow passing through the gate will occur at the intersection point of the free and submerged flow curves, which highlights a new concept to identify the submergence threshold of the radial gate. Therefore, parameter F will be determined when α is minimized (i.e., the term of the square root in Equation (6) equals 0). Thus, the following equation can be concluded to determine the submergence threshold:
(18)
where,
(19)
(20)
(21)
(22)
(23)
The solution of Equation (18) depends on the sign of (Δ′), which can be evaluated as:
(24)
where,
(25)
(26)
Algebraic solutions of Equation (18) are too detailed and complex and cannot be explained herein. However, one can employ Figure 10 as the physical domain of outflow from the radial gate where Δ′ > 0. Therefore, Equation (18) will have four solutions:
(27)
(28)
(29)
(30)
where,
(31)
(32)
(33)
(34)
Figure 10

A graphical representation for obtaining (Δ′) in Equation (18).

Figure 10

A graphical representation for obtaining (Δ′) in Equation (18).

Close modal

Figure 11(b) and 11(d) show that Equations (28) and (30) give the negative answers to identify the limit of the radial gates, which physically cannot be correct ( and < 0). Also, it can be seen from Figure 11(a) and 11(c) that < γc and > γc. Therefore, Equation (27) is the only solution which is valid for the subcritical flow condition at the tailwater section.

Figure 11

Range of four roots of Equation (18) to determine the correct solution: (a) γ*1/ γc, (b) γ*2/ γc, (c) γ*3/ γc and (d) γ*4/ γc.

Figure 11

Range of four roots of Equation (18) to determine the correct solution: (a) γ*1/ γc, (b) γ*2/ γc, (c) γ*3/ γc and (d) γ*4/ γc.

Close modal

Figure 8 compares the distinguishing limits from Equations (15) and (27) on the base of a classical hydraulic jump. As shown in the figure, both limits give similar results. However, the use of Equation (15) is preferable due to its simplified form.

By replacing the relative tailwater depth from Equation (27) in Equation (6), the relative flow depth just after the gate (y2L/(δ.w)) can be estimated for transitional flow conditions. Figure 12 shows a typical variation of y2L/(δ.w) with θ and w/y0 for the hard rubber bar gates. As can be noted, the flow depth just after the gate increases with decreasing the relative gate opening and increasing gate lip angle. This result is an alternative to the finding of Bijankhan et al. (2011), which assumed y2L = 1.5 (δ.w) at a transition zone.

Figure 12

Typical variation of the transitional value of the flow just after the gate with relative gate opening and gate lip angle.

Figure 12

Typical variation of the transitional value of the flow just after the gate with relative gate opening and gate lip angle.

Close modal

Generally, for the transition zone, y2L > (δ.w), as is shown in Figure 12. This result agrees with the assumptions made in concluding the classical hydraulic jump. When the tailwater depth is slightly greater than the threshold tailwater depth determined from Equation (15), the hydraulic jump moves towards the gate, while the gate still operates under the free flow condition with no changes in upstream depth. This continues to intersect the supercritical flow jet with the gate lip, where the flow becomes submerged. Therefore, it is believed that the transition occurs when the tailwater depth is slightly greater than the values revealed in Equation (15).

Field verification test

The proposed methods in this study are specifically developed to estimate the discharge of a radial gate with a width equal to the upstream and downstream channel. For field applications, a set of parallel radial gates may be installed and operated (Figure 1(a)). The opening of the gates may differ from each other, such as in the passage of low discharge. In this case, some gates may be open while others are closed (Figure 1(a)). Also, the difference in the gate opening in parallel applications may cause different flow conditions in each gate as free, submerged, or transition flows (Figure 1(b)). The gates may also be designed at higher or lower levels than the upstream or downstream channels or may be affected by the curvature of the approaching flow lines in a channel intake. These issues can affect the accuracy of the newly proposed methods to calculate the discharge of a radial gate.

The WinGate software has been developed to compute the flow through a complete check structure made up of multiple gates. However, a systematic study covering the field evaluation of WinGate is lacking in the literature. To investigate the effects of parameters as mentioned above on the efficiency of the proposed equations and WinGate software, some available field data from the operation of 12 check structures in the United States' irrigation canals (468 data) and 16 check structures in the Doroodzan irrigation network of Iran (65 data) were utilized. Moreover, a series of 2,240 data was collected related to some measurements since 1977 on the check structure located at the entrance of the main canal in the west of the Dez irrigation network, Khuzestan province, Iran.

Table 10 shows the physical properties of the radial gates used in the field verification. It should be emphasized that the field data were collected from a wide number of parallel gates (N) with different gate openings, seal types, sill levels relative to downstream channel bed, and flow conditions. The simplest method for estimating outflow from parallel gates is based on using the proposed equation by neglecting the effects of interaction between the parallel jets emerging from multiple gates and adjusting the water depths at upstream and downstream channels relative to the sill elevation. Table 10 shows the values of MARE and Percentage of Correct Estimation (PCE) of flow conditions in the data series. As previously discussed, the percentage of errors in discharge estimation increases when the ratio of yt/y0 rises to 0.9 (Figure 5(a)). In the data collection from California Aqueduct check No. 21, the ratio of yt/y0 changes in the range of 0.939 < yt/y0 < 0.98. Also, the discharge coefficient varies in the range of 0.096 < Cd < 0.199. Accordingly, significant errors are expected in the estimation of discharge with this data series, where the value of MARE for this data set was found as 18.3% (see Table 10).

Table 10

Physical properties of the canal radial gates used in the field verification test

CountryCheck structure or irrigation network nameReferenceFlow conditionNumber of gatesDifferent gate openings?Number of testsGate seal typeE.LG − E.LU (m)E.LG − E.LD (m)γ = yt/y0MARE (%) – this studyPCE (%) this studyMARE (%) – WinGate
United States of America Tehama-Colusa Canal check No.1 Buyalski (1983)  Submerged No 38 HR 3.69 0.602–0.816 3.83 100 6.33 
Tehama-Colusa Canal check No.2 Submerged No HRB 1.39 0.615–0.736 23.54 100 18.97 
Tehama-Colusa Canal check No.3 Submerged No HRB − 0.62 − 0.51 0.893–0.938 5.46 100 10.54 
California Aqueduct check No.21 Submerged No 201 HRB − 0.03 0.92 0.939–0.988 18.31 100 23.63 
West Canal headworks before 1974 Submerged No 35 MN 1.24 0.434–0.839 3.07 91.43 3.32 
West Canal headworks after 1975 Submerged No 48 MN&HRB 1.24 0.446–0.927 2.67 97.92 5.68 
Sand Creek check No. 3, Frinat-Kern Canal Submerged No MN 0.609–0.947 3.52 100 3.06 
Yes 11 0.593–0.897 4.25 100 3.49 
Open one gate 0.614–0.619 2.38 100 4.68 
Dodge Avenue check No.4, Frinat-Kern Canal Submerged No 10 MN 0.503–0.758 4.85 100 4.65 
Yes 0.518–0.938 5.55 100 4.91 
Open one gate 0.491–0.540 3.34 100 2.21 
Fifth Avenue check No.7, Frinat-Kern Canal Submerged No MN 0.769–0.817 3.38 100 3.13 
Yes 0.713–0.920 5.34 100 2.64 
Putah South Canal headworks Submerged No MN 1.52 0.78 0.415–0.792 4.75 100 6.04 
Tule River check No.8, Frinat-Kern Canal Submerged No MN 0.2 0.656–0.710 5.95 100 5.77 
Yes 0.743–0.754 5.42 100 2.23 
East Low Canal headworks Free No 37 MN 2.82 0.032–0.526 4.63 100 2.92 
Kaweeh River check No.5, Frinat-Kern Canal Submerged No MN 0.719–0.849 3.87 100 10.77 
Yes 26 0.662–0.869 4.08 100 10.79 
Iran Doroodzan Irrigation Network (in total, the data for 16 check structures were collected) Safarinezhad (1991)  Free 1 or 2 No HRB – 4.25 – WinGate was not run due to lack of information about as-built map in this case 
Yes 7.13 
Open one gate 39 6.73 
Submerged – 10 0.440–0.939 12.49 100 
Dez Irrigation Network, Main West Canal Measurements from 1977 Free No 2,240 Sharp 2.58 – 3.92 – 4.2 
This study No 13 3.73 3.9 
Yes 66 3.26 3.4 
CountryCheck structure or irrigation network nameReferenceFlow conditionNumber of gatesDifferent gate openings?Number of testsGate seal typeE.LG − E.LU (m)E.LG − E.LD (m)γ = yt/y0MARE (%) – this studyPCE (%) this studyMARE (%) – WinGate
United States of America Tehama-Colusa Canal check No.1 Buyalski (1983)  Submerged No 38 HR 3.69 0.602–0.816 3.83 100 6.33 
Tehama-Colusa Canal check No.2 Submerged No HRB 1.39 0.615–0.736 23.54 100 18.97 
Tehama-Colusa Canal check No.3 Submerged No HRB − 0.62 − 0.51 0.893–0.938 5.46 100 10.54 
California Aqueduct check No.21 Submerged No 201 HRB − 0.03 0.92 0.939–0.988 18.31 100 23.63 
West Canal headworks before 1974 Submerged No 35 MN 1.24 0.434–0.839 3.07 91.43 3.32 
West Canal headworks after 1975 Submerged No 48 MN&HRB 1.24 0.446–0.927 2.67 97.92 5.68 
Sand Creek check No. 3, Frinat-Kern Canal Submerged No MN 0.609–0.947 3.52 100 3.06 
Yes 11 0.593–0.897 4.25 100 3.49 
Open one gate 0.614–0.619 2.38 100 4.68 
Dodge Avenue check No.4, Frinat-Kern Canal Submerged No 10 MN 0.503–0.758 4.85 100 4.65 
Yes 0.518–0.938 5.55 100 4.91 
Open one gate 0.491–0.540 3.34 100 2.21 
Fifth Avenue check No.7, Frinat-Kern Canal Submerged No MN 0.769–0.817 3.38 100 3.13 
Yes 0.713–0.920 5.34 100 2.64 
Putah South Canal headworks Submerged No MN 1.52 0.78 0.415–0.792 4.75 100 6.04 
Tule River check No.8, Frinat-Kern Canal Submerged No MN 0.2 0.656–0.710 5.95 100 5.77 
Yes 0.743–0.754 5.42 100 2.23 
East Low Canal headworks Free No 37 MN 2.82 0.032–0.526 4.63 100 2.92 
Kaweeh River check No.5, Frinat-Kern Canal Submerged No MN 0.719–0.849 3.87 100 10.77 
Yes 26 0.662–0.869 4.08 100 10.79 
Iran Doroodzan Irrigation Network (in total, the data for 16 check structures were collected) Safarinezhad (1991)  Free 1 or 2 No HRB – 4.25 – WinGate was not run due to lack of information about as-built map in this case 
Yes 7.13 
Open one gate 39 6.73 
Submerged – 10 0.440–0.939 12.49 100 
Dez Irrigation Network, Main West Canal Measurements from 1977 Free No 2,240 Sharp 2.58 – 3.92 – 4.2 
This study No 13 3.73 3.9 
Yes 66 3.26 3.4 

Note: E.LG, E.LU and E.LD are the elevations of the gate seal, upstream channel bed and downstream channel bed, respectively.

In the proposed approach for deducing Equations (8) and (9), the gate was installed at the same level of upstream and downstream channels' levels. The gate sill causes an additional force on the control volume at the downstream side of the gate. It is noteworthy that overlooking the effects of the gate sill height can result in significant errors in estimating the discharge, such as for Tehama-Colusa Canal check No. 2, in which the gates are designed about 1.4 m above the downstream channel level.

When multiple gates are under operation, adjusting all gates to an equal opening would be more desirable in flow estimation, although it is difficult (Clemmens 2004). The complexity of discharge estimation from multiple gates has been mentioned by some researchers such as Clemmens et al. (2003), Clemmens (2004), Sauida (2014), and Bijankhan & Kouchakzadeh (2015). The complexity is due to the interaction between the jets emerging from the multiple gates, which cause a momentum exchange and additional shear force.

Based on all field data sets, the MARE values in estimating the discharge through the proposed equations are 5.1% (Table 10). The proposed methods in this study also predict the flow conditions at a level of confidence of 99.2%. Also, by ignoring the high submerged data from California Aqueduct check No. 21 and using other field data series from 11 check structures in the United States' irrigation canals, the MARE for discharge estimation using WinGate software is about 5.9%. Hence, the new proposed equations in this study and WinGate's method provide acceptable accuracy. Interestingly, the new suggested method, with its simplifying assumptions, presents an equal accuracy in comparison with WinGate, which has been developed for a complete check structure made up of multiple gates. Consequently, further studies are needed to clarify the effects of the parameters mentioned on the discharge passing under radial gates; particularly, some efforts are required to calibrate multiple gates with different openings.

This paper deals with flow passage through radial gates under free and submerged flow conditions, taking recourse from E-M equations. The theoretical equations have been verified based on the experimental data of Buyalski (1983) and collected data in the present study for the three types of radial gates.

Based on all experimental data, the MARE value to estimate the discharge is 1.4% and 2.8% for free and submerged flow conditions, respectively. The error considerably decreases for flow limit conditions by replacing the tailwater depth with the flow depth just after the gate (y2) and using the energy equation for the sections before and after the gate. Although the direct measurement of y2 depth is possible in the case of gate lip and high submerged flows, there are some difficulties due to the gate's turbulence under the transition between free and submerged flow conditions. As a result, it is recommended that a gauge is installed just after the gate (in the sidewalls) when the field measurement of y2 is required.

The results showed that the proposed method in this study and WinGate software provide an acceptable uncertainty of about ±5% for discharge estimating of radial gates under field applications.

It was observed that the error may increase by ignoring the effects of difference in the gate seat and downstream canal levels and by operating multiple parallel radial gates with different openings. Consequently, further studies are needed to clarify the effects of the parameters mentioned above, particularly when more accuracy is desired.

Data cannot be made publicly available; readers should contact the corresponding author for details.

Some data used during the study are available from the corresponding author by request [experimental new data sets from the present study related to sharp-edged gates]. Other data used during this study appeared in Buyalski (1983).

There is no funding for this article.

The authors declare that they have no conflict of interest.

None.

This research did not receive any specific grant from funding agencies in the public, commercial, or not-for-profit sectors.

This article does not contain any studies with human participants or animals performed by any of the authors.

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