Prediction of Flow Dynamic Features forRiver...
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IOSR Journal of Engineering (IOSRJEN) www.iosrjen.org
ISSN (e): 2250-3021, ISSN (p): 2278-8719
Vol. 10, Issue 3, March 2020, ||Series -I|| PP 47-58
International organization of Scientific Research 47 | Page
Prediction of Flow Dynamic Features forRiver NileConfluence
Zone
Gamal El Saeed1, Neveen Badway
2, Hossam Elsersawy
3, Fatma Samir
4
1Professor of Hydraulics and Water Resources, Faculty of Engineering, Shobra, Benha University.
2Associate Professor, Faculty of Engineering, Shobra, Benha University.
3Associate Professor, Nile Research Institute, National Water Research Center.
4ResearcherAssistant, Nile Research Institute, National Water Research Center.
Received 26 February 2020; Accepted 09 March 2020
Abstract A confluence is a natural component in river and channel networks. The incoming flow from the tributary
channel causes extensive variation of the flow velocity, flow discharge, turbulent intensity and sediment
discharge in the main-channel. In the present paper, numerical model is applied to predict flow pattern and
morphological changes at the future. The numerical model was calibrated using available confluence field data
and then was applied to a confluence. The objectives of this study are to: evaluate the morphological changes at
channel confluence, showing the behavior of the planform confluence morpho-hydro dynamics zones at the
future, presenting the cumulative erosion and sediment at the study confluence and the rate of changes for the
confluence hydrodynamic zone (CHZ) stagnation zone, separation zone, confluence scour, region of maximum
velocity, region of flow recovery, and mixing interface/shear layer. Key Words Confluence, Hydro-dynamic Features, Nile River,Numerical Modeland Prediction.
I. INTRODUCTION River confluences play a major role in the routing of flow and sediment through fluvial systems. The
hydrodynamic zone (CHZ) divided the flow into six zones and denoted them as follows: (i) a stagnation zone
where flow velocity is reduced near the upstream junction corner; (ii) a flow separation zone at the downstream
junction corner; (iii) a confluence scour; (iv) the maximum velocity/flow acceleration zone of the downstream
channel; (v) flow recovery at the downstream end of the CHZ. and (vi) a shear layer/mixing interface between
the two confluent flows. The key factors controlling the bed morphology, sediment transport, and flow pattern
of the CHZ at simple confluences include planform symmetry, junction angle, momentum flux ratio, and bed
concordance [Rhoads and Johnson, 2018].
Over the last 30 years, both laboratory and field experiments have provided valuable information on
the morphology and flow dynamics of river junctions [Mosley, 1976; Ashmore, 1982; Reid et al.,1989; Best,
1987, 1988; Best and Roy, 1991; Biron et al., 1993a, 1993b; Gaudet and Roy, 1995; Biron et al., 1996a, 1996b;
McLelland et al., 1996; De Serres et al., 1999; Rhoads and Kenworthy, 1995, 1998; Rhoads and Sukhodolov,
2001, 2004; Sukhodolov and Rhoads, 2001]. However, very few studies have examined sediment transport at
those sites [Best, 1987, 1988]. Furthermore, the relation between sediment transport and the dynamics of the
shear layer created at the interface between the two combining flows has not been described. Shear layers are
characterized by high turbulence intensities and shear stresses and by the presence of well-organized flow
structures [Winant and Brownand, 1974; Lee and Clark, 1980; Hussain and Zaman, 1985; Nezu and Nakagawa,
1993; Biron et al., 1996b; McLelland et al., 1996; De Serres et al., 1999; Sukhodolov and Rhoads, 2001; Rhoads
and Sukhodolov, 2004]. The complexity of the flow in this zone has, however, generated many questions
concerning the type and scale of the turbulent structures within this region and the processes responsible for
their creation and dissipation [Best and Roy, 1991; Biron et al., 1993b; Rhoads and Sukhodolov, 2001, 2004].
Critically, this turbulence intensity may play an important role in the transport of sediment.
The principal objectives of the present study are:evaluate the morphological changes at channel
confluence, showing the behavior of the planform confluence morpho-hydro dynamics zones at the future,
presenting the cumulative erosion and sediment at the study confluence and the rate of changes for the
hydrodynamic zones.
II. MATERIAL AND METHODS 2.1 Methodology
The methodology of this paper is:Review the literature and collecting the available field data such as bed levels
flow velocity, properties of the bed particles and the passing discharge at the selected confluence. Collect the
Prediction of Flow Dynamic Features forRiver NileConfluence Zone
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field data including surveying the water surface profile and morphological changes due to different discharge
conditions along the entire reach. Applying numerical model (Delft-3D) to get the hydraulic properties at the
selected confluence at this time and future.The model is utilized to predict naturally morphological changes,
including hydrodynamic features, to estimate the forces that influence the entrainment and deposition of
individual particles.
2.2 Study area
Anasymmetrical confluence at km 27 from El Roda gauge, near El Marzeek bridge was used for this
study. This is an asymmetrical confluence, channelized confluence with a junction angle of 25°, momentum flux
ratio 0.4 at maximum flow, and upstream channel widths (mean and tributary) of approximately 223m and
124m respectively, merging into a downstream channel of width 363m, at year 2016.There is bridge at 750m
downstream the confluence (figure 1).
Figure 1: The study confluence and its location
2.2.1 Data collection
The bathymetric data were obtained from the contour maps,produced from the hydrographic survey of
year 2016 provided by Nile Research Institute (NRI).Field measurements were conducted on a series of cross
sections at the confluence in July 2019. Data were obtained from hydrodynamic measurements and bathymetric
surveys by using Doppler current profiler (ADCP), the measured cross sections location shown at figure 2.
The hydrological data presents water level and flow rate downstream Assuit Barrage.The daily monitoring of
passing discharges through the located hydraulic structures (barrages) and the upstream and downstream
corresponding water levels of those barrages as well as at different gauge stations is essential. Concerning study
reach, two-gauge stations are located as shown in table 1.
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Figure 2: ADCP data points along the study reach during the field measurements at year 2019
Table 1:Location of water level measuring stations
Km from Gauge
Gauge El Roda OAD
El Roda 0 927
Al Lathy 53.3 873.7
III. MODELAPPLICATION 2.2.2 Model description
A detailed numerical morphological model was setup using the numerical software package Delft-3D,
which was developed by Deltares for multi-approaches; where it can carry out simulations of flows, sediment
transports, waves, water quality, particle tracking, morphological developments and ecology, DELTARES
(2014a). The primary purpose of the computational model Delft3D is to solve various one-, two- and three-
dimensional, time-dependent, non-linear differential equations related to hydrostatic and non-hydrostatic free-
surface flow problems.Delft3D-FLOW solves the Navies Stokes equations for an incompressible fluid, under the
shallow water and the Boussinesq assumptions. In the vertical momentum equation, the vertical accelerations
are neglected, which leads to the hydrostatic pressure equation.
For reliable hydrodynamic computations the grid should fulfill the requirements of smoothness,
orthogonality, and should have an aspect ratio close to unity (see Thompson et al., 1985; Wijbenga, 1985; and
Mosselman, 1991). A fine unstructured grid (5 m*5 m) consisting of 145587 nodes was created.
2.2.3 Boundary Condition
The model was calibrated from year 2016 to year 2019. To predict the hydrodynamic features the model was run
as a time series of the last ten years from year 2019 to year 2029. Figures 4&5 show the time series (discharge
and corresponding water level) used for calibrate the model and time series from year 2019 to 2029 used to
prediction case.Survey of year 2016 is used.
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Figure 4: The used water level from year 2016 to year 2029 at the study confluence
Figure 5: The corresponding discharge from year 2016 to year 2029 at the Assuit barrage
2.2.4 Model calibration
The model was run from year 2016 to 2019 and the results were compared with measured field data at year 2019
(with discharges of 1930 m3/s and corresponding water level 18.80 m), on average velocity, and bed elevation.
The model output showed that the simulation of water levels and bed elevation was highly accurate as shown at
figures 6 and 7. Manning roughness coefficient (n) was defined at each grid point, and ranged from 0.025 to
0.035. The morphology of the fractions was computed using the “Meyer-Peter-Muller (1948)”sediment
transport predictor formula.
17.20
17.60
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/20
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wat
er L
evel
(m
)
Date
Prediction TimeCalibration Time
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Dis
char
ge
(m3
/s)
Date
Prediction TimeCalibration Time
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Figure 6: Comparison of measured and predicted bed elevations at year 2019 and the cross sections
location
8.00
10.00
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0 100 200 300 400 500 600 700 800
Bed
Ele
vat
ion (
m)
Distance from Upstream (m)
Cross Section 1
Field Model
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200 300 400 500 600 700
Bed
Ele
vat
ion (
m)
Distance from Upstream (m)
Cross Section 3
Field Model
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0 100 200 300 400 500 600 700
Bed
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ion (
m)
Distance from Upstream (m)
Cross Section 5
Field Model
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0 100 200 300 400 500 600 700 800
Vel
oci
ty (
m/s
ec)
Distance (m)
Cross Section 2
Field Model
Prediction of Flow Dynamic Features forRiver NileConfluence Zone
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Figure 7: Comparison of measured and predicted depth average velocity at year 2019 and the cross
sections location
IV. RESULTS AND ANALYSIS 2.2.5 Confluence morphological changes
The modelwas utilized to predict naturallymorphological changes, including hydrodynamic features.
Figure 8 shows the reach bed elevation at years 2016 and 2029, one cross section upstream and eight cross
sections downstream the confluence. At the upstream cross section, the bed elevation will be deposed about 2 m
at the main and tributary channel and the river bed discordance will change from 2.5m at year 2016 to 2m at
year 2029. It is also clear from the figure that at year 2029 the reach will be recovered at section eight as same
as year 2016. There is some different at bed elevation from years 2016 and 2029. At year 2029 the reach will be
deposed at the east bank from section four to section seven about 1 to 2 m, however at section four to section
eight will be eroded at the west bank about 1m. It’s obvious that the separation zone decreases from year 2016
to 2029.
0.00
0.20
0.40
0.60
0.80
1.00
1.20
0 100 200 300 400 500 600 700 800
Vel
oci
ty (
m/s
ec)
Distance (m)
Cross Section 4
Field Model
0.00
0.20
0.40
0.60
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0 100 200 300 400 500 600 700 800
Vel
oci
ty (
m/s
ec)
Distance (m)
Cross Section 6
Field Model
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0 100 200 300 400 500 600 700 800
EL
EV
AT
ION
(m
)
DISTANCE (m)
Upstream Confluence Cross Section
2016 2029
8.00
10.00
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18.00
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0 100 200 300 400 500 600 700 800
EL
EV
AT
ION
(m
)
DISTANCE (m)
Cross Section No.(1)
2016 2029
8.00
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0 100 200 300 400 500 600 700 800
EL
EV
AT
ION
(m
)
DISTANCE (m)
Cross Section No.(2)
2016 2029
Prediction of Flow Dynamic Features forRiver NileConfluence Zone
International organization of Scientific Research 53 | Page
Figure 8:Morphological changes in bed morphology from year 2016 to year 2029
2.2.6 Sedimentation and Erosion Pattern
Figure 9 shows the cumulative erosion and sediment from year 2016 to year 2029. It can be observed that the
island will be deposedtowards the main channel by rate0.15 m/year.
8.00
10.00
12.00
14.00
16.00
18.00
20.00
22.00
0 100 200 300 400 500 600 700 800
EL
EV
AT
ION
(m
)
DISTANCE (m)
Cross Section No.(3)
2016 2029
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0 100 200 300 400 500 600 700 800
EL
EV
AT
ION
(m
)
DISTANCE (m)
Cross Section No.(4)
2016 2029
8.00
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14.00
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18.00
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0 100 200 300 400 500 600 700 800
EL
EV
AT
ION
(m
)
DISTANCE (m)
Cross Section No.(5)
2016 2029
8.00
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0 100 200 300 400 500 600 700 800
EL
EV
AT
ION
(m
)
DISTANCE (m)
Cross Section No.(6)
2016 2029
8.00
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0 100 200 300 400 500 600 700 800
EL
EV
AT
ION
(m
)
DISTANCE (m)
Cross Section No.(7)
2016 2029
8.00
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16.00
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0 100 200 300 400 500 600 700 800
EL
EV
AT
ION
(m
)
DISTANCE (m)
Cross Section No.(8)
2016 2029
Prediction of Flow Dynamic Features forRiver NileConfluence Zone
International organization of Scientific Research 54 | Page
Figure 9: Cumulative erosion and sediment from year 2016 to year 2029
The bed shear stress was estimated for the wholereach at years 2016 & 2029 for maximum flow, figure
10. From the figure it is noticed that the bed shear stressstarted from the main channel. At year 2016 the bed
shear stress reached to 5.5 N/m2 while at year 2019 it reached to 4.5 N/m
2. It is noticed also that the value of
shear stress reduced at year 2029 compared with year 2016.
From the previous part, it means that without human interference the reach will be safer to the bridge in the
future from the local scour.
Figure 10: Bed shear stress of maximum flow at years 2016&2029
2.2.7 Hydro-dynamic zones
The hydrodynamic zones at years 2016 and the predicted year 2029 presented at figure 11. From the figure there
is changes at the zones would be presented as follows:
Zone no. 1: the stagnation zone will be expanded toward the east side (main channel) subsequently,
the confluence angle will be decreased from 25° to 15°.
Zone no. 2: the separation zone will be decrease at year 2029 consequenceof the change at the
direction of the stagnation zone. The east bank will be deposed about 3 m compared with the bed elevation at
year 2016.
x coordinate
y c
oord
inate
642.6 642.8 643 643.2 643.4
786
786.5
787
787.5
788
788.5
cum
. ero
sio
n/s
edim
enta
tion (
m)
-2
-1.5
-1
-0.5
0
0.5
1
1.5
2
x coordinate (km)
y c
oord
inate
(km
)
642.6 642.8 643 643.2 643.4
786
786.5
787
787.5
788
788.5
Bed s
hear
str
ess o
f year_
2016,
magnitude (
N/m
2)
0
0.5
1
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2
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4
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5.5
x coordinate (km)
y c
oord
inate
(km
)
642.6 642.8 643 643.2 643.4
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788.5
Bed s
hear
str
ess o
f year_
2029,
magnitude (
N/m
2)
0
0.5
1
1.5
2
2.5
3
3.5
4
4.5
5
5.5
Prediction of Flow Dynamic Features forRiver NileConfluence Zone
International organization of Scientific Research 55 | Page
Zone no. 3: the location of the scour zone changes from just downstream the confluence at year 2016
to be direct upstream the bridge at about 400 m from the confluence at year 2029.
Zone no. 4: the maximum velocity changes at value and location from year 2016 to 2029. The value
will be increase and located downstream the bridge.
Zone no. 5: the flow will be recovered earlier at year 2029 compared with year 2016.
Zone no. 6: the mixing shear layer at year 2029 will be deflected toward the east bank (main channel)
and it will be end earlier than year 2016.
Features 2016 2029
Sta
gn
ati
on
& S
epa
rati
on
zon
e
Co
nfl
uen
ce s
cou
r
x coordinate (km)
y c
oord
inate
(km
)
642.6 642.8 643 643.2 643.4
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bed level in
wate
r le
vel poin
ts (
m)
14
14.55
15.09
15.64
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17.82
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18.91
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x coordinate (km)
y c
oord
inate
(km
)
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bed level in
wate
r le
vel poin
ts (
m)
14
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15.64
16.18
16.73
17.27
17.82
18.36
18.91
19.45
x coordinate (km)
y c
oord
inate
(km
)
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bed level in
wate
r le
vel poin
ts (
m)
10
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10.73
10.82
10.91
x coordinate (km)
y c
oord
inate
(km
)
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787.8
bed level in
wate
r le
vel poin
ts (
m)
10
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10.64
10.73
10.82
10.91
Prediction of Flow Dynamic Features forRiver NileConfluence Zone
International organization of Scientific Research 56 | Page
Reg
ion
of
ma
xim
um
vel
oci
ty
Reg
ion
of
flo
w r
eco
ver
y
Mix
ing
in
terf
ace
/sh
ear
lay
er
Figure 11: The hydro dynamic features at the confluence zone at year 2016 and 2029
x coordinate (km)
y c
oord
inate
(km
)
642.6 642.8 643 643.2 643.4
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786.2
786.4
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787.8
depth
avera
ged v
elo
city,
magnitude (
m/s
)
0.8
0.8182
0.8364
0.8545
0.8727
0.8909
0.9091
0.9273
0.9455
0.9636
0.9818
x coordinate (km)
y c
oord
inate
(km
)
642.6 642.8 643 643.2 643.4
786
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786.4
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depth
avera
ged v
elo
city,
magnitude (
m/s
)
0.8
0.8182
0.8364
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0.8727
0.8909
0.9091
0.9273
0.9455
0.9636
0.9818
x coordinate (km)
y c
oord
inate
(km
)
642.6 642.8 643 643.2 643.4
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788.5
bed level in
wate
r le
vel poin
ts (
m)
8
9.091
10.18
11.27
12.36
13.45
14.55
15.64
16.73
17.82
18.91
x coordinate (km)
y c
oord
inate
(km
)
642.6 642.8 643 643.2 643.4
786
786.5
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788.5
bed level in
wate
r le
vel poin
ts (
m)
8
9.091
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13.45
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17.82
18.91
x coordinate (km)
y c
oord
inate
(km
)
642.6 642.8 643 643.2 643.4
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vert
ical eddy v
iscosity (
m2/s
)
0
0.005
0.01
0.015
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0.045
0.05
x coordinate (km)
y c
oord
inate
(km
)
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vert
ical eddy v
iscosity (
m2/s
)
0
0.005
0.01
0.015
0.02
0.025
0.03
0.035
0.04
0.045
0.05
Prediction of Flow Dynamic Features forRiver NileConfluence Zone
International organization of Scientific Research 57 | Page
2.2.8 The rate of changes at CHZ
Table 2 and figure 12 presented the changes of distance, value and length of the hydrodynamic zones at year
2016 and the predicted year 2029. The figure shows also the map of key hydrodynamic features observed at
years 2016 and 2029.
It can observe that the stagnation zone will be deposed by rate 18.7 m/year, the separation zone length will be
expanded about 12.5 m/year while the separation index value will be decreased and the confluence scour will be
deposed about 0.08 m/year.
Table 2:Comparing between the hydrodynamic features proports at years 2019 and 2029
Features Magnitude Location(m) Length (m)
2016 2029 2016 2029 2016 2029
Stagnation Zone - - - - - 244
Separation Index 0.13 0.095 - - 1890 2057
Confluence Scour 9.88 m 10.91 m 218 411 - -
Maximum Velocity 0.99 m/s 1.10 m/s 721 640 - -
Flow Recovery - - 1488 1226 - -
Shear Layer - - - - 869 387
Where: location= the distance downstream the confluence, Separation index = H/L, where H is maximum
separation zone width and L is separation zone length; (Best 1984).
Figure 12: Comparing between the zones proports at years 2019 and 2029
V. CONCLUSIONS The numerical model is applied to predict flow pattern and morphological changes at the future.The
results showthe hydro-morpho-sedimentary processes occurring in confluence zone. With a morphological scale
factor, the bed-form change of the study confluence is predicted.Interaction between flow dynamics and bed
morphology was observed.
The results show that at the future without any human interference, the stagnation zone will be
expanded toward the east side, the separation zone will be decrease, the location of the scour zone changes, the
(5)(5)
(4)
(1)
(6)
2016(1)
(2)
(3)
2029
(3)(4)
(2) (6)
218
721
1488
411
640
1226
0
200
400
600
800
1000
1200
1400
1600
Confluence ScourMaximum VelocityFlow Recovery
Dis
tance
(m
)
Distance
2016
2029
0.13
9.88
0.990.095
10.91
1.1
0
2
4
6
8
10
12
Separation IndexConfluence ScourMaximum Velocity
Val
ue
(m)
Value
2016
2029
1890
869
244
2057
387
0
500
1000
1500
2000
2500
Stagnation ZoneSeparation IndexShear Layer
Len
gth
(m
)
Length
2016
2029
Prediction of Flow Dynamic Features forRiver NileConfluence Zone
International organization of Scientific Research 58 | Page
maximum velocity changes at value and location, the flow will be recovered earlier, the mixing shear stress will
be ended earlierthe erosion and deposition migrate in both directions. So, the results show that the confluence
zone will be changes compared with the present time. The different erosion patterns are related to net deflection
of flow toward the east bank (main channel) and the consequent acceleration. The spatial distribution of the bed
sediments exhibited segregation between the sediments provided by the tributary and main channel.
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