# Two-Dimensional Simulation of Flows in an Open Channel with Groin-Like Structures by iRIC Nays2DH

Authors: Md. Shahjahan Ali; Md. Milon Hasan; Masuma Haque
Journal: Mathematical Problems in Engineering
 (2017)

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## Abstract

This study presents the results obtained from the numerical simulation on turbulent flows around a single groin for different orientations. Here iRIC Nays2DH, which is based on 2D model, is used to simulate the flows in a straight open channel with groin of 45°, 90°, and 135° angled with the approaching flow. A depth-averagedk-ε model is used as turbulence closure model with finite differential advections as upwind scheme. The numerical results of velocity and bed shear stress profiles are compared with the available experimental data. Good agreements are found between experimental and calculated results. From the simulation, it is observed that the peak of velocity and bed shear stress is maximum at the position of head of groin when lateral distance y/l=1, wherel is the groin length. The position of maximum velocity and bed shear stress is found to be shifted towards downstream with increasing y/l. The maximum velocity and bed shear stress for 135° groin are found lower than the other two cases for all the sections of y/l.


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## Body

## 1. Introduction

The simulation of water flow and sediment transport in rivers has been the subject of many researches in the field of hydraulics and river engineering [1]. In hydraulics and coastal engineering, groins are very important structures for river navigation, coastal protection, and beach reclamation [2]. It is an elongated obstruction having one end on the bank of the stream and the other end projecting into the current. Groins have been used extensively all over the world as river training and bank protection structure to reduce the current along the stream bank, thus reducing the erosive capacity of the stream and in some cases inducing sedimentation between two groins. It can be built at right angles to the bank or current (normal/deflecting groin) or angled towards upstream (repelling groin) or angled towards downstream (attracting groin). The obstructed flow field in the downstream of a single groin or the flow field enclosed by two consecutive groynes is low velocity region compared to mainstream. This type of zone is generally termed as dead zone [3]. Flow velocity inside such kind of arrangement is lower than main channel. In addition to engineering applications, such structures increase the biodiversity of aquatic species by creating habitat and providing shelter for them. The main stream of a river, where the velocity is high, is not suitable for weak and small fishes. That is why the dead zone is a suitable shelter for them.Many experimental and numerical researches have been performed to investigate the flow pattern and scouring around groins [4–7]. Those studies were carried out in different conditions in terms of groin length, groin inclination angle to the flow direction, permeable or impermeable states, submerged and nonsubmerged states, flow separation, recirculating length, and number of groins. The groin which is placed perpendicular to the river approaching flow causes narrowing and deviation of the flow and consequently this gives a complex three-dimensional form to flow around a groin [4, 5]. However, dealing with the practical engineering problems, such as alluvial geomorphic processes, it is computationally efficient to use 2D models compared to 3D. In this study, 2D software called iRIC Nays2DH (available in http://www.i-ric.org) has been used which is based on Navier-Stokes equations to simulate the flows in an open channel with groin-like structures.It is well known that the RANS (Reynolds Averaged Navier-Stokes) type turbulence models, such as two-equation model or Reynolds stress model, are the most popular tool used for practical engineering applications [8–10]. Because it requires less CPU time and computer memory compared to LES and DNS. Therefore, the clarification of the possibility, the limitation, and areas of improvement of RANS models should be still paid attention to. To resolve the Reynolds stress term which appeared in the averaged Navier-Stokes equations, the k-ε model is one of the most frequently adopted ones [10, 11]. However, the standard k-ε model cannot produce satisfactory results for the flow field having high rate of strain and rotation [12, 13]. In iRIC Nays2DH, a nonlinear k-ε model is used to predict the turbulent flow field by capturing the anisotropic turbulence.


## 2. Basic Equations of the Model

iRIC (International River Interface Cooperative), pre- and postprocessing software application and framework for computational models of flow and sediment transport in rivers, is used in this study. The application is a Graphical User Interface (GUI) that allows the model user to build, run, and visualize the results of the system’s computational models. The GUI provides tools for building both structured and unstructured grids, defining topography and other boundary conditions on the grid, and defining grid-dependent values such as grain size, vegetation, and obstacles by mapping measured values to the grid or by creating user-defined polygons with attributes of grid-dependent value. It combines the functionality of MD_SWMS, developed by the USGS (U.S. Geological Survey), and RIC-Nays, developed by the Foundation of Hokkaido River Disaster Prevention Research Center. The details of the model can be found in iRIC [14] and Jang and Shimizu [15].For the analysis, the general curvilinear coordinate system is adopted, allowing direct consideration of complex boundaries and riverbed shapes. Basic equations of two-dimensional plane flow at orthogonal coordinates(x,y) are transformed into general coordinates (ξ,η). By transforming the equations into general coordinates, it becomes possible to set a calculation mesh of any shape (in keeping with the boundary conditions). The basic equations in an orthogonal coordinate system (x,y) are as follows [16].Equation of Continuity
(1)
∂
h
∂
t
+
∂
h
u
∂
x
+
∂
h
v
∂
y
=
0
.
Equations of Motion
(2)
∂
u
h
∂
t
+
∂
h
u
2
∂
x
+
∂
h
u
v
∂
y
=
-
h
g
∂
H
∂
x
-
τ
x
ρ
+
D
x
,
∂
v
h
∂
t
+
∂
h
u
v
∂
x
+
∂
h
v
2
∂
y
=
-
h
g
∂
H
∂
y
-
τ
y
ρ
+
D
y
,where h is water depth, t is time, u is velocity in the x direction, v is velocity in the y direction, g is gravitational acceleration, and H is the total water depth. Here, the bed shear stresses in x and y directions (τx and τy) are expressed by using coefficient of riverbed shearing force Cf as(3)τxρ=Cfuu2+v2,τyρ=Cfvu2+v2.In the model, the bottom friction is set using Manning’s roughness parameter. The coefficient of riverbed shearing force Cf is estimated by Manning’s roughness parameter nm as follows:(4)Cf=gnm2h3.The diffusion terms in x and y directions are expressed as (5) and (6), respectively. Here, vt is the eddy viscosity coefficient.(5)Dx=∂∂xvt∂uh∂x+∂∂yvt∂uh∂y,(6)Dy=∂∂xvt∂vh∂x+∂∂yvt∂vh∂y.


### 2.1. Depth-Averagedk-ε Model

The eddy viscosity coefficientvt in the standard k-ε model is expressed by the following equation:(7)vt=Cμk2ϵ,where Cμ is a model constant. k and ϵ are obtained by the following equations [16]:(8)∂k∂t+u∂k∂x+v∂k∂y=∂∂xvtσk∂k∂x+∂∂yvtσk∂k∂y+Ph+Pkv-ϵ,∂ϵ∂t+u∂ϵ∂x+v∂ϵ∂y=∂∂xvtσϵ∂ϵ∂x+∂∂yvtσϵ∂ϵ∂y+C1ϵϵkPh+Pϵv-C2ϵϵ2k,where C1ϵ, C2ϵ,  σk, and σϵ are model constants whose respective values are shown in Table 1. Note that Pkv and Pϵv are calculated with the following equations:(9)Pkv=Cku∗3h,Pϵv=Cϵu∗4h2.Table 1
Model constants for nonlineark-ε model [16].
Cμ
C1ε
C
2
ε
σ
k
σ
ε
0.09
1.44
1.92
1.0
1.3


## 2.1. Depth-Averagedk-ε Model

The eddy viscosity coefficientvt in the standard k-ε model is expressed by the following equation:(7)vt=Cμk2ϵ,where Cμ is a model constant. k and ϵ are obtained by the following equations [16]:(8)∂k∂t+u∂k∂x+v∂k∂y=∂∂xvtσk∂k∂x+∂∂yvtσk∂k∂y+Ph+Pkv-ϵ,∂ϵ∂t+u∂ϵ∂x+v∂ϵ∂y=∂∂xvtσϵ∂ϵ∂x+∂∂yvtσϵ∂ϵ∂y+C1ϵϵkPh+Pϵv-C2ϵϵ2k,where C1ϵ, C2ϵ,  σk, and σϵ are model constants whose respective values are shown in Table 1. Note that Pkv and Pϵv are calculated with the following equations:(9)Pkv=Cku∗3h,Pϵv=Cϵu∗4h2.Table 1
Model constants for nonlineark-ε model [16].
Cμ
C1ε
C
2
ε
σ
k
σ
ε
0.09
1.44
1.92
1.0
1.3


## 3. Numerical Tests

### 3.1. Flow Domain and Hydraulic Parameters

The hydraulic parameters for different test cases that were simulated are shown in Table2. The parameters for case 2 of flows in a straight open channel with groin of 90° angle to the direction of flow were taken the same as the experiments by Rajaratnam and Nwachukwu [7]. In their experiments, a 37 m long, 0.9 m wide, and 0.76 m deep flume with smooth bed and sides were used. The groin was an aluminum plate with 3 mm thickness and 152 mm length and was projected partly above the water surface. The hydraulic parameters for the 45° and 135° angled groin are the same as case 2.Table 2
Hydraulic parameters for the simulated cases.
Cases
Groinposition
L (m)
W (m)
Q
o (m3/s)
h
o (m)
S
o
n
U/S
D/S
Case1
45°
2
4
0.9
0.043
0.189
0.001
0.01
Case2
90°
2
4
0.9
0.043
0.189
0.001
0.01
Case3
135°
2
4
0.9
0.043
0.189
0.001
0.01
Here,L = length of the straight channel, W = width of channel, Qo = upstream discharge, ho = water depth at downstream, So = channel slope, and n = Manning’s roughness coefficient.Figure2 shows the sketch of the flow domain for flows in a straight open channel with groin of 90° angled to the direction of flow which was performed under the same conditions of the experiments conducted by Rajaratnam and Nwachukwu [7]. Figures 1 and 3 show the sketch of the flow domain for 45° and 135° which were performed under the same conditions as case 2. For all these cases, 120 × 20 grids were used considering fixed bed condition. Figure 4 shows a sample of computational mesh that consists of 120 grids in the longitudinal direction and 20 grids in transverse directions.Figure 1
Groin orientation for 45° angled to the direction of flow (case 1).Figure 2
Groin orientation for 90° angled to the direction of flow (case 2).Figure 3
Groin orientation for 135° angled to the direction of flow (case 3).Figure 4
Plan of input grid for simulation of flow around groin with 45° angle (case 1).For all the cases of numerical simulation, the computational domain was 6 m in length and 0.9 m in width. The upstream and downstream boundaries were located at 2 m and 4 m away from the groin, respectively. The constant discharge at upstream was 0.043 m3/s, and at the downstream the constant flow depth was 0.189 m. Manning’s roughness coefficient n=0.01 and the time step Δt = 0.003 sec are assigned in the present computation. The simulations are performed in fixed bed condition with bottom slope, So=0.001.Quanhong and Pengzhi [17] also used the same experimental data of Rajaratnam and Nwachukwu [7] to validate their model. Governing equations of their model were shallow water equations and depth-averaged k-ε model as the turbulence model. According to Quanhong and Pengzhi [17] model, the computational domain was 6 m in length and 0.9 m in width. Flow flux of 0.047817 m2/s and water depth of 0.189 m are specified at the upstream and downstream boundaries, respectively. For the same flow geometry and hydraulic conditions, Sarveram et al. [2] also simulated the flow field around 90° groin using semi-implicit semi-Lagrangian method and compared their computed results with the Rajaratnam and Nwachukwu’s experimental result. In the present study, the simulated flow field is compared with previous experimental results of Rajaratnam and Nwachukwu [7] as well as previous simulation results of Quanhong and Pengzhi [17] and Sarveram et al. [2].


### 3.2. Computational Scheme

The governing equations for mean velocities and turbulent flows were discretized with the finite difference method based on full staggered boundary fitted coordinate system. The basic equations are discretized as fully explicit forms and solved successively with the time increment step by step. It is solved using iterative procedure at each time step. Constant discharge at upstream and constant depth with zero velocity gradients were given as downstream boundary conditions. Finite difference scheme was used for the solution of the equations, where the nonlinear convection terms were discretized with the upwind scheme.


## 3.1. Flow Domain and Hydraulic Parameters

The hydraulic parameters for different test cases that were simulated are shown in Table2. The parameters for case 2 of flows in a straight open channel with groin of 90° angle to the direction of flow were taken the same as the experiments by Rajaratnam and Nwachukwu [7]. In their experiments, a 37 m long, 0.9 m wide, and 0.76 m deep flume with smooth bed and sides were used. The groin was an aluminum plate with 3 mm thickness and 152 mm length and was projected partly above the water surface. The hydraulic parameters for the 45° and 135° angled groin are the same as case 2.Table 2
Hydraulic parameters for the simulated cases.
Cases
Groinposition
L (m)
W (m)
Q
o (m3/s)
h
o (m)
S
o
n
U/S
D/S
Case1
45°
2
4
0.9
0.043
0.189
0.001
0.01
Case2
90°
2
4
0.9
0.043
0.189
0.001
0.01
Case3
135°
2
4
0.9
0.043
0.189
0.001
0.01
Here,L = length of the straight channel, W = width of channel, Qo = upstream discharge, ho = water depth at downstream, So = channel slope, and n = Manning’s roughness coefficient.Figure2 shows the sketch of the flow domain for flows in a straight open channel with groin of 90° angled to the direction of flow which was performed under the same conditions of the experiments conducted by Rajaratnam and Nwachukwu [7]. Figures 1 and 3 show the sketch of the flow domain for 45° and 135° which were performed under the same conditions as case 2. For all these cases, 120 × 20 grids were used considering fixed bed condition. Figure 4 shows a sample of computational mesh that consists of 120 grids in the longitudinal direction and 20 grids in transverse directions.Figure 1
Groin orientation for 45° angled to the direction of flow (case 1).Figure 2
Groin orientation for 90° angled to the direction of flow (case 2).Figure 3
Groin orientation for 135° angled to the direction of flow (case 3).Figure 4
Plan of input grid for simulation of flow around groin with 45° angle (case 1).For all the cases of numerical simulation, the computational domain was 6 m in length and 0.9 m in width. The upstream and downstream boundaries were located at 2 m and 4 m away from the groin, respectively. The constant discharge at upstream was 0.043 m3/s, and at the downstream the constant flow depth was 0.189 m. Manning’s roughness coefficient n=0.01 and the time step Δt = 0.003 sec are assigned in the present computation. The simulations are performed in fixed bed condition with bottom slope, So=0.001.Quanhong and Pengzhi [17] also used the same experimental data of Rajaratnam and Nwachukwu [7] to validate their model. Governing equations of their model were shallow water equations and depth-averaged k-ε model as the turbulence model. According to Quanhong and Pengzhi [17] model, the computational domain was 6 m in length and 0.9 m in width. Flow flux of 0.047817 m2/s and water depth of 0.189 m are specified at the upstream and downstream boundaries, respectively. For the same flow geometry and hydraulic conditions, Sarveram et al. [2] also simulated the flow field around 90° groin using semi-implicit semi-Lagrangian method and compared their computed results with the Rajaratnam and Nwachukwu’s experimental result. In the present study, the simulated flow field is compared with previous experimental results of Rajaratnam and Nwachukwu [7] as well as previous simulation results of Quanhong and Pengzhi [17] and Sarveram et al. [2].


## 3.2. Computational Scheme

The governing equations for mean velocities and turbulent flows were discretized with the finite difference method based on full staggered boundary fitted coordinate system. The basic equations are discretized as fully explicit forms and solved successively with the time increment step by step. It is solved using iterative procedure at each time step. Constant discharge at upstream and constant depth with zero velocity gradients were given as downstream boundary conditions. Finite difference scheme was used for the solution of the equations, where the nonlinear convection terms were discretized with the upwind scheme.


## 4. Simulated Flow Field

Figures5 and 6 show the predicted velocity vector of the flow field around the groin for different angles with the flow. For all the cases, the model is found to reproduce the general flow features of the flow field around the groin successfully. From the simulated results, it is seen that at the upstream boundary the flow is uniform and hence the flow vectors are straight and parallel to bank. However, when the flow approaches the groin, the flow is deviated towards the left bank compared to the right due to obstruction of flow by the groin. A recirculation zone is observed just downstream region of the groin for all the cases.Figure 5
Computed velocity vector for (a) case 1, (b) case 2, and (c) case 3 developed by iRIC Nays2DH.
(a)
(b)
(c)Figure 6
Computed velocity vector and recirculation zone around groin for (a) case 1, (b) case 2, and (c) case 3 developed by iRIC Nays2DH.
(a)
(b)
(c)Figure7 shows the streamline around a groin, which is obtained by the present study. From the streamline contour, it is also found that at the position of groin head the flow is deviated towards the opposite bank and at the downstream of the groin there is a circulation. Figures 6 and 7 depict that for case 1 (45° groin) the deviations of vectors and streamlines are higher compared to case 2 (90° groin). 135° groin for case 3 shows the least deviation compared to other cases. The length of circulation zone at downstream of the groin is also higher for case 1 and lower in case 3.Figure 7
Streamline around a groin for (a) case 1, (b) case 2, and (c) case 3 developed by iRIC Nays2DH.
(a)
(b)
(c)


## 5. Comparison of Simulated Results with Previous Studies

Simulated results such as computed velocity profiles and bed shear stress profiles for 90° groins (case 2) are compared with previous experimental as well as available previous simulation results. The comparison is described in the following sections.


### 5.1. Velocity Profiles

For 90° groins, the resultant velocity profiles are compared with available experimental results measured aty/l = 1.0, 1.5, 2.0, 3.0, and 4.0, where l = 152 mm is the length of the groin. Figure 8 shows the comparison of velocity profiles for different lateral distances (y/l). Here, the initial flow velocity and water depth were Uo = 0.253 m/s and H = 0.189 m, respectively. In the figure, all the velocities were normalized by Uo. In the figure, x/l = 0 indicated the groin position along flume direction.Figure 8
Comparison of resultant velocity profiles (W) with the available previous studies for 90° groin (case 2).Good agreements are found between experimental and calculated results. For the velocity profiles, the only large discrepancy occurs aty/l=2, where the calculated results underpredict the experimental data in the downstream zone of the groin. It is noticed that the numerical results reported by Quanhong and Pengzhi [17] and Sarveram et al. [2] also underpredicted the experimental data largely in this region. This may be due to the very high velocity gradient arising in this region which makes the depth-averaged model inapplicable. Otherwise, the possible reason may come from the experimental measurement errors in this region [17].


### 5.2. Bed Shear Stress Profiles

Figure9 shows comparison of bed shear stress profiles (τ) of predicted results with the available previous studies. In the figure, all the shear stresses are normalized by τo = 0.1293 N/m2. The comparison between the numerical results and experimental data shows reasonable agreement. For the lateral sections up to y/l = 2, the simulated results underpredict the downstream shear stress slightly. The numerical results reported by Quanhong and Pengzhi [17] also show similar prediction. It may be the deficiency of the depth-averaged model to account for the high velocity gradient arising very near to the groin.Figure 9
Comparison of bed shear stress profiles (τ) with the available previous studies for 90° groin (case 2).


## 5.1. Velocity Profiles

For 90° groins, the resultant velocity profiles are compared with available experimental results measured aty/l = 1.0, 1.5, 2.0, 3.0, and 4.0, where l = 152 mm is the length of the groin. Figure 8 shows the comparison of velocity profiles for different lateral distances (y/l). Here, the initial flow velocity and water depth were Uo = 0.253 m/s and H = 0.189 m, respectively. In the figure, all the velocities were normalized by Uo. In the figure, x/l = 0 indicated the groin position along flume direction.Figure 8
Comparison of resultant velocity profiles (W) with the available previous studies for 90° groin (case 2).Good agreements are found between experimental and calculated results. For the velocity profiles, the only large discrepancy occurs aty/l=2, where the calculated results underpredict the experimental data in the downstream zone of the groin. It is noticed that the numerical results reported by Quanhong and Pengzhi [17] and Sarveram et al. [2] also underpredicted the experimental data largely in this region. This may be due to the very high velocity gradient arising in this region which makes the depth-averaged model inapplicable. Otherwise, the possible reason may come from the experimental measurement errors in this region [17].


## 5.2. Bed Shear Stress Profiles

Figure9 shows comparison of bed shear stress profiles (τ) of predicted results with the available previous studies. In the figure, all the shear stresses are normalized by τo = 0.1293 N/m2. The comparison between the numerical results and experimental data shows reasonable agreement. For the lateral sections up to y/l = 2, the simulated results underpredict the downstream shear stress slightly. The numerical results reported by Quanhong and Pengzhi [17] also show similar prediction. It may be the deficiency of the depth-averaged model to account for the high velocity gradient arising very near to the groin.Figure 9
Comparison of bed shear stress profiles (τ) with the available previous studies for 90° groin (case 2).


## 6. Simulation Results for Different Cases

### 6.1. Predicted Velocity Profiles

Figure10 shows the comparison among predicted velocity profiles (W) for case 1, case 2, and case 3. For each case, the longitudinal velocity profiles are compared at a lateral position of y/l = 1.0, 1.5, 2.0, 3.0, and 4.0. In the figure, all the velocities are normalized by U0 = 0.253 m/s and here x/l = 0 indicates the groin position in the longitudinal direction. The comparisons among the three cases show reasonable differences. Along line y/l=1, the peak of velocities is found at longitudinal distances of x/l = −0.28, 0.0, and 0.56 for case 1, case 2, and case 3, respectively. For y/l=1.0, in all the cases, the velocity is found to be decreased from upstream velocity just before the position of groin head. In other words, in addition to the circulation zone at downstream of groin, a small low velocity zone is observed just upstream of groin at right bank. Along the line y/l=1.5, the peak of velocities is found at longitudinal distances of x/l = −1.0, 0.22, and 0.67 for case 1, case 2, and case 3, respectively. These peak velocities are found to be decayed with the longitudinal distance x/l. For y/l=2, the peaks of velocities are found at a distance of x/l = −0.11, 1.22, and 2.54 for case 1, case 2, and case 3, respectively. For y/l≥2, the decay of velocity along the downstream is found to be slower compared to the regiony/l ≤1.5. Along the line y/l=3, the peak of velocities is found at longitudinal distances of x/l=2.87, 3.53, and 3.88 for case 1, case 2, and case 3, respectively. Along the line y/l=4, the peak of velocities is found at longitudinal distances of x/l = 3.33, 3.89, and 4.44 for case 1, case 2, and case 3, respectively.Figure 10
Comparison between resultant velocity profiles (W) of present study for case 1, case 2, and case 3 along lateral distance, y/l=1, 1.5, 2, 3, and 4.From the figures, it is observed that the peak of velocity is found maximum at the position of head of groin wheny/l=1. However, this position of maximum velocity is found to be shifted towards downstream with increasing y/l. The maximum velocity for case 3 is found lower than the other two cases for all the sections of y/l. However, W/Uo for 90° groin is found maximum for y/l≤2; and for y/l>2, the velocity is maximum for 45° angled groin.


### 6.2. Predicted Bed Shear Stress Profiles

Figure11 shows the predicted bed shear stress profiles (τ) of the proposed model for case 1, case 2, and case 3. For each case, the longitudinal shear stress profiles are compared at a lateral position of y/l = 1.0, 1.5, 2.0, 3.0, and 4.0. In the figure, all the shear stresses are normalized by τo = 0.1293 N/m2, which is the value of upstream region. Here, x/l=0 is the groin position along longitudinal direction. The profiles of bed shear stress are found in similar pattern of velocity profiles. For different values of y/l, the peak of shear stresses is found at the same longitudinal distances (x/l) as reported in velocity profiles. For y/l=1.0, in all the cases, the shear stress is found to be decreased from its upstream value just before the position of groin head.Figure 11
Comparison between computed bed shear stress profiles (τ) of proposed model for case 1, case 2, and case 3 along lateral distance, y/l=1, 1.5, 2, 3, and 4.From the figures, it is observed that the peak of bed shear stress is found maximum at the position of head of groin wheny/l=1. However, this position of maximum bed shear stress is found to be shifted towards downstream with increasing y/l. These peak shear stresses are found to be decayed with the longitudinal distance x/l. However, for y/l≥2, the decay of shear stress along the downstream is found to be slower compared to the region y/l≤1.5. The maximum bed shear stress for case 3 is found lower than the other two cases for all the sections of y/l. However, τ/τo for 90° groin is found maximum for y/l≤1.5, and for y/l≥2, the velocity is maximum for 45° angled groin.


### 6.3. Velocity and Bed Shear Stress Contour

Figure12 shows the simulated velocity contour in shaded color for case 1, case 2, and case 3, respectively. The results are found to be similar in nature. For all the cases, the velocity contour along the left bank is higher than the right bank at the downstream region of the groin; it indicates the deflection of flow towards right bank and sheltering of flow by groin at east bank. The downstream circulation zone is found to be larger for 45° groin compared to 90° groin; similarly the circulation zone for 90° groin is found to be larger compared to 135° groin.Figure 12
Velocity contoured around a groin for (a) case 1, (b) case 2, and (c) case 3 at the end of simulation by iRIC Nays2DH.
(a)
(b)
(c)In the figure, the flow field is seen to be divided into four distinct regions: (i) the uniform flow at upstream end, (ii) big circulation of low velocity zone at the downstream of the groin created due to sheltering of groin where the velocity is zero in the center of the circulation zone, (iii) a small low velocity zone near the foot at the upstream of groin, and (iv) high velocity zone opposite to the circulation zone created due to the deflected flow. The high velocity zone is found to be decayed towards downstream and the low velocity in circulating zone is found to be regained.Figure13 shows the simulated bed shear stress contour in shaded color for case 1, case 2, and case 3, respectively. The results are found to be similar in nature. Like the velocity contour, for all the cases, the shear stress contour along the left bank is higher than the right bank at the downstream region of the groin. Four distinct flow regions as described in velocity contour are also clearly visible in the contour of shear stress.Figure 13
Bed shear stress contour around a groin for test (a) case 1, (b) case 2, and (c) case 3 at the end of simulation by iRIC Nays2DH.
(a)
(b)
(c)


## 6.1. Predicted Velocity Profiles

Figure10 shows the comparison among predicted velocity profiles (W) for case 1, case 2, and case 3. For each case, the longitudinal velocity profiles are compared at a lateral position of y/l = 1.0, 1.5, 2.0, 3.0, and 4.0. In the figure, all the velocities are normalized by U0 = 0.253 m/s and here x/l = 0 indicates the groin position in the longitudinal direction. The comparisons among the three cases show reasonable differences. Along line y/l=1, the peak of velocities is found at longitudinal distances of x/l = −0.28, 0.0, and 0.56 for case 1, case 2, and case 3, respectively. For y/l=1.0, in all the cases, the velocity is found to be decreased from upstream velocity just before the position of groin head. In other words, in addition to the circulation zone at downstream of groin, a small low velocity zone is observed just upstream of groin at right bank. Along the line y/l=1.5, the peak of velocities is found at longitudinal distances of x/l = −1.0, 0.22, and 0.67 for case 1, case 2, and case 3, respectively. These peak velocities are found to be decayed with the longitudinal distance x/l. For y/l=2, the peaks of velocities are found at a distance of x/l = −0.11, 1.22, and 2.54 for case 1, case 2, and case 3, respectively. For y/l≥2, the decay of velocity along the downstream is found to be slower compared to the regiony/l ≤1.5. Along the line y/l=3, the peak of velocities is found at longitudinal distances of x/l=2.87, 3.53, and 3.88 for case 1, case 2, and case 3, respectively. Along the line y/l=4, the peak of velocities is found at longitudinal distances of x/l = 3.33, 3.89, and 4.44 for case 1, case 2, and case 3, respectively.Figure 10
Comparison between resultant velocity profiles (W) of present study for case 1, case 2, and case 3 along lateral distance, y/l=1, 1.5, 2, 3, and 4.From the figures, it is observed that the peak of velocity is found maximum at the position of head of groin wheny/l=1. However, this position of maximum velocity is found to be shifted towards downstream with increasing y/l. The maximum velocity for case 3 is found lower than the other two cases for all the sections of y/l. However, W/Uo for 90° groin is found maximum for y/l≤2; and for y/l>2, the velocity is maximum for 45° angled groin.


## 6.2. Predicted Bed Shear Stress Profiles

Figure11 shows the predicted bed shear stress profiles (τ) of the proposed model for case 1, case 2, and case 3. For each case, the longitudinal shear stress profiles are compared at a lateral position of y/l = 1.0, 1.5, 2.0, 3.0, and 4.0. In the figure, all the shear stresses are normalized by τo = 0.1293 N/m2, which is the value of upstream region. Here, x/l=0 is the groin position along longitudinal direction. The profiles of bed shear stress are found in similar pattern of velocity profiles. For different values of y/l, the peak of shear stresses is found at the same longitudinal distances (x/l) as reported in velocity profiles. For y/l=1.0, in all the cases, the shear stress is found to be decreased from its upstream value just before the position of groin head.Figure 11
Comparison between computed bed shear stress profiles (τ) of proposed model for case 1, case 2, and case 3 along lateral distance, y/l=1, 1.5, 2, 3, and 4.From the figures, it is observed that the peak of bed shear stress is found maximum at the position of head of groin wheny/l=1. However, this position of maximum bed shear stress is found to be shifted towards downstream with increasing y/l. These peak shear stresses are found to be decayed with the longitudinal distance x/l. However, for y/l≥2, the decay of shear stress along the downstream is found to be slower compared to the region y/l≤1.5. The maximum bed shear stress for case 3 is found lower than the other two cases for all the sections of y/l. However, τ/τo for 90° groin is found maximum for y/l≤1.5, and for y/l≥2, the velocity is maximum for 45° angled groin.


## 6.3. Velocity and Bed Shear Stress Contour

Figure12 shows the simulated velocity contour in shaded color for case 1, case 2, and case 3, respectively. The results are found to be similar in nature. For all the cases, the velocity contour along the left bank is higher than the right bank at the downstream region of the groin; it indicates the deflection of flow towards right bank and sheltering of flow by groin at east bank. The downstream circulation zone is found to be larger for 45° groin compared to 90° groin; similarly the circulation zone for 90° groin is found to be larger compared to 135° groin.Figure 12
Velocity contoured around a groin for (a) case 1, (b) case 2, and (c) case 3 at the end of simulation by iRIC Nays2DH.
(a)
(b)
(c)In the figure, the flow field is seen to be divided into four distinct regions: (i) the uniform flow at upstream end, (ii) big circulation of low velocity zone at the downstream of the groin created due to sheltering of groin where the velocity is zero in the center of the circulation zone, (iii) a small low velocity zone near the foot at the upstream of groin, and (iv) high velocity zone opposite to the circulation zone created due to the deflected flow. The high velocity zone is found to be decayed towards downstream and the low velocity in circulating zone is found to be regained.Figure13 shows the simulated bed shear stress contour in shaded color for case 1, case 2, and case 3, respectively. The results are found to be similar in nature. Like the velocity contour, for all the cases, the shear stress contour along the left bank is higher than the right bank at the downstream region of the groin. Four distinct flow regions as described in velocity contour are also clearly visible in the contour of shear stress.Figure 13
Bed shear stress contour around a groin for test (a) case 1, (b) case 2, and (c) case 3 at the end of simulation by iRIC Nays2DH.
(a)
(b)
(c)


## 7. Conclusions

This simulation has provided us with detailed information regarding the flow pattern, the velocity, and bed shear stress profiles of a groin. This adds to the effort of work done by others on different types of groins. In the simulation, the general flow features around a groin is reproduced successfully. The flow field is found to be divided into four distinct regions: (i) the uniform flow at upstream end, (ii) big circulation of low velocity zone at the downstream of the groin created due to sheltering of groin where the velocity is zero in the center of the circulation zone, (iii) a small low velocity zone near the foot at the upstream of groin, and (iv) high velocity zone opposite to the circulation zone created due to the deflected flow. The high velocity zone is found to be decayed towards downstream and the low velocity in circulating zone is found to be regained.The computed velocity and bed shear stress profiles of present study are compared among case 1, case 2, and case 3. From the simulation, it is observed that the peak of velocity and bed shear stress is found maximum at the position of head of groin when lateral distancey/l=1, where l is the groin length. The position of maximum velocity and bed shear stress is found to be shifted towards downstream with increasing y/l. The maximum velocity and bed shear stress for 135° groin are found lower than the other two cases for all the sections of y/l. W/Uo and τ/τo for 90° groin are found maximum for y/l≤2, and for y/l>2, the velocity and bed shear stress are maximum for 45° angled groin. The downstream circulation zone is found to be larger for 45° groin compared to 90° groin; similarly, the circulation zone for 90° groin is found larger compared to 135° groin.In order to validate the present model, the computed results are compared with previous numerical and experimental results. The comparison between numerical and experimental results showed that except in areas where strong downward flow is observed there are good agreements between experimental and calculated results.



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*Source: 1275498-2017-09-14.xml*