The current research examines the after-effects of climate-induced disasters in India's Himalayan region, as well as the consequences of highway damage. To avoid the damages caused by heavy rain, cloudbursts, and landslides, a design of stepped storm waterway downstream of the underpass rainwater drainage is recommended to overcome such failure in highway design. As a result, an experimental model study was carried out on a stepped channel for a slope of 26.6° with two specific widths. The slope is chosen as it is close to the ideal slope based on the literature. The present research evaluates several characteristics such as the behaviour of flow at different locations (jet length and pool depths), air–water flow properties (air concentration), and energy dissipation efficiency. Different aerated flow depths have been studied to understand their effects on aeration, as well as on energy dissipation. The outcomes showed that the wider channel has a relatively higher energy dissipation efficiency. This outcome could help in modifying the existing storm waterway by widening the channel to facilitate huge runoff during bad climatic conditions. Finally, a multi-nonlinear regression expression is proposed to predict energy dissipation by taking into consideration channel geometry and inflow condition.

  • To mitigate the damage to the hilly road due to heavy rain and landslides, a planned storm waterway design downstream of the underpass rainwater system is suggested.

  • As a result, a thorough study on air–water flow parameters and flow depths (Y90, Y98, and Y99) is conducted under the nappe flow regime.

  • The air–water flow parameters were studied to determine energy dissipation downstream of the stepped channel.

Cmean

cross-sectional mean void fraction

cross-sectional mean void fraction for nth flow depth

dp

water depth in step cavity (m)

Fr

Froude's number at the inlet of the channel

g

gravity acceleration constant (m2/s)

h

step height (m)

hi

equivalent clear water flow depth at different locations (m)

Hcha

height of the channel (m) above the step edge from where measurements are taken (Nh)

Hres(n)

residual energy at nth equivalent clear water depth

Ljet

distance from the start of a step cavity to the midpoint of the impinging jet (m)

L

length of the channel (m)

l

length of the step (m)

N

number of steps

Q

flow rate (m3/s)

qw

specific flow rate (m2/s)

Re

Reynolds number is defined in terms of the hydraulic diameter

Uw

equivalent clear water flow velocity (m/s)

w

channel width (m)

Wr

(q/ho)2(h sin(θ))/ Weber number

X

coordinate perpendicular to horizontal step face at the end of Step-1 (m)

yc

critical flow depth (m)

Y90

bulked water depth where air concentration C = 0.90

Y98

bulked water depth where air concentration C = 0.98

Y99

bulked water depth where air concentration C = 0.99

surface tension (N/m)

θ

slope of the channel

ν

kinematic viscosity (m2/s)

The changing patterns of the atmosphere, ocean systems, and land as well as their relationships with one another at both global and local levels are being changed by the rise in worldwide temperatures (Wang et al. 2004; Soden & Held 2006; Vecchi & Soden 2007; Collins et al. 2010). Additionally, there has been a significant reduction in rainfall frequency (or wet days) during the Indian summer monsoon (ISM) over the past century. The prime differences are reflected as an alteration of the period of rainfall, increased intensity, or reduction in various rainfall factors. The agricultural system across the globe as well as the system of water resources including in India are being negatively impacted by changes in the frequency and intensity of precipitation, which are causing typical phases of disastrous floods in some regions and extreme drought in others (Arnell 1999; Lobell et al. 2011; Schiermeier 2011; Dai 2013; Trenberth et al. 2014; Roxy et al. 2017). As a result, a greater number of studies have been conducted over the last few decades to gain insights into the changing behaviour of the precipitation system over India. Rainfall patterns in India are altering with unusually catastrophic floods affecting areas of the Himalayan region specifically in Uttarakhand and Himachal Pradesh.

Previous research additionally documented the extreme rainfall events triggered disasters in the Himalayan region (Karki et al. 2018; Talchabhadel et al. 2018; Gouda et al. 2022). A study on the extreme flood events that occurred in Himachal Pradesh was thoroughly studied in the research conducted by Gouda et al. (2022). Despite this, there have been few studies that have explored extreme rainfall assessment in Himalayan states, particularly Himachal Pradesh, which has been experiencing various extreme rainfall events including cloud bursting, severe floods, and landslide threats (Bhan et al. 2004, 2015; Dimri et al. 2017). Furthermore, a large number of landslides and three catastrophic flooding incidents occurred in Himachal Pradesh during the current monsoon season, which spanned from 24 June to 15 September 2023. As shown in Figure 1, the districts of Kullu, Mandi, Shimla, Sirmaur, Solan, and Chamba were severely damaged. During those events, the primary challenge was the communication barrier that resulted from highway damage caused by an inadequate storm waterway system. There are numerous ways to lessen the impact of these extreme events as a remedy, including land use and disaster mitigation, more accurate planning for construction of infrastructure, better hydropower projects, and a closer examination of flooding. However, the primary concern highlighted by the present research is first of addressing the inadequate rainwater drainage system in the mountainous regions of the Himalayas, which might cause landslides and damage to highway routes (Figure 1).
Figure 1

(a) Landslides on the highway of Kullu and Mandi in 2023 , (b) Landslides on the highway of Shimla and Kalka in 2017, (c) Landslides in Manali and Leh in 2023 Kullu Mandi highway, article, 2023 Himachal Pradesh: Kullu Mandi highway, article, 2023, https://www.mid-day.com/news/india-news/article/himachal-pradesh-kullu-mandi-highway-closed-following-landslide-amidst-monsoon-deluge-23305705. (b) Shimla-Kalka Highway, article, 2017 Himachal Pradesh: Blocks Shimla-Kalka Highway, article, 2017, https://www.ndtv.com/cities/landslide-blocks-shimla-kalka-national-highway-hundreds-of-vehicles-stranded-1733861. (c) Manali-Leh national highway, article, 2023 Himachal Pradesh Floods: Manali-Leh national highway caves in near Sissu, article, 2023, https://timesofindia.indiatimes.com/city/shimla/hundreds-of-tourists-stranded-in-himachal-pradesh-manali-leh-national-highway-caves-in-near-sissu/articleshow/101636996.cms.

Figure 1

(a) Landslides on the highway of Kullu and Mandi in 2023 , (b) Landslides on the highway of Shimla and Kalka in 2017, (c) Landslides in Manali and Leh in 2023 Kullu Mandi highway, article, 2023 Himachal Pradesh: Kullu Mandi highway, article, 2023, https://www.mid-day.com/news/india-news/article/himachal-pradesh-kullu-mandi-highway-closed-following-landslide-amidst-monsoon-deluge-23305705. (b) Shimla-Kalka Highway, article, 2017 Himachal Pradesh: Blocks Shimla-Kalka Highway, article, 2017, https://www.ndtv.com/cities/landslide-blocks-shimla-kalka-national-highway-hundreds-of-vehicles-stranded-1733861. (c) Manali-Leh national highway, article, 2023 Himachal Pradesh Floods: Manali-Leh national highway caves in near Sissu, article, 2023, https://timesofindia.indiatimes.com/city/shimla/hundreds-of-tourists-stranded-in-himachal-pradesh-manali-leh-national-highway-caves-in-near-sissu/articleshow/101636996.cms.

Close modal

To address this lack in highway design, a stepped storm waterway downstream of the underpass rainwater drainage is suggested as an alternative solution. Its efficiency allows it to dissipate the huge potential energy of heavy rain throughout its entire length, thereby stabilizing the natural slope of the embankment. Stepped waterways have several applications such as sewers, water treatment plants, reoxygenation in canals, emergency spillways over embankment dams, road gutters, and city stormwater structures (Robison 1994; Chanson & Toombes 1997, 2002a; Chinnarasri & Wongwises 2004). Five artificial cascades were built near Chicago along a waterway system in order to help the process of reoxygenation of a dirty canal (Robison 1994). Some of the properties of stepped storm waterway systems, drains, and culverts for different slopes as well as geometries were experimentally tested (Chanson & Toombes 1997, 2002a). Stepped chutes are advantageous for various fields of civil engineering such as mountain drainage systems and emergency spillways over embankment dam downstream faces (Chinnarasri & Wongwises 2004). All these findings from the literature provide a clear image of its applicability in designing an excessive rainwater drainage system for highways in the Himalayan Mountain ranges. This study examines some of the design requirements for stepped channels as well as the hydraulic features associated to gain additional insights into them.

Flows over stepped chutes are identified by their high energy dissipation efficiency and strong air–water interaction between the flows downstream of the inception point (Gonzalez & Chanson 2008; Bung & Valero 2016; Felder & Chanson 2016a; Zhang & Chanson 2018). Many experimental studies were conducted on stepped chutes to understand more about flow behaviour (Figure 2). Most of the studies are conducted on geometric parameters of stepped chutes to obtain a further improved design that can maximize the rate of energy dissipation for an optimum slope. The literature indicates that energy dissipation strongly depends on height and critical depth of flow. Several researches focused on the characteristics of nappe flow condition (Essery & Horner 1978; Peyras et al. 1992; Chanson 1994a, 1994b; Toombes & Chanson 2008a; Felder et al. 2019). A few experiments focused on nappe flow without hydraulic jump to show the three-dimensional flow properties of nappes for a slope of θ = 3.4° (Toombes & Chanson 2008a). Likewise, research conducted by Felder et al. (2019) studied air–water flow properties, energy dissipation, and re-aeration efficiencies of nappe flow for a slope of θ = 15°. A few studies regarding the design of stilling basin below the stepped channel and other rectangular channels were also well described in the literature (Frizell et al. 2016; Achour et al. 2022a, 2022b, 2022c; Milovanovic et al. 2023). This study will assist in further designing a stilling basin for the residual energy downstream.
Figure 2

Different design perspectives of the stepped channel.

Figure 2

Different design perspectives of the stepped channel.

Close modal
In nappe flow, the rate of energy dissipation is larger for fewer steps at identical step height, discharge, and slope. Research by Matos & Quintela (1995b) and Peruginelli & Pagliara (2000) concluded that energy loss in nappe flow reduces with an increase in the number of steps for the same spillway height, discharge, and slope. Nevertheless, nappe flow produces better energy dissipation as compared with skimming flow under non-uniform flow (Andre 2004). Research conducted by Christodoulou (1993) experimentally resolved that a considerable increase in energy dissipation is observed due to an increase in the number of steps for a certain ratio of yc/h. An analysis by Chinnarasri & Wongwises (2006) concluded that with constant step height (h) or constant yc/h, the relative energy dissipation ΔH/Hmax increases with an increase in the number of steps for a certain flow rate. The detailed documentation of nappe flow on the stepped channel is given in Table 1. Likewise, Chamani & Rajaratnam (1994) proposed the following semi-empirical equation to evaluate the rate of energy dissipation:
(1)
where Hmax = Hcha + 1.5yc, ΔH = HmaxHres, Hres is the residual energy, Hcha is the height of the channel (m) above the step edge from where measurements are taken, h is the step height, yc is the critical depth, N is the number of steps, and . Equation (1) is applicable for h/l ranging from 0.421 to 0.842, and yc/h less than 0.8. Further, experiments conducted by Chanson (1994a) proposed the following expression for a fully developed hydraulic jump nappe:
(2)
Table 1

Experimental studies on nappe flow over the stepped channel from the literature

AuthorsSlope of the channel θ (°)Number of stepsUnit discharge
qw (m2/s)
Flow regime and structure typeWidth of the channel w (m)
Pinheiro & Fael (2000)  14, 18.4 10 0.004–0.057 Nappe flow/stepped channels 0.7 
Chanson & Toombes (2002)  3.4 0.04–0.15 Nappe flow/stepped storm waterway 0.5 
Chinnarasri & Wongwises (2004)  30, 45, 60 20 0.01–0.17 Nappe flow, transition flow, skimming flow/stepped chute 0.4 
Toombes & Chanson (2005)  2.6, 3.4 12 0.08–0.15 Nappe flow/stepped waterway 0.25, 0.5 
Takahashi et al. (2007)  19 – 0.0001–0.099 Nappe flow, transition flow, skimming flow 0.4 
Baylar et al. (2007)  14.5–50 – 0.017–0.17 Nappe flow, transition flow, skimming flow/stepped channel chute 0.3 
Toombes & Chanson (2008a)  2.6, 3.4 10 0.038–0.163 Nappe/stepped chute 0.25, 0.5 
Toombes & Chanson (2008b)  – 0.07–0.15 Nappe/backward-facing step 0.25, 0.5 
Renna & Fratino (2010)  14–45 10 0.008–0.42 Nappe/stepped chute 0.6 
Felder et al. (2019)  15 0.005–0.637 Nappe/stepped chute 0.2 
AuthorsSlope of the channel θ (°)Number of stepsUnit discharge
qw (m2/s)
Flow regime and structure typeWidth of the channel w (m)
Pinheiro & Fael (2000)  14, 18.4 10 0.004–0.057 Nappe flow/stepped channels 0.7 
Chanson & Toombes (2002)  3.4 0.04–0.15 Nappe flow/stepped storm waterway 0.5 
Chinnarasri & Wongwises (2004)  30, 45, 60 20 0.01–0.17 Nappe flow, transition flow, skimming flow/stepped chute 0.4 
Toombes & Chanson (2005)  2.6, 3.4 12 0.08–0.15 Nappe flow/stepped waterway 0.25, 0.5 
Takahashi et al. (2007)  19 – 0.0001–0.099 Nappe flow, transition flow, skimming flow 0.4 
Baylar et al. (2007)  14.5–50 – 0.017–0.17 Nappe flow, transition flow, skimming flow/stepped channel chute 0.3 
Toombes & Chanson (2008a)  2.6, 3.4 10 0.038–0.163 Nappe/stepped chute 0.25, 0.5 
Toombes & Chanson (2008b)  – 0.07–0.15 Nappe/backward-facing step 0.25, 0.5 
Renna & Fratino (2010)  14–45 10 0.008–0.42 Nappe/stepped chute 0.6 
Felder et al. (2019)  15 0.005–0.637 Nappe/stepped chute 0.2 
However, aeration is one of the important parameters that directly affect the energy dissipation efficiency of the stepped channel. Flow over stepped channel has three different flow regimes, i.e., nappe flow, transition flow, and skimming flow. Nappe flow appears at a large step height and a low flow rate, where water impinges as a successful free-falling jet on each step. As per Lane (1939), air entrainment occurs when a turbulent boundary layer developing along the boundary emerges to the water surface. Research conducted by Straub & Anderson (1958) made a major contribution towards air concentration distribution in an open channel flow. The air concentration, C, is defined as volume of air per unit volume. Similarly, the depth average mean air concentration, Cmean (Felder et al. 2019), is represented as
(3)
Equation (3) is valid for all the flow regimes of the stepped channel (nappe and skimming). Again, for a given mean air concentration, the advective-diffusion equation of air bubbles in S-shaped skimming flows (Chanson & Toombes 2002b) is given as
(4)
where Do is the function of depth-averaged void fraction, K′ is an integration constant, and Do and K′ are functions of the mean air concentration and these may be estimated as and . Equation (4) is also applicable to nappe flow (Felder et al. 2019) and skimming flow conditions.

Numerous studies have been conducted to trace the correct range of Cmean in different regions. In experimental analysis, Toombes (2002) investigated that for low-gradient spillways the mean air concentrations vary from 40 to 50%. Similarly, observations made by Murillo Muñoz (2006) found Cmean as 35% for a 11° slope, and Takahashi et al. (2007) measured Cmean as 57% for a 19° slope for nappe flow. Detailed observation made by Felder et al. (2019) found Cmean to range from 0.05 to 0.65 at different locations of the spillway. However, Renna & Fratino (2010) took Cmean as 0.5 to calculate equivalent clear water depth. A detailed measurement of Cmean for nappe flow was well described by Toombes & Chanson (2008a), where Cmean for free-falling nappe varies from 0.05 to 0.3, and for spray region, from 0.25 to 0.5. However, the analysis by Toombes & Chanson (2008a) and Felder et al. (2019) took Y90 as the upper limit of the free-surface level to evaluate Cmean. Taking the free-surface level of nappe flow as Y90 will underestimate some of the aeration characteristics as bulking of water is more in the nappe flow compared with the skimming flow.

However, it is observed that many methods of estimating mean air concentration are given in the literature (Toombes & Chanson 2008a; Renna & Fratino 2010; Felder et al. 2019). Therefore, it is necessary to identify the mean air concentration and other properties of the jet with respect to its location at various steps. Since the steps are the key factor of energy dissipation, further designing the steps for better efficiency will help. Equations (1) and (2) are a few fundamental expressions proposed on the stepped channel to predict energy dissipation where yc/h and height of the channel are the most significant parameters to predict energy dissipation. Further studies on multiple parameters are needed to predict energy dissipation for various channel geometries.

As nappe flow is the combination of a series of jets, the first objective of this study is to find out the different jet properties, such as jet length, pool water depth, and mean air concentration, at different locations. Hence, the study determines the behaviour of jets (Ljet, dp) at various locations of a single step as well as at different steps. The second objective is to identify the appropriate free surface of the aerated flow by taking three different bulked water depths such as Y99 (water depth where air concentration C = 0.99), Y98, and Y90. It also includes the effect of different aerated flow depths on air–water flow properties and energy dissipation. Further, to provide more clarity, the air–water flow characteristics at various phases of a jet and various locations are also presented.

As seen from the literature (Table 1), several experiments were conducted in nappe flow by considering different geometries of a channel such as height of the step ( length of the step (l), critical depth of flow (), number of steps (N), width of the channel (w), and maximum height of the channel. Therefore, the third objective of this research is to identify the set of input parameters and their contribution in estimating energy dissipation at various steps and to develop a functional relationship that can predict energy dissipation more precisely.

Experimental plan

Experiments were conducted along a 6 m length, and across two different widths, such as 0.52 m (Model-1) and 0.28 m (Model-2), of the stepped channel for a slope of 26.6° with base as shown in Figure 3(a). The channel consists of 10 identical steps of height 0.1 m and length 0.2 m with a training wall of height 0.5 m. A constant discharge was supplied with the help of a channelized gate of 0.5 m height consisting of a large 2 m deep water tank with a surface area of 3 m × 1.54 m. The sidewall was tapered (1.02 m long) with a 2.96:1 contraction ratio to make the flow waveless. A schematic diagram of the channel set-up is shown in Figure 3(b).
Figure 3

(a) Photo of the stepped channel, (b) schematic diagram of channel set-up, and (c) sketch of measurement location.

Figure 3

(a) Photo of the stepped channel, (b) schematic diagram of channel set-up, and (c) sketch of measurement location.

Close modal

Three different locations are selected in each step for measuring flow properties of the channel as shown in Figure 3(c). Section-1 is selected at the inward side of the jet, Section-2 at the outward side of the jet, and Section-3 at the step edge. The corresponding equivalent clear water depth is denoted as h1, h2, and h3. The ranges of the different variables involved in the experimental program are given in Tables 2 and 3, which include the direct measurements of air–water flow properties and jet properties. According to the literature, stepped channels are used for two distinctive purposes, i.e., aeration and energy dissipation. Similarly, the parametric study of these two criteria is also important. That's why the current study includes all the jet properties and air concentration (C) on the rigid stepped channel. All the experiments are conducted on each step by taking three different sections such as free-falling region (Section-1/inward side of the jet), nappe spray region (Section-2/outward side of a jet), and step edge (Section-3).

Table 2

Details of experimental flow conditions for different configurations

ModelUnit discharge (q) m2/syc/hWidth of channel (m)Slope
Model-1, 2 8.9 × 10−3
65.7 × 10−3 
0.201–0.761 0.52, 0.28 26.670° 
ModelUnit discharge (q) m2/syc/hWidth of channel (m)Slope
Model-1, 2 8.9 × 10−3
65.7 × 10−3 
0.201–0.761 0.52, 0.28 26.670° 
Table 3

Experimental parameters in different flow conditions

yc/hUnit discharge (q)
m2/s
Froude number
(Fr)
Reynolds number
(Re)
Weber number
(Wr)
0.201 8.9 × 10−3 0.706 0.80 × 104 42.25 
0.761 65.7 × 10−3 0.965 5.08 × 104 770 
yc/hUnit discharge (q)
m2/s
Froude number
(Fr)
Reynolds number
(Re)
Weber number
(Wr)
0.201 8.9 × 10−3 0.706 0.80 × 104 42.25 
0.761 65.7 × 10−3 0.965 5.08 × 104 770 

A pump with a frequency regulator AC motor carried the flow rate, allowing an accurate flow change in a closed-circuit system. The channel centreline was selected to measure clear water flow depths with the help of a point gauge. Discharge measurements were taken with the help of an ultrasonic flowmeter at the entrance of the pipe. To take the uncertainty of time and space of the observed data into consideration, multiple samples were taken and the average error was less than ±0.5% for all the flow rates. An open downstream reservoir was used to channelize the water back to the upstream tank. Pressure and velocity measurements were taken with a Pitot tube (Ø = 3.0 mm) upstream. A finely adjustable travelling mechanism was introduced to control the horizontal movement of the Pitot tube. Detailed photographs of the nappe flow for the two different widths of the channel are shown in Figure 4(a) and 4(b). Likewise, Figure 4(c) and 4(d) shows the side view of Model-1 as well as the skimming flow pattern of Model-2.
Figure 4

Photo of the stepped channel. (a) Model-1 for yc/h = 0.255, (b) model set-up of Model-2 for yc/h = 0.201, (c) side view of Model-1, and (d) side view of Model-2 (skimming flow).

Figure 4

Photo of the stepped channel. (a) Model-1 for yc/h = 0.255, (b) model set-up of Model-2 for yc/h = 0.201, (c) side view of Model-1, and (d) side view of Model-2 (skimming flow).

Close modal
Inclusive quantities of the hydro-air flow across the steps were measured by using a CCS hydro-air phase meter (Figure 5(a)) having a single conductivity probe of 0.3 mm diameter of the inner electrode. The datasets of air concentration (C) were acquired with a data acquisition system. Based on the number of observations, a sampling duration of 60 s and a sampling rate of 100 Hz (sampling duration of 45 s recommended by Felder et al. (2019) per sensor) were taken as optimal for the accurate measurement of the air concentration shown in Figure 5(b) (signal output).
Figure 5

(a) Model set-up with CCS hydro-air phase meter and (b) low pass-filtered void fraction data by using CCS hydro-air phase meter 100 Hz, scan duration: 60 s, C = 0.79, F = 100 Hz.

Figure 5

(a) Model set-up with CCS hydro-air phase meter and (b) low pass-filtered void fraction data by using CCS hydro-air phase meter 100 Hz, scan duration: 60 s, C = 0.79, F = 100 Hz.

Close modal

The probe was vertically supported by a trolley to measure flow depth normal to the flow direction. An error of less than 0.028 mm is measured in the vertical position of the probe. An interval of 0.5 cm is taken as the longitudinal movement of the probe. Similarly, in the crosswise direction, the interval of the probe is taken as 0.15 cm. A maximum error of 4.65% is measured for all values of void fraction varying from a minimum air concentration of 0.06 to a maximum of 0.99, for a flow range of unit discharges 0.008925 < qw < 0.0657 m2/s (0.201 < yc/h < 0.761), with Reynold number Re varying from 0.80 × 104 to 5.088 × 104 and Weber number Wr ranging from 42 to 770. Visual observation of the propagation of jet impact on the horizontal steps provides clarity on the nappe flow pattern. The nappe flow appeared to be very regular along the flow and agreed well with a common description that the flow pattern may be observed as a succession of the free-falling jet.

Method

As the experiment was conducted on a fully aerated flow, the measurement of bulked water depth, as well as air–water flow properties are essential to study the flow behaviour. Among the three flow regimes of the stepped flow, the nappe flow regime is considered for further study. To identify the behaviour of the nappe at each particular step, the jet length (Ljet) and pool water depth (dp) were studied at different flow conditions. Air–water flow measurements were conducted at three different locations of each step to identify the behaviour of the jet as shown in Figure 3(c).

Likewise, the air–water flow properties at each step were conducted. One of the major studies was undertaken to find out the upper limit of the free surface as the flow is highly aerated. To identify that, three different bulked water depths are thoroughly studied such as Y90, Y98, and Y99. Because the flow has different behaviours at different flow depths, the effect of the relative increase or decrease in bulked water depth at different flow depth conditions (Y90, Y98, and Y99) was studied. Likewise, its effect on mean air concentration (Cmean) was also verified at these flow depths.

Similarly, the effects of the relative increase or decrease in and at different flow depth conditions (Y90, Y98, and Y99) were also studied. Further, the rates of energy dissipation were calculated at each of the three locations (Section-1, Section-2, and Section-3) to identify the point of maximum energy dissipation. The flow diagram of the research methodology is shown in Figure 6.
Figure 6

Flowchart of the methodology.

Figure 6

Flowchart of the methodology.

Close modal

A few parametric studies have been carried out in order to get further insights into the jet flow over the stepped channels. The investigation was initially carried out by measuring the pool water depth and the jet length at various steps. It helps in understanding the jet's movement and fluctuations at various locations. It will most likely assist in designing various step geometries and their spacings. Furthermore, there have not been many studies on determining the aerated flow's free-surface level and how it affects energy dissipation. Therefore, a study on the effect of flow depth variations on aeration as well as energy dissipation will help in optimizing the design stepped channels. The results also identify the effect of channel width on energy dissipation and aeration.

Identification of steady jet region

Here in this study, the variation of jet length at each step was found. For that, two main parameters, jet length Ljet and pool depth dp, were measured in each step at different flow rates.

The jet is highly stable and no aeration is observed throughout the flow for the first step, as shown in Figure 4(a). A small amount of air entrainment is observed at the impingement point, where the depth of flow is much lower to measure flow properties. Aeration started from the edge of the second step and full aeration was achieved at the free-falling region of the third step. The present study shows the variations of jet length (Ljet, the distance from the step corner to the centre of the impinging jet), jet impact point, and pool water depth (dp) for each step at different flow rates.

A minimum value of Ljet was observed at the first step and the flow curvature was ogee-shaped. There was no similarity in the shape of the falling jet between the first step and the other adjacent steps. That is why during the prediction of flow properties, the first step is not taken into consideration. Figure 4(a) and 4(b) clearly displays the difference in flow patterns from Step 3 to Step 6 and agrees with the statement given by Toombes & Chanson (2008a) that some deviation has been observed in Steps 3 and 5. However, regular flow patterns are observed from Step 7 onwards. Observations were made on each location where the jet strikes on the horizontal face of each step. It is found that with an increase in discharge, the deflection of the jet increases, and at a certain points it crosses the step and jumps over the subsequent step. The flow regime at that point is called transition flow.

The present study represents a non-dimensional parameter with variation in the number of steps, as shown in Figure 7(a). It is found that at each , Step 5 has the maximum jet length compared with the others. Consequently, the jet stablizes from Step 7 onwards. The study of the non-dimensional parameters (Figure 7(a)) and (Figure 7(b)) is undertaken to see the pattern of the jet at each step with different flow rates for the 0.52 m width channel. Experimental analysis on with respect to the number of steps for = 0.201 to 0.466 displays a minimum pool depth at Step 5. It may be due to the maximum deflection of the jet occurring at that step. Again, maximum pool depth is observed at Step 4. Pool depth fluctuations become stable from Step 7 onwards.
Figure 7

Dimensionless parameters of jet properties: (a) jet length with respect to the step number and (b) jet pool depth with respect to the step number.

Figure 7

Dimensionless parameters of jet properties: (a) jet length with respect to the step number and (b) jet pool depth with respect to the step number.

Close modal

The above analysis confirmed that the flow becomes stable at X/L ≥ 0.6, where X is the horizontal distance from Step 1, and L is the length of the channel. Based on the present observation, it is clear that after crossing the horizontal face of Step 7 (60–70% of the total length of the channel) for all discharges, the flow seems to be uniform, whereas Felder et al. (2019) observed a uniform flow at the edge of Step 4 out of 6 (66.67% of the total length of the channel) the number of steps for a slope of 15° and a width of 0.2 m. This may be due to variations in the slope and width as well. It is also observed that air entrainment starts from the edge of Step 3 for almost all flow rates. Accordingly, Steps 1 and 2 come under the non-aerated zone, while the partially aerated flow region starts from the Step 2 edge to Step 3. Similarly, a fully aerated zone has been achieved from the Step 3 edge to Step 7.

The aeration increases with the flow rate, which leads to the enlargement of the jets at each successive step. To further develop different designs for the steps (non-uniform steps or any modification to the step's shape), it is necessary to understand the variations in both jet length and pool depth in a uniform step. By studying jet behaviour, it was also determined that each jet must stick to the horizontal face of the step to dissipate kinetic energy.

Identification of free-surface level

The study on the free-surface level of nappe flow is essential to estimate mean air concentration (Cmean). Therefore, one of the most important parts of this study is identifying the free-surface level as the bulking of flow depth is high for nappe flow. In this regard, few trials have been made by taking three free-surface levels (Y90, Y98, and Y99) to estimate Cmean. As described in the literature, the calculation of Cmean is based on an accurate measurement of bulked water depth. In some cases, the upper limit of the bulked water depth was taken as Y90 (Toombes & Chanson 2008a; Felder et al. 2019). In some cases, Cmean is considered as 0.5 (Renna & Fratino 2010). Therefore, to identify the variation of bulked water depth on the estimation of Cmean, three depths were selected.

To examine the amount of variation in water depth among Y90 and other depths, two different water depths (Y98 and Y99) were selected for experimental analysis in three specific locations (free-falling region, nappe spray region, and step-edge region). Y98 refers to the flow depth measured with respect to the channel bottom up to 98% of flow depth. In the free-falling jet section, the variation of bulked water depth in Y99 to Y90, Y98 to Y90, and Y99 to Y98 is followed as 20.68 to 37.31%, 8 to 32.25%, and 6.4 to 15.4% with Y90 as the reference value as shown in Figure 8(a). Likewise, for the nappe spray region, this varied from 26.68 to 40.04%, 19.04 to 37.71%, and −4 to 11.76% as shown in Figure 8(b). While for the step edge, the variation was 37.05 to 57.06%, 35 to 48.06%, and 4 to 18.89% as shown in Figure 8(c). It has been apparent that the variation between Y90 and Y99 is maximum in the step edge and minimum in the free-falling region. The selection of bulked water depth is very sensitive to the calculation of mean air concentration, therefore taking Y98 or Y99 for free-surface level may produce better results compared with Y90. The expression of for different flow depths is as follows:
(5)
(6)
(7)
Figure 8

(a) Variation of bulked water depth flows for q = 0.0214 m2/s Section-1, (b) variation of bulked water depth flows for q = 0.0214 m2/s Section-2, (c) variation of bulked water depth flows for q = 0.0214 m2/s Section-3, and (d) variation of Cmean for q = 0.0214 m2/s.

Figure 8

(a) Variation of bulked water depth flows for q = 0.0214 m2/s Section-1, (b) variation of bulked water depth flows for q = 0.0214 m2/s Section-2, (c) variation of bulked water depth flows for q = 0.0214 m2/s Section-3, and (d) variation of Cmean for q = 0.0214 m2/s.

Close modal

, , and are the mean air concentrations at flow depths of Y99, Y98, and Y90. Equations (5)–(7) are applicable for flow depth of Y99, Y98, and Y90. Similarly, the variation of Cmean is also different for all three zones as shown in Figure 8(d). As per Toombes & Chanson (2008a), Cmean for free-falling nappe varies from 0.05 to 0.35, and for the spray region, from 0.25 to 0.55 under the slope of 2.6° by using Y90 as the free surface. While in the present case, variations of Cmean in all three regions are shown in Figure 8(d) with three different depths (Y90, Y98, and Y99). In the free-falling section, the variation in Cmean varies from 0.259 to 0.518 for Y90, 0.303 to 0.619 for Y98, and 0.37 to 0.75 for Y99. Similarly, for the nappe-spray region, it varies from 0.45 to 0.608 for Y90, 0.57 to 0.731 for Y98, and 0.58 to 0.738 for Y99. While for the step edge, it varies from 0.38 to 0.53 for Y90, 0.63 to 0.70 for Y98, and 0.66 to 0.765 for Y99. As the selection of bulked water depth is very sensitive to the calculation of Cmean, taking Y98 or Y99 as the free-surface level will produce better results compared with Y90.

However, the difference between Y98 and Y99 in terms of Cmean is much less. So, Y98 can be taken as the free-surface level for the present study. It is also critical to examine the impact of these increased water depths on energy dissipation. Therefore, all these three flow depths are further considered to identify their effect on energy dissipation.

Effect of free-surface level on energy loss

Estimation of energy dissipation is one of the most vital parts of designing a stepped channel. Energy dissipation is the basic parameter to evaluate the efficiency of stepped channels. It identifies the functional ability of stepped channels at a particular step geometry. To obtain variation of flow depth on energy dissipation, all three of the aerated flow depths (Y90, Y98, and Y99) are considered. By considering equivalent clear water depth, energy dissipation at different locations (Section-1, Section-2, and Section-3) is also evaluated.

Consequently, the performance of energy dissipation depends on accurate measurement of air–water flow properties. The residual head at the chute end is the key parameter for the evaluation of the hydraulic performance of the channel. Relative energy loss (η) is commonly used to quantify energy dissipation. Residual energy at the step edge is calculated (Felder et al. 2019) as
(8)
where is the residual energy at flow depth Y90. The energy dissipation rate, ΔH/Hmax, is an indicator to evaluate the relative energy loss over the channel. The rate of energy dissipation is calculated as
(9)
As the upper limit of the aerated flow depth for skimming flow was taken as Y90, in case of nappe flow also a similar pattern was taken by Felder et al. (2019). But in the current research, it is found that identifying the free-surface level of nappe flow is different, and therefore, the criteria for selecting free-surface level of nappe flow by considering Y90 similar to skimming flow is not justified as per the observed flow pattern. Hence, residual energy at the step edge is also calculated for two other depths, Y98 and Y99, as
(10)
(11)
are the residual energy at the equivalent flow depths of Y98 and Y99, respectively. Equation (8) is applicable for the equivalent flow depth of Y90. Likewise, Equations (10) and (11) are applicable for the equivalent flow depths of Y98 and Y99. As per the literature, the calculation of Hres is based on accurate measurement of equivalent clear water depth. To examine the amount of variation in residual energy at each step, three flow depths are selected: Y90, Y98, and Y99. However, the selection of equivalent clear water depth between Y98 and Y99 for free-surface level is essential for precise estimation of energy dissipation. That's why a trial has been made in Figure 9(a) to get the %variation of residual energy along the channel.
Figure 9

Variation of energy dissipation with respect to step channel height for q = 0.0214 m2/s (a) relative variation of for step edge, (b) relative variation of for step edge, and (c) variation of for step edge.

Figure 9

Variation of energy dissipation with respect to step channel height for q = 0.0214 m2/s (a) relative variation of for step edge, (b) relative variation of for step edge, and (c) variation of for step edge.

Close modal

For the step edge, the variation of for depth of flow Y99 to Y90, Y98 to Y90, and Y99 to Y98 varied from −2.49 to −6.72%, −2.67 to −6.17%, and −0.515 to 0.502%, respectively. It clearly shows that Y90 overpredicts energy loss. In another way, the parameter is also used to show energy dissipation efficiency by using three flow depth conditions as shown in Figure 9(b). The relative energy loss varies from 0.228 to 2.16% for depth of flow Y99 to Y90, 0.22 to 2.16% for Y98 to Y90, and −0.03 to 0.11% for Y99 to Y98. It again shows that by using Y90, the energy dissipation rate is mostly underpredicted. Figure 9(c) shows the variation of for three different depths, which shows that the variation of for Y98 and Y99 is much less compared with Y90 for different channel heights. The study mentioned above leads to the finding that using Y98 flow depth is more advantageous than using Y90 and Y99. Therefore, the aerated flow depth Y98 is chosen as the free-surface level for further study.

Aerated property

Here in this section, the study of air concentration and its distribution across the flow depth have been discussed. For measurement of aeration parameters, three different locations (Section-1, placed at the inward side of jet; Section-2, placed at the outward side of the jet; and Section-3, placed at step edge) are selected to identify the behaviour of the jet. One of the most important parameters of aerated flow is the estimation of mean air concentration (Cmean). Ultimately, it facilitates the construction of the stepped channel for better aeration efficiency.

Based on the advective-diffusion equation given by Chanson & Toombes (2002b), is observed to influence the air concentration. Figure 10(a)–10(c) shows the variation of air concentration distribution along for different steps in three different regions. Figure 10(a) and 10(b) shows the variation of air concentration distribution against for different steps (Steps 4 to 10) at Section-2 and the step-edge region. Again, Figure 10(c) shows the variation of air concentration distribution against for different steps (Steps 4 to 10) at the free-falling region. The theoretical expression of Chanson & Toombes (2002b) (Equation (4)) matches well (Felder et al. 2019) with the present study and gives an S-shape profile as shown in Figure 10(a) and 10(b).
Figure 10

Variation of air concentration (C) distribution along (a) Section-2, (b) Section-3, and (c) Section-1.

Figure 10

Variation of air concentration (C) distribution along (a) Section-2, (b) Section-3, and (c) Section-1.

Close modal

However, in the case of the free-falling region, the pattern of the curve has been changed, although some variation has been observed in the range of from 0.22 to 0.6 owing to the presence of a pool. The observed pattern of air concentration distribution against matches well with the air concentration contour at the free-falling region. One of the important considerations in computing air concentration is defining the depth over which air concentration needs to be averaged out. The existing literature indicates the consideration of this region as 90% of flow water depth. Therefore, use of Y90 is very common in aerated flows. Since the region between Y90 to free-surface can have larger air concentration because of exchange processes happening near the surface, therefore it is also obvious to consider a certain proportion of air concentration between Y90 to free-surface.

Thus, two depths Y98 and Y99 are considered for computing air concentration. A plot between Cmean at Y90 and Y98 at the step edge for is shown in Figure 11(a)–11(d). This figure depicts these distinctive air–water flow characteristics as a function of the dimensionless distance downstream of Step edge 1, X/L.
Figure 11

Variation of depth average air concentration (Cmean) as a function of longitudinal length of the channel. (a) Model-1 Y90Cmean, (b) Model-1 Y98Cmean, (c) Model-2 Y90Cmean, and (d) Model-2 Y98Cmean.

Figure 11

Variation of depth average air concentration (Cmean) as a function of longitudinal length of the channel. (a) Model-1 Y90Cmean, (b) Model-1 Y98Cmean, (c) Model-2 Y90Cmean, and (d) Model-2 Y98Cmean.

Close modal

In addition to the air–water flow distribution, various typical air–water flow parameters were also considered for all data and measurements. The Cmean is one of the distinguishing factors that have been represented for different yc/h in Figure 11. It has been observed that for the wider channel, the difference between Y90 and Y98 varies up to 41%, whereas for the 0.28 m width channel, it varies up to 51.68%. Further, it is observed that there is not much variation in Cmean computed between Y98 and Y99 for both the models. Therefore, in the subsequent analysis, Y98 has been considered to compute mean air concentration for all further calculations. As per the analysis, Cmean at Y98 varies from 0.47 to 0.82 for the wider channel at different flow rates as shown in Figure 11(a) and 11(b). Whereas for Model-2, Cmean at Y98 ranges up to 0.78.

The difference between Cmean for two specific widths varies up to 16% for the initial few steps whereas the difference becomes insignificant as the number of steps increases. However, this analysis identifies the variation of Cmean as per different widths of the channel. So, during the design, a channel of wider width must be recommended to enhance the aeration properties in it.

Energy dissipation along the channel

In this phase of the study, the energy dissipation of a channel is examined for three separate locations (inward side of the jet, outward side of the jet, and step edge of a step) in a single step. Consecutively, the energy dissipation at the step edge of two different models (Model-1 and Model-2) is also included. However, it helps in identifying the effect of step geometry and location on energy dissipation.

Studies on energy dissipation were previously undertaken by several researchers on step edge. Those studies aimed to check the residual energy at the last step and efficiency of the model. However, in the present research, all the experiments are conducted to get the details about the mechanism behind energy dissipation, for which different sections are selected at each step. Figure 12(a)–12(c) shows the energy dissipation rate at different points of a step such as Section-1, Section-2, and Section-3 throughout the channel. It shows that maximum energy dissipation occurs at the step-edge region due to strikes of the jet at each successive step. Figure 12(b) shows the difference in ΔH/Hmax at different step edges for different flow rates.
Figure 12

Energy dissipation rate as a function of channel height for (a) Section-2, (b) Section-3, and (c) Section-1.

Figure 12

Energy dissipation rate as a function of channel height for (a) Section-2, (b) Section-3, and (c) Section-1.

Close modal
This observation simplifies some of the ambiguity regarding energy dissipation, specifically whether the energy loss in nappe flow increases or decreases with an increase in number of steps for the same height and certain flow rate (Chanson 1994a, 1994b; Matos & Quintela 1995b; Peruginelli & Pagliara 2000; Chinnarasri & Wongwises 2006). The present analysis verified that with the increase in the number of steps, energy dissipation increases. The present study also supports the statement given by Christodoulou (1993) that a considerable increase in energy dissipation has been observed due to an increase in the number of steps for a certain ratio of yc/h. From the present analysis, it is clear that with the increase in the number of steps, energy dissipation increases, and at a certain point, it reaches its optimum value from where the dissipation rate becomes insignificant. In the present observation, the rate of energy dissipation became insignificant near Step 8, or 80% of the total length of channel, as shown in Figure 13(a) and 13(b).
Figure 13

Energy dissipation at step edge for Model-1 (0.52 m width) and Model-2 (0.28 m width) (a) yc/h = 0.36 and (b) yc/h = 0.42.

Figure 13

Energy dissipation at step edge for Model-1 (0.52 m width) and Model-2 (0.28 m width) (a) yc/h = 0.36 and (b) yc/h = 0.42.

Close modal
Likewise, the effect of channel width on energy dissipation has been found and shown in Figure 13, with the wider channel showing greater potential to dissipate potential energy. For the smaller width, the dissipation rate is relatively less compared with the wider channel for a few initial steps where variation reaches 26% for the same unit discharge. For the low-discharge flow, the relative variation is less, but as the discharge increases, the variation increases. Further, an important part of this study is to predict energy dissipation from the known parameters of any specific design. The equation proposed from the observed energy plot against the channel height at different steps is
(12)
However, a single parametric study is not sufficient to represent the energy dissipation property. To investigate in further detail, a parametric study has been conducted. To understand the effect of jet parameters on energy dissipation, all the dimensional parameters such as ρw, g, h, l, yc, N, ΔH, w, Hmax, and Q are taken into consideration. Here, ρw is the density of water, g is the gravitational acceleration, and Q is the total flow rate. Considering all the parameters, the relative energy loss downstream of N number of steps with a constant slope can be expressed in dimensional analysis. By selecting ρw, g, and Hmax as the repeated variables, a dimensional analysis using the Buckingham theorem is considered as follows:
(13)
(14)
A total 71 number of datasets are taken at the step-edge region to predict energy dissipation. To analyse the datasets, all the datasets are divided into training (75%) and testing (25%) segments. The use of correlation and regression analysis is required to determine the variables influencing the target variable. The Pearson correlation coefficient between the energy dissipation rate and the independent factors shows the clarity to choose the correct input parameters for the prediction. The highest correlation coefficient is observed between and . Likewise, during training and testing, the variables with the lowest relationship (Rc = 0.61) are observed in between and . However, all the factors have a significant correlation (Rc ≥ 0.5) with one another, and elimination of any single parameter might have an impact on the prediction accuracy. Therefore, all the parameters are taken for the prediction of multi-nonlinear regression expression to predict energy dissipation as follows:
(15-i)
(15-ii)
However, the Violin box diagram is used to represent the efficiency of the predicted energy dissipation of the training and testing datasets in Figure 14. As for the regression analysis, it took into consideration three major parameters, namely, From this observation, it can be resolved that the experimentally observed and predicted datasets show good correlation. Equation (15) provides a precise estimation of energy loss within a range of 0.201 ≤ yc/h ≤ 0.685.
Figure 14

Violin box of predicted training and testing datasets versus observed datasets.

Figure 14

Violin box of predicted training and testing datasets versus observed datasets.

Close modal

Designing a stepped channel for drainage in a hilly area is one of the climate-induced disaster mitigation strategies that have been suggested here. To achieve a wide view of this investigation, data from the current study were obtained. This modelling approach encourages more research to make stepped channel design simpler. This is probably a means of reducing the after-effects of a natural catastrophe and enhancing its use in the actual world.

Here, the few main functions of the flow over stepped channel have been discussed: primarily, its capacity of aeration, and subsequently, its capacity for dissipating high potential energy. Different properties of jets such as jet length and pool water depth are studied to get an idea of the steady state of the jet region where the fluctuations of Ljet/h and dp/h in successive steps are less. From this study, it is observed that at nearly 60–70% of the entire length or Step 7 onward, a steady state of the jet has been achieved. This finding will also be beneficial during the design of steps with varying geometric shapes rather than uniform steps, to ensure flow stability. To obtain even more clarity on the free-surface of the aerated flow depth, three flow depths (h1, h2, h3) were taken into consideration (Figures 811). It was discovered how flow depth affects the mean air concentration (aeration). However, the free-surface level was taken to be Y98. This finding aids in accurately calculating energy dissipation and reduces the possibility of over- or underestimating energy loss. Additionally, finding the set of input parameters and their role in predicting energy dissipation at different stages, and creating a functional relationship that can accurately predict energy dissipation, was the final objective of this research. Finally, the effect of aerated flow depths on energy dissipation (Figure 9) as well as the expression (Figures 1214) to predict energy dissipation is proposed based on the geometry of the channel. With the proposed expression (Equation (15)), design of stepped channels becomes more feasible.

Further, some statistical analysis has been conducted to analyse the efficiency of the predicted energy dissipation datasets. In this regard, the following goodness-of-fit parameters are selected:

  • Correlation coefficient: 0 ≤ CC ≤ 1
    (16)
  • Squared correlation coefficient: 0 ≤ R2 ≤ 1
    (17)
  • Root mean squared error: 0 ≤ RMSE ≤ 1
    (18)
    where N is the number of data, yexp is the experimental data, and ysim is the simulated data.

It displays the predicted values of energy loss with higher accuracy using Equation (15). The experimentally observed and predicted datasets are shown in Figure 15(d) with a correlation coefficient of 0.961 and RMSE of 0.040451. Since the above approach gives considerably good results in more than 97.88% of the cases, it proves an efficient method to compute at each step for the nappe flow. A summary of the present experimental parameters is given in Table 4. This expression has taken the variation of width and its effect on energy dissipation into consideration. It may be useful in both the planning and design of a stepped waterway. One more finding of this study is that for the nappe flow the wider channel has greater energy dissipation ability (Figure 13). Further, the ineffective culverts and storm waterways that are incapable of handling high discharge during heavy rainfall may be reused by increasing their widths.
Table 4

Summary of the experimental data collected from the present study under nappe flow

ParametersUnitRange
MinimumMaximum
Unit discharge (qwm2/s 0.00892 0.0561 
Ljet/h – 0.96 1.85 
dp/h – 0.02 0.685 
Cmean – 0.259 0.83 
yc/h – 0.201 0.685 
Nh/yc – 2.91 44.77 
w/yc – 4.08 25.87 
 – 0.425 0.956 
ParametersUnitRange
MinimumMaximum
Unit discharge (qwm2/s 0.00892 0.0561 
Ljet/h – 0.96 1.85 
dp/h – 0.02 0.685 
Cmean – 0.259 0.83 
yc/h – 0.201 0.685 
Nh/yc – 2.91 44.77 
w/yc – 4.08 25.87 
 – 0.425 0.956 
Figure 15

(a) Energy dissipation at the step edge of the present study for Model-1 and the existing literature, (b) energy dissipation at the step edge for Model-2 and the existing literature, (c) energy dissipation at the step edge for Model-1, 2, and the existing literature, (d) agreement diagram of the observed and predicted datasets, (e) agreement diagram of simulated datasets and existing expression of Chanson (1994a), and (f) agreement diagram of simulated datasets and existing expression of Chamani & Rajaratnam (1994).

Figure 15

(a) Energy dissipation at the step edge of the present study for Model-1 and the existing literature, (b) energy dissipation at the step edge for Model-2 and the existing literature, (c) energy dissipation at the step edge for Model-1, 2, and the existing literature, (d) agreement diagram of the observed and predicted datasets, (e) agreement diagram of simulated datasets and existing expression of Chanson (1994a), and (f) agreement diagram of simulated datasets and existing expression of Chamani & Rajaratnam (1994).

Close modal

To further compare the present results, experimental data with varying slopes as well as widths of channels from the literature (Essery & Horner 1978; Pinheiro & Fael 2000; Chanson & Toombes 2002a; Renna & Fratino 2010; Felder et al. 2019) are well compared with the present experimental data in Figure 15(a)–15(c). Eventually, the current results showed a decrease in energy dissipation performance with increasing flow rate, which is also consistent with the earlier findings (Essery & Horner 1978; Pinheiro & Fael 2000; Chanson & Toombes 2002a; Renna & Fratino 2010; Felder et al. 2019). These results of existing experimental studies are based on different instrumentation, different methods of estimation, and different ranges of input parameters as mentioned in Table 1. After having all these differences in experimental conditions, the energy dissipation data of the present study as well as the existing study can be explained by the fact that the energy dissipation decreases with the increase in flow rate.

However, few proposed expressions are again compared with the present datasets. The observed and predicted datasets by using the expression given by Chanson (1994a) (Equation (2)) and Chamani & Rajaratnam (1994) (Equation (1)) are also compared in Figure 15(e) and 15(f). These expressions show good agreement with the present dataset with an error of ±29.30% for the expression given in Equation (2) and ±37.44% for the expression given in Equation (1). However, the proposed expression (Equation (15)) from the present study shows a better result with an error of ±10%.

Finally, based on the flow parameters (Table 4), the regression model was developed to estimate the energy dissipation . Equation (15) can be used effectively for the initial design of a stepped channel. Even though it has been derived based on certain broad assumptions and laboratory studies (w, l, h, N, α, discharge), it can still predict the energy dissipation efficiently. This study is limited to nappe flow. Therefore, the expressions suggested in this study are less appropriate for transitional or skimming flows, because the energy dissipation processes in the skimming flow and transition flow are different.

However, this study describes a climate change–mitigation approach that uses nappe flow to construct stepped storm waterways on mountainous roads to address climate change challenges. It regulates the flow throughout every step with a high impact that would likely reduce the energy downstream and reduce the risk of landslides and highway erosion. In summary, a thorough study on stepped channels was conducted by taking both air and water flow properties and the energy dissipation potential into consideration. In this regard, two different models with varying widths were taken. To predict the energy dissipation of a stepped channel, different parametric studies were conducted at different flow rates.

One of the major goals of the present work is to design a stepped storm waterway that can regulate surplus water during periods of heavy rainfall, distribute the potential energy of flowing water, and protect the hilly road against damages caused by heavy rain in the Himalayan range. To accomplish these objectives, two types of models with different datasets of air concentrations with various jet parameters were studied. A stepped channel with two different widths was experimentally modelled to verify its utility and efficiency in successfully handling the underpass rainwater drainage system as of a hilly road or highway. In this regard, both air and water flow properties and energy dissipation parameters were systematically studied in the current research. The following results are obtained from the present study.

Fluctuations of pool water depth and jet length become stable from Step 7 onwards. The present analysis confirmed that the flow gets stable at X/L ≥ 0.6. One of the important considerations in computing air concentration is to define the depth over which air concentration needs to be averaged out. As per the air–water flow properties, three different bulked water depths were studied to decide the most appropriate depth for the free-surface level. From the computation of the Cmean, the results are found to be sensitive to the selection of flow depths. The use of Y90 predicts a lesser value of Cmean, which means it is underpredicting the mean air concentration. In the present study, mean air concentration was computed based on Y90, Y98, and Y99. However, the difference in the results of Y98 and Y99 appears to be insignificant. Likewise, the effect of these flow depths on energy dissipation was also found. The variation of the residual head at the step edge in terms of was found to be minimum between Y99 and Y98, as −0.515%, whereas between Y98 and Y90, it was found to range from −2.67 to −6.17%. This means the residual head is overpredicted by using Y90 flow depth. Similarly, the variation in for the flow depths, Y98 and Y90, was found to range from 0.22 to 2.16%. Therefore, it is suggested to use Y98 for mean air concentration as well as energy dissipation.

The mean air concentration and energy dissipation rate of the stepped channel for two specific widths have been studied. The maximum energy dissipation has been observed at the step-edge region. Likewise, the wider channel has a better potential ability to dissipate high potential head. For a few initial steps, the dissipation efficiency is lower for a narrower channel than the broader channel, with a relative difference of 26%. The present study also provides multi-nonlinear regression expression for predicting energy dissipation by taking channel property and flow conditions as the known input parameters (Nh/yc, yc/h, and w/yc). The current study may be useful in predicting energy dissipation at the step edge by taking channel properties as input parameters.

To obtain the optimum design for stepped channel at any specific location, an integrated study of the hydrological incidence of severe rainfall events and hydraulics of the stepped storm waterway is necessary for effective modelling. Further, in designing a stepped storm waterway, variation of slopes as well as step geometry (pooled steps, non-uniform steps, flip-bucket shaped steps) can be studied taking the stability of flow, variation of jet, and energy dissipation efficiency into consideration.

The authors are thankful to the entire staff of Hydraulics Laboratory, Department of Civil Engineering, IIT Roorkee, India, for the efficient experimental set-up of the channel.

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

The authors declare there is no conflict.

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