Climate change has caused the inefficient operation of a significant number of old weirs to pass large discharges. Therefore, this study aims to increase the discharge capacity of the labyrinth weir. A new approach was proposed by modifying a labyrinth weir structure. The data was obtained from the quarter-round crest and different sidewall angles ranging from 8 to 35°. A conventional labyrinth weir was used for comparison. The results showed that the percentage of the notches area to sidewalls area of the weir (An/Aw) does not exceed 8%. Also, the percentage of the notches' length to total crest length (ΔL/Lc) does not exceed 32%. Also, the percentage of the notch depth to the sidewall depth (ΔP/P) does not exceed 30%. The other parameters are kept constant. These dimensionless terms provided a maximum compound coefficient of discharge of 0.74. Also, the compound discharge coefficient initially increased at low water head ratios and decreased at higher values of water head ratios. The regression empirical equations were generated. The maximum increase in efficiency was 10% for a sidewall angle of 6° when compared to conventional labyrinth weirs. The maximum improvement of the compound coefficient of discharge was 18.8% for a sidewall angle of 8°.

  • A new approach to the labyrinth weir was proposed and named compound labyrinth weir to improve the discharge capacity of the labyrinth weir.

  • Derivation of hydraulic equation for compound labyrinth weir has been done.

  • Establishing the set of curves showing the relationship between the compound coefficient of discharge Cdc against total head over the entire compound labyrinth weir H′t/P′ with a range of sidewall angles.

  • Empirical equations for compound labyrinth weir and compound linear weir were created.

  • Using the compound labyrinth weir efficiency (έ) as a new tool to provide a guide in choosing a suitable design of the sidewall angle (α).

Graphical Abstract

Graphical Abstract
Graphical Abstract

The following symbols are utilised in the present study:

A

Inside apex width

An

Notch area

Aw

Sidewall area of the weir

b1

Bottom width of the notch

B

Labyrinth weir length in the flow direction

Cdc

Compound coefficient of discharge

D

Outside apex width

έ

Cycle efficiency

g

Acceleration of gravity

h

Flow depth over the weir crest (high stage)

h

Flow depth over the notch (low stage)

Ht

Total head over the weir crest (high stage)

Ht

Total head over the notch (low stage)

Ht′/P

Headwater ratio

Lc

Total centreline length of labyrinth weir

lc

Centreline length of weir side wall

Lc-cycle

Centreline length for a single labyrinth weir cycle

Length of the labyrinth weir crest after subtracting the length of notches (ΔL), ()

l

Length of the notch

N

Number of labyrinth weir cycles

n

Number of notches

P

Weir height

P

Notch height

Q

Discharge over the weir

Rcrest

Radius of crest shape

tw

Thickness of weir wall

V

Average cross-sectional flow velocity upstream of weir

W

Channel width

w

A single labyrinth weir cycle width

ΔL

The top width for the notch

ΔP

The notch depth

α

Sidewall angle

Climate change and associated extreme weather events are resulting in flood events that occur at higher frequency and magnitude (Fowler & Kilsby 2003; Bruwier et al. 2015; Kvočka et al. 2016). Climate change caused a change in the hydrological information that was relied upon in the existing weir design. However, the return period of the flood is often updated. This situation could lead to increased water depth upstream of a weir. When this occurs, it leads to an increased risk of failure in the structure that might be linked to the high level of water over the weir crest, which is more than the allowable value of the design water head. Therefore, it has become impossible to discharge flood waves regularly and safely as a result of climate change. Therefore, old weirs need to be upgraded to labyrinth weirs because labyrinth weirs play an important role in ensuring the security of human life as well as safety in developing areas and the natural environment.

However, labyrinth weirs are overflow structures folded in plan-view and consist of a series of linear weirs installed non-perpendicularly to the sidewall of a channel, resulting in a longer crest length compared with the channel width. For sites where the weir width is restricted but a high discharge is demanded, the labyrinth weirs are an effective and economical choice (Khode et al. 2011), since they can provide a higher discharge capacity for a given water head. Also, labyrinth weirs have become popular as an alternative rehabilitation measure in the upgrading of existing weirs. For example, in areas where rainfall has resulted in peak flows exceeding the capacity of existing weir systems, the labyrinth weir can provide a practical means of rehabilitation (Vasquez et al. 2007). Labyrinth weirs are useful not only for handling larger flow rates but are also used for energy dissipation and self-aeration.

The hydraulic behaviour of labyrinth weirs has received interest from researchers and engineers. Early studies were conducted by Taylor (1968) that provided information on the hydraulic performance and design of the labyrinth weir. Hay & Taylor (1970) developed design criteria based on Taylor's earlier work. Darvas (1971) developed a set of curves to estimate labyrinth spillway performance. Houston (1982) extensively studied a physical model to assess different labyrinth geometries and approach conditions. Lux (1989) mentioned that the aeration condition behind the nappe flow of the labyrinth weir was identified as aerated, transitional, and suppressed. Tullis et al. (1995) investigated labyrinth weir performance and obtained design curves relating the coefficient of discharge, upstream head, and the height of the weir for various sidewall angles from 6 to 18°. Savage et al. (2004) identified errors of up to ±25% in the proposed method by Tullis et al. (1995). Falvey (2003) showed crest flow conditions consist of four conditions of nappe aeration, including pressure, atmospheric, cavity, and sub-atmospheric. Ouamane & Lempérière (2006) studied the rectangular planform of the labyrinth weir and found the rectangular plan shape to be more efficient than the trapezoidal plan shape. Tullis et al. (2007) conducted physical model studies and derived relationships of head–discharge for labyrinth weirs. Ghare et al. (2008) found that discharge capacity was reduced when the crest length of the labyrinth weir was decreased. A sidewall angle has a significant effect on both the discharge capacity and the labyrinth weir layout. Effective length is increased with a smaller angle, which thereby provides a higher discharge capacity.

Also, Crookston & Tullis (2010) included experimental outcomes for 8° sidewall angles. Khode et al. (2011) showed the relationship between coefficients of discharge and H/P for various sidewall angles. They found that the discharge coefficient decreased as the sidewall angle decreased. Paxson et al. (2011) showed that flow conditions downstream of the labyrinth weir could also influence discharge capacity. Khode et al. (2012) developed the relationship between the coefficient of discharge and H/P for a variety of sidewall angles from 8 to 30°. Crookston et al. (2012) developed different models with a sidewall angle α = 15° and used trapezoidal labyrinth weirs. A significant decrease in cycle efficiency with an increase in the Ac/lc ratio occurred. The apex had the lowest impact on total discharge efficiency, as it had a larger impact on the total cycle length and caused a decrease in sidewall length, which thereby caused a reduction in total flow efficiency. Carollo et al. (2012) studied five groups of physical models and adapted the empirical equation suggested by Ghodsian (2009). Dimensional analysis was used to investigate the discharge over the sharp crest of the labyrinth weir. Kumar et al. (2012) investigated discharge capacity using the sharp crest and curving plan shape weir. The coefficients of discharge equations were proposed and the results showed an increase of approximately 40% of the flow capacity over a curved weir compared with a conventional weir. Gupta et al. (2013) studied the characteristics of the discharge under free-flow conditions for a sharp-crested, contracted triangular planform weir. The discharge efficiency across the triangular planform weir was greater than across the normal weir. The equation of flow was suggested for the given range of data and was within ±5% of the observed data.

Moreover, Gupta et al. (2014) investigated W-planform weirs to determine discharge characteristics. The efficiency of the discharge for W-planform labyrinth weirs was greater than that of the normal weir. The equation of flow was suggested for the given range of data and was within ±5% of the observed data. Gupta et al. (2015) used 24 sharp crests to create a labyrinth weir. A rectangular planform weir was utilised to study the impact of the height of the crest on the performance of discharge with different crest lengths. The discharge efficiency of the rectangular labyrinth weir was shown to be higher than that of the conventional weir. Savage et al. (2016) showed the design curves that were found by Crookston & Tullis (2013) are suitable for headwater ratios (Ht/P) > 2.0. Also, Gebhardt et al. (2017) solved navigation requirement problems in the Ilmenau waterway in northern Germany by using a side labyrinth weir. A relationship between the coefficient of discharge and head over various weir heights was obtained. The labyrinth weir is more reliable to operate and safer. Ghaderi et al. (2020a) conducted a numerical and experimental study to investigate the effects of the geometry parameters of trapezoidal–triangular labyrinth weirs (TTLW) on the energy dissipation, discharge coefficient, and downstream flow regime. The results demonstrated that the experimental results agree with the numerical model. Energy dissipation is reduced with an increase in sidewall angle. Daneshfaraz et al. (2020) used the FLOW-3D model to study the effect of channel-bed slope and different channels on the coefficient of discharge of a labyrinth weir. The findings showed that modifying the channel improved the coefficient of discharge. Ghaderi et al. (2020b) used FLOW-3D software to simulate the hydraulic performance of labyrinth weirs. They used the inclining crest edge of the weir and notches in the weir wall. The outcomes showed that modifying the labyrinth weir geometry improved discharge capacity over the labyrinth weir compared with a conventional weir.

Despite the availability of many previous studies about labyrinth weirs’ geometry, evaluation of the performance of the labyrinth weir is still a primary concern and a serious challenge for designers of this type of weir due to major concerns about flood control. This concern has emerged because of climate change and the development of new methods to estimate extreme floods. These methods have demonstrated the insufficiency of a significant number of weirs in handling increasing numbers of extreme flooding events. Consequently, solutions for increasing the capacity of existing weirs and providing more efficient weirs for new projects are being sought. However, due to a lack of knowledge and exemplary ideas, labyrinth weirs need to be investigated further to improve their performance. However, in the present study, a new shape of the labyrinth weir has been proposed. This shape is developed by modifying a labyrinth weir structure (named a compound labyrinth weir). These modifications are made by using trapezoidal notches on the sidewalls of the labyrinth weir. This work provides new knowledge about the new shape of the labyrinth weir. The results of the present study are important to engineers and designers, especially given the current climate change impacts evidenced by possibly higher storm intensities and peak discharges, and where weir rehabilitation is becoming an issue of concern.

Theoretical considerations and hydraulic equation derivation for a compound labyrinth weir

The present study introduces a new approach to the labyrinth weir, which is called the compound labyrinth weir. The flow approach over labyrinth weirs is three-dimensional because of the complex geometry of labyrinth weirs. Thus, it is difficult to accurately describe mathematically (Crookston & Tullis 2012). In addition, the flow function is obtained through experimental investigations and analysis. Therefore, researchers typically use a weir discharge equation. Empirically, compound coefficient of discharge (Cdc) values are determined using experimental results that are obtained from physical modelling. However, the capacity of discharge of a compound labyrinth weir is a function of the coefficient of discharge, total head over the weir, and crest length. A Cdc depends on the labyrinth weir height, wall thickness, total head, crest shape, apex configuration, and sidewall angle of the labyrinth weir. To simplify the analysis, the impact of surface tension and viscosity could be neglected. These parameters are applied to select a satisfactory magnitude of the model and velocity. According to these assumptions, gravitational acceleration is the only significant parameter. Tullis et al. (1995) recommended a new design method for the labyrinth weirs by depending on a basic design equation for the linear weir. Later, it was developed into a labyrinth weir design. The present study found that the Cdc for compound labyrinths is affected by the same variables that affect conventional labyrinth weirs, such as the sidewall angle and the apex of the labyrinth weir. In addition, some variables are related to notched geometry. To calculate the Cdc for the compound labyrinth weir, the flow pattern consists of two scenarios. First, flow only passes over the notches. Second, the flow passes over the entire labyrinth weir. Figure 1 shows a compound labyrinth weir with common geometry and the following equation determines the theoretical discharge (Qtheo.) over the crest of the labyrinth weir and notches:
(1)
Figure 1

Compound labyrinth weir: (a) 3D compound labyrinth weir; (b) Quarter-round crest shape; (c) Plan-view of common geometry; and (d) Longitudinal section of the compound labyrinth weir.

Figure 1

Compound labyrinth weir: (a) 3D compound labyrinth weir; (b) Quarter-round crest shape; (c) Plan-view of common geometry; and (d) Longitudinal section of the compound labyrinth weir.

Close modal
Qwtheo. is the theoretical discharge over the entire labyrinth weir and under the free-flow condition. Theoretical discharge can be expressed as follows:
(2)
Qntheo. is the theoretical discharge only passes over the notches (Henderson 1966) that can be expressed as follows:
(3)
Because there are two crest elevations for a single labyrinth weir, the definition of the head (h) should be for a staged weir. The actual discharge over the notches can be expressed as follows:
(4)
The actual discharge over the labyrinth weir can be expressed as follows:
(5)
(6)
Here, Cdn and Cdw represent the compound coefficient of discharge (Cdc) for the passing flow over all notches and the labyrinth weir. For the compound discharge over the notches and the labyrinth weir, it can be expressed as follows:
(7)
Here, Cdc is the compound coefficient of discharge. The discharge equation for the compound labyrinth weir is obtained by integrating the flow through notches and the labyrinth weir. The discharge equation for a notch is given in Equation (5). The discharge over the compound labyrinth weir with four notches is calculated by adding the flow through the four notches, as shown in Figure 1(d). The Cd values for the trapezoidal notch are calculated separately from Equation (5). Equation (5) can be used to calculate the flow over the notch when the head over the labyrinth weir (h) is less than the head over the notch (h′) when h = 0 and is determined by as shown in Figure 1(d). In this case, the discharge coefficient Cd corresponding to the notch is used. When the head over the labyrinth weir (h) is greater than the head over the notch (h′), the flow over the compound weir is estimated using Equation (7). Where Ht is computed by and is the length of the labyrinth weir after subtracting the notches length (ΔL), (), as shown in Figure 1(d). θ is the side slope angle for the notch (degrees), b1 is the bottom width of the notch, is the crest length of the labyrinth weir, g is the acceleration due to gravity, as shown in Figure 1. Figure 2 shows the hydraulic parameters for flow over the compound labyrinth weir.
Figure 2

Sketch of hydraulic parameters for flow over the compound labyrinth weir: (a) Lower crest and (b) Higher crest.

Figure 2

Sketch of hydraulic parameters for flow over the compound labyrinth weir: (a) Lower crest and (b) Higher crest.

Close modal

Experimental setup

The experiments were carried out in a rectangular flume of length 7 m, width 0.5 m, and height 0.6 m. The flume walls were made from acrylic panels supported by a steel frame. The flume bed was set horizontally. The water was supplied from a storage tank with a volume of 2.5 m3 and recirculated via a 200 mm supply pipe. Two pumps are connected in parallel using a water supply line. The capacity of each pump was 50 L/s giving a total capacity of 100 L/s for both. The flow metre was installed in the main pipeline. The flow metre diameter is 150 mm with an accuracy of 0.5% of the discharge rate. The discharge rates ranged from 10 to 100 L∕s with an accuracy of ± 0.05 to ± 0.5 L/s. A gate valve was utilised in the pipeline to control the flow rate. The flume also contains one regulating gate downstream to control the tailwater elevation. The wave suppressors were provided at upstream of the flume. The wave suppressors were used to control the flow and dissipate the surface disturbances. The water level was measured upstream of the labyrinth weir using a movable pointer gauge with an accuracy of 0.001 m mounted on the flume side rails (allowing longitudinal and transverse movement). As recommended by Dabling (2014), the point gauge was located at a distance of 4 P times the weir height. In the present study, approximately 80 cm was measured from the inlet of the flume to the upstream of the physical models to avoid a water drawdown at the weir edge. Water level measurements varied from 5 to 100 mm for the range of flows tested. For each tested weir geometry, 25 readings of head–discharge were carried out. For each run, the water head over the crest of the labyrinth weir was measured about 2–3 times by a point gauge and the average of the readings was recorded to ensure more accuracy.

In the present study, nine models were used to investigate the optimal notch geometry of the compound labyrinth weir. Table 1 shows the physical model test for the optimal geometry of the trapezoidal notch and Figure 1(a) shows the three-dimensional geometry of the compound labyrinth weir. In addition, eight models are used to study the hydraulic characteristics of compound labyrinth weirs, as shown in Table 2. These models consisted of rang sidewall angles (α) configurations of 6, 8, 10, 12, 15, 20, 35, and 90° (linear weir for comparison). The quarter-round crest experiments were carried out with the curved edge facing upstream, as shown in Figure 1(b). These models were two cycles (N = 2) of compound labyrinth weirs and the total width (W) was 0.5 m. All models were fabricated from acrylic sheets with a thickness (tw) of 10 mm. The acrylic sheets were cut using a laser machine to obtain precise dimensions and then the parts were assembled using screws. Silicon was used to prevent the leakage of water through all the joints of the models. The walls of the model were fixed on the base of the acrylic with a thickness of 6 mm to assist with installing the weir inside the flume. To avoid the curvature effect, all models were located approximately 1.5 m from the inlet point of the flume. An is the notch area that is defined as An= ΔPL+b1)/2. Aw is the sidewall area of the weir that is defined as Aw=lc P.

Table 1

Physical model test for optimal geometry of trapezoidal notch

Labyrinth geometryModel no.Notch geometry
An/AwΔP/PΔL/Lc
b1 (cm)ΔL (cm)ΔP (cm)
α = 15°
P = 20 cm
B = 40.05 cm
lc-one leg = 41.46 cm
Lc = 173.87 cm
W = 50 cm
N = 2
D = 3.5 cm
A = 2 cm
tw = 1 cm 
15.58 17.58 4% 0.1 0.42 
6.29 10.29 4% 0.2 0.24 
2.52 8.529 4% 0.3 0.20 
23.88 25.88 6% 0.1 0.62 
10.44 14.44 6% 0.2 0.34 
5.29 11.29 6% 0.3 0.27 
32.17 34.17 8% 0.1 0.82 
14.58 18.58 8% 0.2 0.44 
8.05 14.05 8% 0.3 0.33 
Labyrinth geometryModel no.Notch geometry
An/AwΔP/PΔL/Lc
b1 (cm)ΔL (cm)ΔP (cm)
α = 15°
P = 20 cm
B = 40.05 cm
lc-one leg = 41.46 cm
Lc = 173.87 cm
W = 50 cm
N = 2
D = 3.5 cm
A = 2 cm
tw = 1 cm 
15.58 17.58 4% 0.1 0.42 
6.29 10.29 4% 0.2 0.24 
2.52 8.529 4% 0.3 0.20 
23.88 25.88 6% 0.1 0.62 
10.44 14.44 6% 0.2 0.34 
5.29 11.29 6% 0.3 0.27 
32.17 34.17 8% 0.1 0.82 
14.58 18.58 8% 0.2 0.44 
8.05 14.05 8% 0.3 0.33 
Table 2

Test programme

α (°)P (cm)B (cm)Lc (cm)A (cm)D (cm)Notch geometry
ΔP/PΔL/lcShape of crest
b1 (cm)ΔL (cm)ΔP (cm)
20 100.8 413.6 3.8 52.8 60.8 0.2 0.6 QR 
20 75.6 313.5 3.7 37.8 45.8 0.2 0.6 QR 
10 20 60.4 253.5 3.6 28.8 36.8 0.2 0.6 QR 
12 20 50.2 213.6 3.6 22.8 30.8 0.2 0.6 QR 
15 20 40.0 173.8 3.5 16.8 24.8 0.2 0.6 QR 
20 20 29.6 134.3 3.4 10.9 18.9 0.2 0.6 QR 
35 20 15.6 84.5 3.0 3.4 11.4 0.2 0.6 QR 
90 20 – 50 – – 22 30 0.2 0.6 QR 
α (°)P (cm)B (cm)Lc (cm)A (cm)D (cm)Notch geometry
ΔP/PΔL/lcShape of crest
b1 (cm)ΔL (cm)ΔP (cm)
20 100.8 413.6 3.8 52.8 60.8 0.2 0.6 QR 
20 75.6 313.5 3.7 37.8 45.8 0.2 0.6 QR 
10 20 60.4 253.5 3.6 28.8 36.8 0.2 0.6 QR 
12 20 50.2 213.6 3.6 22.8 30.8 0.2 0.6 QR 
15 20 40.0 173.8 3.5 16.8 24.8 0.2 0.6 QR 
20 20 29.6 134.3 3.4 10.9 18.9 0.2 0.6 QR 
35 20 15.6 84.5 3.0 3.4 11.4 0.2 0.6 QR 
90 20 – 50 – – 22 30 0.2 0.6 QR 

The current research is based mainly on laboratory experiments to study the effect of the sidewall angle, which contains different notch geometries for each angle. The trapezoidal shape is considered a suitable choice for the notch shape because the trapezoidal shape is best for hydraulic sections. In the present study, to maintain the notches’ shape as a trapezoid, the geometry of the notches was adopted as 0.1 ≤ ΔP/P ≤ 0.3 and 4% ≤ An/Aw ≤ 8%. In other words, if the notches scale is outside this range, it will change to a triangular shape and thus it will be outside the limitations of the present study. Also, the height of the notch from the bottom of the channel to the notch crest should be at least two times the maximum estimated head of water level above the notch crest. This is essential to reducing the velocity of approach (Walkowiak 2006).

Water level data was collected with respect to the weir crest elevation with 0.05 < Ht′/P′ < 0.80 (for the range of flow rate (Q) tested) by measuring the water level over the low stage (h′) and high stage (h) weirs. The measurements were taken only after the flow conditions had reached approximately steady conditions (Crookston 2010), where Q, h, and h′ were measured and recorded. The total heads, Ht and Ht′ were computed by adding the velocity head (V2/2g) to h and h. The velocity of flow was calculated by dividing the actual discharge value, which was measured by a flow metre, by the cross-sectional area of flow based on the width of the weir and flow height. All the measurements were taken at the centre of the width of the flume.

Scale effect

In open channel flow, Froude similarity (i.e., gravitational force) is predominant. In general, researchers have endorsed various scale ratios. Pegram et al. (1999) indicated that prototype behaviour can be represented by a scale ratio of 1:20 or more and showed that the scale ratio of 1:15 was optimal. Furthermore, Boes & Hager (2003) stated that the scale ratio should be from 1:10 to 1:20 if smaller scale models can provide safe design information. In the present study, the scale was set to 1:20 to limit possible scale effects. The purpose of utilising a scaled model is to find values for use at a prototype scale. Chanson et al. (2002) recommended adopting a Reynolds number greater than (105) to avoid scale effects. As shown in the Moody's diagram, the Reynolds number is independent of the friction factor in a wholly rough turbulent flow. In other words, energy dissipation is independent of the Reynolds number in a roughly turbulent flow. Reynolds number was defined by Equation (8). For the present study, the flow adopted a minimum Reynolds number of 102,850 for a sidewall angle of 6° and reached a maximum of 277,778 for a sidewall angle of 15°. Afterwards, the Reynolds number is large enough to avoid scale effects. Because the Reynolds number is greater than 105, the flow conditions are referred to as turbulent flow:
(8)
where V is the velocity of the flow, L is the length of the labyrinth weir in the flow direction, and Ѵ is the kinematic viscosity.
A Weber number is a dimensionless parameter that was defined by Equation (9). It is an indicator of the ratio between the surface tension and the forces of inertia (Falvey 2003). Therefore, the Weber number is used to avoid the impact of surface tension forces, especially in models where the depths are small enough that this effect may be significant. Novak & Cabelka (1981) recommended a minimum Weber number of 11. In the present study, the flow adopted the minimum Weber number of 12 for sidewall angles of 12 and 15°. A maximum Weber number of 3,134 was reached for a sidewall angle of 6°. These results showed that the Weber number varies between 12 and 3,134, allowing surface tension effects to be ignored:
(9)
where σ is the surface tension and ρ is the fluid density. The water temperature was 22 °C during the physical tests.

Determination of the optimal geometry for the notch

In the present study, a new approach has been proposed for the geometry of the labyrinth weir. The new proposal focused on making notches on the sidewalls of the labyrinth weir. The benefit of using notches was to decrease the water level upstream of the weir during peak flood events. In addition, this type of labyrinth weir can provide sufficient flow capacity to deliver greater storm events. The low stage weir is designed to pass moderate-flow events, while the higher stage weir is designed to add sufficient capacity to deliver the more extreme weir design flood. Therefore, it was important to determine the optimal geometry of the notches and the geometry effect on the Cdc under free-flow conditions.

Figure 3 shows the relationship between Cdc and Ht′/P′ for various ΔP/P, various An/Aw and the sidewall angle α = 15° of a compound labyrinth weir. The other dimensions of the notch were constant. ΔP/P represents the percentage notch depth to weir height, while An/Aw represents the percentage notch area to the sidewall area of the weir. All the parameters have been presented in Figure 1.
Figure 3

Variation Cdc versus Ht′/P′ for various ΔP/P, α = 15° and (a) An/Aw = 4%; (b) An/Aw = 6%; and (c) An/Aw = 8%.

Figure 3

Variation Cdc versus Ht′/P′ for various ΔP/P, α = 15° and (a) An/Aw = 4%; (b) An/Aw = 6%; and (c) An/Aw = 8%.

Close modal

According to Figure 3, the impact of notch depth on the Cdc has been observed when the ratio of dropped height increases (ΔP/P from 0.1 to 0.3). Cdc values differed significantly at low Ht′/P′, but Cdc values converged as Ht′/P′ values increased. This difference affects the notch depth in low discharge, but this effect reduces at high discharge. When Ht′/P′ > 0.5, the flow over the compound labyrinth weir becomes submerged; therefore, the effect of notch depth is neglected. When An/Aw = 4% (Figure 3(a)), the Cdc for ΔP/P = 0.3 was about 3 and 7% greater than the Cdc values for ΔP/P = 0.2 and 0.1, respectively. While An/Aw = 6% (Figure 3(b)), the Cdc value for ΔP/P = 0.3 was 4.5 and 8% greater than the Cdc values for ΔP/P = 0.2 and 0.1, respectively. Furthermore, when An/Aw = 8% (Figure 3(c)), the Cdc value for ΔP/P = 0.3 was 5 and 10% higher than the Cdc values for ΔP/P = 0.2 and 0.1, respectively.

Figure 4 shows the relationship between Cdc and Ht′/P′ for various ΔP/P values and various ΔL/Lc values for the sidewall angle α = 15° of a compound labyrinth weir. In Figure 4, the effect of notch length on the Cdc has been investigated. The models for each dropped height (ΔP/P) with different lengths of the notch crest (ΔL/Lc) were tested. These tests investigated the impact of the notch length on the weir's efficiency. The behaviour of the compound labyrinth weir in various ΔL/Lc cases was similar to the behaviour of the compound labyrinth weir for various ΔP/P values.
Figure 4

Variation Cdc versus Ht′/P′ for various ΔL/Lc, α = 15° and (a) ΔP/P = 0.1; (b) ΔP/P = 0.2; and (c) ΔP/P = 0.3.

Figure 4

Variation Cdc versus Ht′/P′ for various ΔL/Lc, α = 15° and (a) ΔP/P = 0.1; (b) ΔP/P = 0.2; and (c) ΔP/P = 0.3.

Close modal

Moreover, Figure 4 shows that the difference in Cdc values was significant at low Ht′/P′ and that the Cdc values converged when Ht′/P′ values increased. This difference is attributed to the effect of notch length in low discharge, but this effect decreases with high discharge. When Ht′/P′ > 0.5, the flow over the labyrinth weir may become submerged and, therefore, the effect of the notch length is neglected. When ΔP/P = 0.1 (Figure 4(a)), the average Cdc for (ΔL/Lc = 0.82, An/Aw = 8%) was 4.5 and 8% higher than the Cdc values for (ΔL/Lc = 0.62, An/Aw = 6%) and (ΔL/Lc = 0.42, An/Aw= 4%), respectively. While ΔP/P = 0.2 (Figure 4(b)), the average Cdc for (ΔL/Lc = 0.45, An/Aw = 8%) was about 5 and 9% greater than the Cdc values for (ΔL/Lc = 0.35, An/Aw = 6%) and (ΔL/Lc = 0.25, An/Aw = 4%), respectively. Also, in case ΔP/P = 0.3 (Figure 4(c)), the average Cdc value for (ΔL/Lc = 0.34, An/Aw = 8%) was about 4 and 11% greater than the Cdc values for (ΔL/Lc = 0.27, An/Aw = 6%) and (ΔL/Lc = 0.21, An/Aw = 4%), respectively.

Using a trapezoidal notch at the sidewall of a labyrinth weir has a good effect on the Cdc when using various An/Aw percentages (4, 6, and 8%) and different values of ΔP/P (0.1, 0.2, and 0.3). From the results, the optimum geometry of the notch to yield the optimum Cdc was noted. For the present study, the An/Aw does not exceed 8%, ΔL/Lc does not exceed 0.32, and ΔP/P does not exceed 0.3 when the other parameters are constant. These parameters have also been given a maximum Cdc of 0.74.

Discharge rating curves

Figure 5 shows the relationship between the Cdc and Ht′/P′ for a quarter-round crest. Different sidewall angles (α) of compound labyrinth weir (6° ≤ α ≤ 35°) were used. For comparison, the linear weir (α = 90°) has been included. In general, the flow over the compound labyrinth weir has two different scenarios: first, the flow passes through notches, as shown in Figure 6(a). Second, flow passes over the entire labyrinth weir, as shown in Figure 6(b).
Figure 5

Cdc versus Ht′/P′ for compound labyrinth weirs. The symbols represent the current experimental study, sold lines indicate curve-fit, and non-continuous lines indicate the data generated by Equations (10) and (11).

Figure 5

Cdc versus Ht′/P′ for compound labyrinth weirs. The symbols represent the current experimental study, sold lines indicate curve-fit, and non-continuous lines indicate the data generated by Equations (10) and (11).

Close modal
Figure 6

Discharge over compound labyrinth weir for a = 12°. (a) Discharge pass over notches only and (b) Discharge pass over entire labyrinth weir.

Figure 6

Discharge over compound labyrinth weir for a = 12°. (a) Discharge pass over notches only and (b) Discharge pass over entire labyrinth weir.

Close modal

Figure 5 shows that Cdc initially behaves similarly for all models when Ht′/P′ are low and the flow only passes through the notch. When Ht′/P′ values are low, the Cdc begins to rise because the nappe flow is still non-aerated with little to no interference nappe, as shown in Figure 6(a). At a low value of H′t/P′, the flow touches the sidewalls of the compound labyrinth wear. This case is analogous to the linear weir because losses at the weir crest still dominate. Also, obviously, nappe interference is absent. When the flow passes over the entire labyrinth weir, Cdc reaches a maximum value because the flow is compound. The discharge over the notches is aerated and the nappe flow becomes more effective. At the same time, the discharge over the entire weir is non-aerated, and nappe flow does not interfere. Figure 5 also shows that Cdc reaches a maximum value before decreasing and tending towards an asymptotic value when the flow is large values of Ht′/P. This is different from linear weirs, where Cdc reaches a maximum and approaches Cdc asymptotically after a slight decrease. When Ht′/P′ is large, increasing Ht′/P′ has a marginal effect on Cdc. When the weir is fully submerged, interference effects between the discharges from the individual weir elements become insignificant. The clinging condition finished at H′t/P′∼0.07 for α = 6, 8, 12, and 20°, whereas it ended at H′t/P′ ∼0.06 for α = 10 and 15°. In comparison to linear weirs, the results showed that the Cdc decreases significantly after its peak. A significant decrease is because labyrinth weirs are subject to the nappe interference of the falling jets (Crookston & Tullis 2011), which is absent in linear weirs. In addition to the sudden removal of the air cavities behind the nappe, nappe interference becomes less significant as α increases; therefore, Cdc increases as α increases for a given upstream head.

As shown in Figure 5, empirical curves are used to simulate experimental data using IBM SPSS 22 software (Allen et al. 2014). Equations (10) and (11) are valid for 0.05 ≤ Ht′/P′ < ∼0.75–0.8, and the coefficients of A, B, C, and D are tabulated in Table 3. After applying Equation (10) for compound labyrinth weir and Equation (11) for compound linear weir, the data display a well-behaved nature when the Cdc (α°) curves have been generalised to Ht′/P′ = 1.0, as shown in Figure 5 with dashed lines. Equations (10) and (11) were selected instead of polynomial formulas because the data have a good correlation representation (R2 ≥ 0.98). In addition, extrapolation performance remains well-behaved up to Ht′/P 2.0. Equations (10) and (11) reflect a good choice for the designer in the case of using compound labyrinth weirs with different sidewall angles:
(10)
(11)
Table 3

Fitting coefficients valid for 0.05 ≤ Ht′/P′ < ∼0.75–0.8

Crest shapeFitting coefficientsSidewall angle (α)
10°12°15°20°35°90°
Quarter-round crest 0.601 0.653 0.697 0.732 0.749 0.765 0.543 2.716 
0.254 0.268 0.28 0.346 0.376 0.466 0.804 0.061 
0.353 0.384 0.446 0.435 0.475 0.544 0.642 1.127 
3.262 2.923 2.886 3.313 3.255 4.916 −4.25 0.632 
R2 0.985 0.986 0.991 0.992 0.982 0.979 0.978 0.987 
Crest shapeFitting coefficientsSidewall angle (α)
10°12°15°20°35°90°
Quarter-round crest 0.601 0.653 0.697 0.732 0.749 0.765 0.543 2.716 
0.254 0.268 0.28 0.346 0.376 0.466 0.804 0.061 
0.353 0.384 0.446 0.435 0.475 0.544 0.642 1.127 
3.262 2.923 2.886 3.313 3.255 4.916 −4.25 0.632 
R2 0.985 0.986 0.991 0.992 0.982 0.979 0.978 0.987 

Labyrinth weir efficiency (ε)

The efficiency of the labyrinth weir represents the flow per unit width of the compound labyrinth weir (at a specific Ht′ value). A compound labyrinth weir is a complex structure; consequently, optimising the design could be difficult. Therefore, the efficiency of the compound labyrinth weir provides guidance for choosing a suitable design. As shown in Figure 5, although the Cdc for labyrinth weirs is less than the Cdc for linear weirs, the increase in weir length for labyrinth weirs results in a higher overall discharge capacity. Cdc varies for a given water depth in labyrinth weirs. As a result, the alternative analysis for the Cdc of labyrinth weirs takes into account the total width of the labyrinth weir by analysing the efficiency, as follows:
(12)
Here, Q is the flow over the compound labyrinth weir and W is the width of the compound labyrinth weir.
The results of ε for the sidewall angles range from 6 to 35° and the quarter-round crest are shown in Figure 7. In general, ε is larger when α is small. According to total capacity, labyrinth weirs with larger sidewall angles are less efficient. For each α, the labyrinth weir efficiency (ε) increases with increasing Ht′/P′. This is because nappe interference and aeration behind the nappe flow decrease when Ht′/P′ increase. For comparison between the efficiency of the compound and conventional labyrinth weirs, the percentage of the improvement in efficiency was 10, 8.9, 7.8, 7.2, 6.6, 5, and 4% for α = 6, 8, 10, 12, 15, 20, and 35°, respectively. The best curve-fit coefficients of Equation (13) and the coefficient of determination (R2) are presented in Table 4. These equations are valid for 0.07 ≤ Ht′/P′ < ∼ 0.85. Equation (13) assists in determining the efficiency of the compound and conventional labyrinth weirs:
(13)
Table 4

Curve-fit coefficients for efficiency of the compound and conventional labyrinth weirs validated for 0.07 ≤ Ht′/P′ < ∼0.85

Compound labyrinth weir
Conventional labyrinth weir
α(°)abR2abR2
0.37 1.41 0.99 0.36 1.49 0.99 
0.33 1.51 0.99 0.32 1.65 0.99 
10 0.30 1.60 0.99 0.30 1.80 0.99 
12 0.27 1.81 0.99 0.26 2.03 0.99 
15 0.25 1.99 0.99 0.24 2.22 0.99 
20 0.24 2.15 0.99 0.24 2.36 0.99 
35 0.23 2.16 0.99 0.233 2.91 0.99 
Compound labyrinth weir
Conventional labyrinth weir
α(°)abR2abR2
0.37 1.41 0.99 0.36 1.49 0.99 
0.33 1.51 0.99 0.32 1.65 0.99 
10 0.30 1.60 0.99 0.30 1.80 0.99 
12 0.27 1.81 0.99 0.26 2.03 0.99 
15 0.25 1.99 0.99 0.24 2.22 0.99 
20 0.24 2.15 0.99 0.24 2.36 0.99 
35 0.23 2.16 0.99 0.233 2.91 0.99 
Figure 7

Efficiency versus Ht′/P′ for compound and conventional labyrinth weirs for 6° ≤ α ≤ 35° and quarter-round crest. The data have been collected from the present study.

Figure 7

Efficiency versus Ht′/P′ for compound and conventional labyrinth weirs for 6° ≤ α ≤ 35° and quarter-round crest. The data have been collected from the present study.

Close modal

Nappe aeration conditions

Nappe aeration is a phenomenon referring to the existence of air cavities behind the nappe flow. In the present study and based on physical observations during the tests, the nappe aeration conditions of compound labyrinth weirs can be classified into four conditions: clinging (Figure 8(a)), aerated (Figure 8(b)), partially aerated (Figure 8(c)), and drowned (Figure 8(d)). Nappe aeration conditions are a function of the velocity head, shape of the crest, weir height, total water head over the weir crest, and tailwater level adjacent to the sidewalls of the compound labyrinth weir. These aeration conditions affect the pressure distribution beneath the nappe and affect the trajectory and momentum of the flow delivered over the weir crest.
Figure 8

Nappe aeration conditions during weir operation for quarter-round crest shape, α = 10°: (a) Clinging nappe observed for Ht′/P′ = 0.05; (b) Aerated nappe observed for Ht′/P′ = 0.25; (c) Partially aerated nappe observed for Ht′/P′ = 0.4; and (d) Drowned nappe observed for Ht′/P′ = 0.55.

Figure 8

Nappe aeration conditions during weir operation for quarter-round crest shape, α = 10°: (a) Clinging nappe observed for Ht′/P′ = 0.05; (b) Aerated nappe observed for Ht′/P′ = 0.25; (c) Partially aerated nappe observed for Ht′/P′ = 0.4; and (d) Drowned nappe observed for Ht′/P′ = 0.55.

Close modal

The results showed that when increasing Ht′ over a compound labyrinth weir, the nappe flow condition changes from clinging aerated to partially aerated to finally drowned. However, all aeration conditions do not certainly take place for all geometries of the compound labyrinth weir. The nappe aeration condition is one of the factors that influence the efficiency of flow over a compound labyrinth weir. Aeration conditions also characterise nappe behaviour. The nappe flow may initially be relatively tranquil and then develop into an unstable condition because of the fluctuating pressure produced on the weir wall. This pressure causes nappe vibrations and noise. In general, the compound labyrinth weir is more efficient when the nappe is clinging (Figure 8(a)) than when it is aerated (Figure 8(b)). This difference is because sub-atmospheric pressures develop on the downstream face of the weir. A partially aerated nappe (Figure 8(c)) occurs at higher Ht′/P′ values. In this case, the air cavities behind the nappe are unstable and vary both temporally and spatially. The air cavities fluctuate between labyrinth weir apexes. Also, the air cavities may be completely removed when the nappe flow condition is submerged. This process reappears as the unsteady flow and turbulent levels behind the nappe fluctuate. The air cavities are highly dynamic and cause oscillating pressures on the downstream face of the weir.

The results showed that nappe trajectories are unstable for the partially aerated nappe condition based on flow conditions and weir geometry. For a stable nappe, the partially aerated condition had less effect on the nappe trajectory. In addition, increasing Ht′/P′ causes the nappe to transition from partially aerated to drowned (Figure 8(d)). The drowned nappe appears as a thick nappe without an air cavity.

The clinging condition finished at Ht′/P′ ∼ 0.07 for α = 6, 8, 12, and 20° and at Ht′/P′ ∼ 0.06 for α = 10°, 15°. The compound labyrinth weir with α = 35° was observed to change directly to an aerated or partially aerated nappe condition. The nappe aeration condition was observed when 0.12 < Ht′/P′ < 0.22 for α = 35°. Depending on α, the largest range of aeration nappe was observed for α = 6–20°. The nappe condition changes from aerated to partially aerated at 0.23 ≤ Ht′/P′ ≤ 0.43 for α = 6°. Depending on α, the largest range of partially aerated nappe was observed for α = 8–35°. The nappe drowned condition was observed when Ht′/P′ > 0.43 for α = 6°. Also, when α increased, the nappe drowned condition increased. The range of Ht′/P′ observed for each nappe aeration condition of compound labyrinth weirs is shown in Table 5. This table will assist the designer to avoid using undesirable ranges of Ht′/P′ in the design process.

Table 5

Nappe aeration conditions for ranges of Ht′/P′ of compound labyrinth weirs with a quarter-round crest

(Ht′/P)
α (°)ClingingAeratedPartially aeratedDrowned
<0.073 0.073–0.23 0.23–0.43 >0.43 
<0.067 0.067–0.31 0.31–0.48 >0.48 
10 <0.064 0.064–0.32 0.32–0.5 >0.5 
12 <0.074 0.074–0.29 0.29–0.54 >0.54 
15 <0.06 0.06–0.28 0.28–0.58 >0.58 
20 <0.07 0.07–0.26 0.26–0.60 >0.60 
35 – 0.12–0.22 0.22–0.62 >0.62 
(Ht′/P)
α (°)ClingingAeratedPartially aeratedDrowned
<0.073 0.073–0.23 0.23–0.43 >0.43 
<0.067 0.067–0.31 0.31–0.48 >0.48 
10 <0.064 0.064–0.32 0.32–0.5 >0.5 
12 <0.074 0.074–0.29 0.29–0.54 >0.54 
15 <0.06 0.06–0.28 0.28–0.58 >0.58 
20 <0.07 0.07–0.26 0.26–0.60 >0.60 
35 – 0.12–0.22 0.22–0.62 >0.62 

Comparison of the compound labyrinth weir and conventional labyrinth weir

As shown in Figure 9, the Cdc of the proposed compound labyrinth weirs is compared with research in the literature on conventional labyrinth weirs. The available data for traditional labyrinth weir were collected by Willmore (2004) and Crookston & Tullis (2013). The comparisons demonstrated a considerable increase in Cdc for the compound labyrinth weir over the data of Willmore (2004) and Crookston & Tullis (2013) for α ranging from 6 to 35°. The results showed that the existing notches on the sidewall of the labyrinth weir have significantly improved the discharge capacity of the labyrinth weir. In Figure 9, comparing the present study with Willmore (2004), the maximum value of the improved percentage was for α = 6°, with an improvement of 20.5% and the minimum value of the improved percentage was for α = 8°, with an improvement of 17.3%. While comparing the present study with Crookston & Tullis (2013) data, the maximum value of the improved percentage was for α = 8°, with an improvement of 18.8%, and the minimum value of the improved percentage was for α = 35°, with an improvement of 15.3%.
Figure 9

Comparison between the present study (compound labyrinth weir), Crookston & Tullis (2013), and Willmore (2004) (traditional labyrinth weir) for quarter-round crest, where (a)–(g) represent sidewall angles of 6, 8, 10, 12, 15, 20, and 35°, respectively.

Figure 9

Comparison between the present study (compound labyrinth weir), Crookston & Tullis (2013), and Willmore (2004) (traditional labyrinth weir) for quarter-round crest, where (a)–(g) represent sidewall angles of 6, 8, 10, 12, 15, 20, and 35°, respectively.

Close modal

The purpose of the present study is to improve the discharge capacity of the labyrinth weir. The labyrinth weir reflects an effective method for increasing storage capacity. The results have shown that dimensionless terms of notches area ratio (An/Aw), notches length ratio (ΔL/Lc), and notches depth ratio (ΔP/P) do not exceed 8, 32, and 3%, respectively, when setting the other parameters as constants. These dimensionless terms have been provided with a maximum Cdc of 0.74. For small values of Ht′/P, Cdc increases with increased Ht′/P′, while Cdc reduces with increased Ht′/P′ and decreases towards a constant value as a function of α when Ht′/P′ is large. This reduction in Cdc is observed in the case of a compound labyrinth weir with a range of sidewall angles (α) (from 6 to 35°) but not in the linear weir. The results also showed that the highest values of the Cdc were with a sidewall angle of 35° and the lowest value of the Cdc was with a sidewall angle of 6° for all examined models. The outcomes demonstrated relationships between Cdc values as a function of Ht′/P. Empirical equations relating to Cdc and Ht′/P′ were created, and the data have a good correlation representation (R2 ≥ 0.98). Empirical equations have been used to predict Cdc values. The set of curves was well-behaved up to Ht′/P′ ≤ 2.0.

Furthermore, the efficiency (ε) is larger when the sidewall angle (α) is small. For each α angle, the efficiency (ε) decreases with increasing Ht′/P. The compound labyrinth weir has higher efficiency when compared with conventional labyrinth weirs, the percentage of the improvement in efficiency was 10, 8.9, 7.8, 7.2, 6.6, 5, and 4% for α = 6, 8, 10, 12, 15, 20, and 35°, respectively. Moreover, the results demonstrated that nappe flow conditions pass through four phases for ranges of Ht′/P. These phases were clinging, aerated, partially aerated, and drowned. In addition, the discharge capacity of the compound labyrinth weir was more efficient with a clinging nappe condition than an aerated, partially aerated, or drowned nappe for all tested models. The maximum value of the improved percentage in the Cdc value, when comparing the present results with a traditional labyrinth weir that was done by Willmore (2004), was as large as 20.5% for α = 6°, while the minimum value of the improved percentage was as large as 17.3% for α = 8°. While comparing the present study with Crookston & Tullis (2013), the maximum value of the improved percentage was as large as 18.8% for α = 8°, and the minimum value of the improved percentage was as large as 15.3% for α = 35°.

Although the methods and information for compound labyrinth weirs have been obtained in the present study, we recommend that a compound labyrinth weir design be verified with numerical and/or physical model studies. This information should be taken into account for site-specific conditions that may be outside the limitations of the present study. Also, the results of the present study will give valuable insights into the operation and performance of the compound labyrinth weir.

The authors would like to express their sincere thanks and gratitude to the government and the Ministry of Higher Education and Scientific Research in Iraq for providing financial support for this study. They also express their sincere thanks to the school of engineering at Deakin University for the use of the new test facility. They appreciate the technical support that is provided by laboratory staff at the School of Engineering (Deakin University).

All relevant data are included in the paper or its Supplementary Information.

The authors declare there is no conflict.

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