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Flow over broad-crested weir with inflow by approach shaft – numerical model.

Abstract

In the case of flow over rectangular broad-crested weir, where the inflow is realized by approach shaft, occurs influence of water surface level by approach flow velocity. The paper describes numerical model of flow including weir, approach and outlet shaft. Simulations of flow were created by 2D and 3D model with using three methods of turbulent modelling. In paper is evaluated water surface level for each model setup and then is compared with measured values.

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Flow over broad-crested weir with inflow by approach shaft – numerical model.

Author: Major, Jakub; Orfánus, Martin; Zachoval, Zbyněk
Publisher: Faculty of Civil Engineering, Czech Technical University in Prague
Year: 2021
DOI: 10.14311/CEJ.2021.01.0019
Source: https://dspace.vut.cz/bitstreams/f4da6bbb-d858-41f2-b284-3dceca42f82d/download
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FLOW OVER BROAD-CRESTED WEIR WITH INFLOW BY
APPROACH SHAFT – NUMERICAL MODEL
Jakub Majo 1, Ma in O ánus 2 and Zbyněk Zacho al 3
1. AQUATIS a.s., Bo anická 834/56, B no, Czech Republic;
jakub.majo @aqua is.cz
2. Slo ak Uni e si y o Technology in B a isla a, Facul y o Ci il Enginee ing,
Depa men o Hyd aulic Enginee ing, B a isla a, Slo akia;
ma in.o anus@s uba.sk
3. B no Uni e si y o Technology, Facul y o Ci il Enginee ing, Ins i u e o Wa e
s uc u es, B no, Czech Republic; zacho al.z@ ce. u b .cz
ABSTRACT
In he case o low o e ec angula b oad-c es ed wei , whe e he in low is ealized by
app oach sha , occu s in luence o wa e su ace le el by app oach low eloci y. The pape
desc ibes nume ical model o low including wei , app oach and ou le sha . Simula ions o low
we e c ea ed by 2D and 3D model wi h using h ee me hods o u bulen modelling. In his pape a
wa e su ace le el o each model se up is e alua ed and hen i is compa ed wi h measu ed
alues.
KEYWORDS
App oach sha , B oad-c es ed wei , F ee su ace le el, Nume ical model
INTRODUCTION
In p ac ice he e a e also used b oad-c es ed wei s wi h app oach sha o de e mine he
discha ge, e en ual o egula e he wa e su ace le el (labo a o ies, pond inle s uc u es,
was ewa e ea men plan s, wei s o e en ion basins in sewe sys ems, e c.) (Chyba! Nenalezen
zd oj odkazů.).
In he p o essional li e a u e, he low o e he men ioned wei wi h he app oach sha is
desc ibed in he publica ions Chyba! Nenalezen zd oj odkazů., Chyba! Nenalezen zd oj
odkazů. and Chyba! Nenalezen zd oj odkazů., which a e based on ex ensi e expe imen al
esea ch. F om he expe imen al esea ch is known he wa e su ace p o ile in he longi udinal
plane o symme y o he app oach sha and wei , as well as he p essu e heigh on he app oach
sha walls o he ull ange o geome ic dimension a ios used in p ac ice [2], [4]. The wa e
su ace le el in he app oach sha and he eloci y ield in he wake a ea a he wei c es a e
known only o speci ic geome ic and low condi ions [3], [4].
As he au ho s know, a p esen only models o o e low o e b oad-c es ed wei wi h
e ical in low a e pe o med [5], [6], [7], [8] and [9], bu none o he au ho s deal wi h nume ical
modelling o o e low o e b oad-c es ed wei wi h app oach sha .
The aim o he esea ch was c ea ing a sui able nume ical model o he mos eliable
desc ip ion o he low o e ec angula b oad-c es ed wei wi h in low by app oach sha . Model
was alida ed on he basis o measu ed wa e su ace le el p o ile. The esul s o he simula ions
could be used o supplemen he measu ed da a om expe imen al esea ch.
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Fig. 1 – Scheme o low o e b oad-c es ed wei s wi h app oach sha
WEIR GEOMETRY
The wei geome y, app oach sha and ou le sha we e c ea ed in he so wa e FLOW-3D
e sion 11.0.4 [10], in which calcula ions we e also pe o med. Two concep s o model cons uc ion
we e used o e alua e hei ad an ages and disad an ages. The 2D model used he concep o
ixed blocks, which de ined he space o low by wo blocks o he ne wo k (Figu e 2, le ). The
wid h o he ixed blocks was 2 m, he wid h o he blocks o he compu e ne wo k was he same
as he wid h o he wei . The e we e h ee solid blocks. The i s block ( ed in Figu e 2) o med he
opposi e wall o he inle sha wi h espec o he wei . The second block (blue in Figu e 2) o med
a b oad-c es ed wei , an adjacen wall o he inle sha and an adjacen wall o he ou le sha . The
hi d block (yellow in Figu e 2) o med he opposi e wall o he ou le sha . Thei mu ual loca ion
was chosen so ha he nodes o he ne wo k we e in one case a he bounda ies o he
compu a ional a ea and in he o he case we e no . The 3D model used he concep o i e blocks
o a ne wo k o de ine he space h ough which wa e can low (Figu e 2).
The wei had a leng h in he di ec ion o low L = 0.650 m. The side walls o he wei and he
sha we e ele a ed 0.500 m abo e he c es o he wei . The wei , he app oach sha and he
ou le sha we e same wid h b = 0.500 m. The leng h o he app oach sha was l = 0.300 m and i s
heigh was 4 m. In he case o a 3D model due o he educ ion o he numbe o cells, he heigh
was only 2 m. The leng h and heigh o he ou le sha we e he same as o he app oach sha .
The o e low was ee wi h a ully ae a ed nappe in he ou le sha .
SIMULATIONS
To desc ibe he wa e su ace le el a simula ion using a 2D and 3D model o he head
h = 0.253 m (measu ed 0.05 m om he sha wall) a discha ge 0.090 m3/s) was pe o med,
he e o e o a l/h a io o app oxima ely 1.2. Simula ions we e pe o med wi h RANS (Reynolds-
a e aged Na ie -S okes) u bulence models k-ω, k-ε and LES (La ge eddy simula ion). In o ma ion
on indi idual u bulence models can be ound in publica ions [10], [11] and [12], due o hei scope
and gene al knowledge hey a e no gi en he e. S eady low was sol ed wi h a ee wa e su ace,
one incomp essible luid (wa e ) wi h densi y 1000 kg/m3 and kinema ic iscosi y 0,001 m2/s. I was
conside ed wi h a su ace ension 0,073 N/m. The h eshold de ia ion in he calcula ion was se
o 2% [2].
app oach sha
l
h
wei
Q
ou le sha
L
z
x
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The coo dina e sys em has been chosen so ha x coo dina e de ined he leng h o he sha
and c es o wei in he low di ec ion, he y coo dina e de ined he wid h o he sha and he wei
and he z di ec ion he heigh o he sha .
Bounda y condi ions o se e al ypes a e desc ibed in Figu e 2. The bounda y condi ion a
he in low (bo om o he app oach sha ) o 2D simula ion was en e ed as he in low eloci y (V)
co esponding o he speci ic discha ge o he gi en s a e. The bounda y condi ion a he in low o
he 3D simula ion was en e ed as a p essu e (P). The ad an age o en e ing he eloci y is he
di ec calcula ion, he disad an age is ela i ely uns able solu ion. The ad an age o en e ing he
p essu e is a s able solu ion, he disad an age is he indi ec (i e a i e) calcula ion. The wall
bounda y condi ion (W) wi h a hyd aulically smoo h su ace was speci ied on all solid walls. The
symme ic bounda y condi ion (S) was speci ied a he junc ion o he ne wo k blocks. The ee
ou low (O) was en e ed a he ou low sec ion o he ou le sha and a he ai bounda ies (Figu e
2). The ini ial condi ion was he hyd os a ic p essu e dis ibu ion along he heigh o he calcula ion
space om he measu ed wa e le el. The ini ial wa e le el was en e ed as a ho izon al le el o e
he wei c es .
Fig. 2 – Scheme o calcula ion a ea and en e ing bounda y condi ions o 2D model (le ) and o
3D model ( igh )
Du ing he calcula ions, h ee analyses we e pe o med o de e mine he minimum
equi emen s o he models so ha he esul s we e conclusi ely and epea able.
The i s analysis conce ned he in luence o he posi ion o he s uc u ed ec angula mesh
agains he solid walls, when i was shown ha he mu ual posi ion in luences he esul s. The
e ec on he wa e su ace le el was up o 0.004 m, he change was mainly e lec ed in he eloci y
ield nea he walls. Fo easons o epea abili y, a posi ion was chosen whe e he nodes o he
ne wo k co esponded o he su ace o he solid wall.
The second analysis conce ned he e ec o cell size on he esul s. A 2D model wi h a k-ω
u bulence model was used o he analysis. The leng h o he cell edges in he calcula ion a ea
was g adually educed un il he wa e le el did no change by mo e han 0.001 m. This s a e
occu ed a a cell size leng h (in he x and z di ec ion) o 0.005 m in he whole calcula ion a ea. In
he y di ec ion, he size o he cells in he 3D model was se o 0.010 m o e he whole wid h o he
a ea. Guidelines o good mesh quali y speci ied by FLOW-3D was sa is ied. The maximum aspec
z
x
y
z
x
y
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a io wi hin a single cell was less han 3, he maximum adjacen cell size a io was less han 1.25,
he maximum in e -block cell size a io was less han 2, and mesh planes coincide in he
bounda ies.
The hi d analysis conce ned he minimum equi ed sha heigh . A 2D model was used o
he analysis, whe e he de elopmen o he eloci y ield and he in luence o he sha leng h on
he wa e su ace le el we e moni o ed. I u ned ou ha he heigh o he app oach sha 2 m
below he wei c es was su icien due o achie e a cons an eloci y dis ibu ion along he sha
heigh . I was also de e mined ha he heigh o he ou le sha 0.100 m below he wei c es will
su ice, when he posi ion o he ne wo k bounda y does no a ec he wa e su ace le el abo e
he wei .
The o al numbe o cells in he 2D model was 183 911, o which 46 366 we e ac i e. In he
3D model, he o al numbe o cells was 4 114 141, all cells we e ac i e. The s abiliza ion ime was
de e mined based on he change in wa e su ace le el o e ime. The c i e ion was a change o
wa e su ace le el smalle han 0.001 m du ing 10 s. Flow was s abilized in 20 s a he la es .
A s anda d desk op compu e was used o he calcula ions (In el i7, 4 co es, 4,6 GHz, 8 GB RAM).
The calcula ion ime las ed in he case o a 2D model in he ange o 3 o 4 hou s, in he case o
a 3D model 1 o 2 days, depending on he o e low heigh .
EVALUATION AND COMPARISON
Wa e le els in he longi udinal plane o symme y o 2D and 3D models and wa e le els in
he en i e app oach sha we e e alua ed using RANS u bulence models k-ω, k-ε and he LES
model. The e alua ion was pe o med in MS Excel. The alues we e hen compa ed wi h he
measu ed alues [3]. In summa y, he expe imen al model has he leng h o he wei 0.650 m,
wid hs o he wei as well as he sha b = 0.500 m, and heigh o he sha 4.02 m. Discha ge was
0.090 m3/s. The b oad-c es ed wei and he igh downs eam wall o he wei we e made om
polyme hyl me hac yla e wi h a hickness o 0.010 m. The le downs eam wall was made o
wa e p oo plywood wi h a hickness o 0.021 m. Wa e su ace was measu ed by he poin gauge
and discha ge by he elec omagne ic lowme e . F ee o e low was achie ed. The space
unde nea h he nappe was ully ae a ed.
Figu e 3 shows measu ed and calcula ed (2D and 3D) wa e su ace longi udinal p o ile
( u bulence model k-ω). Figu e 4 shows measu ed wa e su ace longi udinal p o ile and calcula ed
(3D model) by RANS u bulence models k-ω, k-ε and he LES model.
F om he compa ison o calcula ed and measu ed wa e su ace p o iles shown in Figu e 3
and Figu e 4 is isible he quan i a i e di e ence. All nume ical models unde es ima e he wa e
su ace le el. The di e ence be ween he calcula ed and measu ed alues is up o −0,016 m. F om
Figu e 3, he wa e su ace p o ile in he 3D model is quali a i ely simila o he measu ed. F om
he abo e, he low simula ion using a 3D model be e cap u es measu ed wa e su ace han
using a 2D model, which is due o he inclusion o ic ion agains he side walls in 3D model. F om
Figu e 4 i is isible ha he k-ω model desc ibes wa e su ace p o ile he mos accu a ely.
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Fig. 3 – Longi udinal wa e su ace p o ile, u bulence model k-ω, in luence o model dimension
Fig. 4 – Longi udinal wa e su ace p o ile, 3D model, in luence o u bulence model
Figu e 5 shows he ela i e e o o he calcula ed wa e su ace le el p o iles o he
indi idual u bulence models, whe e hM is measu ed wa e su ace le el and hV is calcula ed o he
indi idual models.
F om Figu e 5 i is isible ha o x < 0.15 m he u bulence models show a ela i e e o up
o 10%, in he ange 0.15  x  0.65 up o 18 %.
0.05
0.10
0.15
0.20
0.25
0.30
-0.30 -0.20 -0.10 0.00 0.10 0.20 0.30 0.40 0.50 0.60 0.70
z[m]
x[m]
2D
3D
measu ed
0.05
0.10
0.15
0.20
0.25
0.30
-0.30 -0.20 -0.10 0.00 0.10 0.20 0.30 0.40 0.50 0.60 0.70
z[m]
x[m]
k-w
k-e
LES
measu ed
k-
e
LES
k-
w

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Fig. 5 - Rela i e e o o he calcula ed wa e su ace p o iles o indi idual models
The wa e su ace le els in he whole app oach sha calcula ed by 2D and 3D model we e
e alua ed in he p og am SMS 12.3. Figu e 6 shows he isolines o he wa e su ace le el ( ela i e
o he wei c es le el) calcula ed by 2D and 3D model using he k-
w
model o u bulence and
isolines om he measu ed alues (linea in e pola ion on a iangula mesh) Chyba! Nenalezen
zd oj odkazů..
Fig. 6 - Wa e su ace le el abo e wei c es [m] in he app oach sha , le – 2D model, middle –
3D model and igh – measu ed, he igh bounda y o he a ea de ines he ups eam edge o he
wei c es
-0.20
-0.15
-0.10
-0.05
0.00-0.3 -0.2 -0.1 0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7
(hV-hM)/hM[-]
x[m]
k-w
k-e
LES
k-
w
k-
e
LES
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Fig. 7 – De ia ion [%] o compu ed alues o wa e su ace le el abo e he wei c es in he
app oach sha om measu ed alues, le – 2D model, igh – 3D model, he igh bounda y o he
a ea de ines he ups eam edge o he wei c es
In Figu e 6 he e a e isible di e ences in he wa e su ace le els o he calcula ed 2D and
3D models compa ed o he measu ed. In he Figu e 7 he e is isible he de ia ion o he
compu ed alues o he wa e su ace le el abo e he wei c es in he app oach sha om
measu ed alues.
In he case o 2D model, he wa e su ace le el is cons an ac oss he en i e wid h o he
in low sha . The wa e le el does no co espond quan i a i ely and quali a i ely o he measu ed
wa e le el. The gi en shape is simila o he condi ions a lowe o e low heigh s o la ge leng hs
o he app oach sha [2]. The di e ence be ween he calcula ed and measu ed wa e su ace le el
is up o −0.033 m (de ia ion −12 %). The la ges de ia ions a e a he ups eam edge o he wei
c es . In he case o 3D model, he esul s a e quan i a i ely di e en , bu quali a i ely mo e
simila o hose measu ed. Nea he app oach sha walls, he wa e su ace le el is lowe , in he
middle o he sha i is highe . The di e ence is up o 0.006 m. The di e ence be ween he
calcula ed and measu ed wa e su ace le el is up o −0.030 m (de ia ion −11 %). The la ges
de ia ions a e a he ups eam edge o he wei c es .
CONCLUSION
The nume ical models in he case o low o e a b oad-c es ed wei wi h app oach sha
made i possible o de e mine he low cha ac e is ics ela i ely quickly. The use o solid blocks in
modelling allows o quick model c ea ion, bu a he cos o la ge numbe o inac i e cells and
equen non-ma ching o he su ace wi h he cell edges. Modelling wi hou hei use seems o be
mo e sui able in e ms o accu acy and complexi y o calcula ion. I is necessa y o obse e a
su icien heigh o he app oach and ou le sha s so ha he in luence o he inpu o bounda y
condi ions, he size and posi ion o he cells and su icien simula ion ime o s abilize he low do
no show.
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Quali a i e ag eemen o he calcula ed wa e su ace le el p o ile by 2D and 3D models
wi h RANS u bulence models k-ω, k-ε and LES model is ela i ely good, bu quan i a i e
ag eemen is insu icien . The wa e su ace le el calcula ed by nume ical models in he sec ion o
he app oach sha and in he sec ion o wei c es is signi ican ly unde es ima ed in he whole
longi udinal plane o symme y agains o he measu ed. The ela i e e o o he wa e su ace
le el abo e he app oach sha is up o 10% and abo e he wei c es up o 18%. The RANS
models calcula e he wa e su ace le el p o ile mo e accu a ely han he LES model. Simula ion
using a 3D model gi es a quali a i ely be e in o ma ion abou he wa e su ace le el in he
app oach sha han he 2D model. The calcula ed wa e su ace p o iles using he RANS
u bulence models k-ω and k-ε a e e y simila .
ACKGNOWLEDGEMENT
The a icle was c ea ed wi h he suppo o he p ojec FAST-J-17-4577. In luence o he
app oach sha geome y on he capaci y o b oad-c es ed wei and p ojec FAST-S-18-5084 Flow
wi h wakes in cons uc ions.
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