12
Numerical Modelling of a Run-of-River Tailrace Canal V. Hasmatuchi HES-SO Valais//Wallis School of Engineering Route du Rawyl 47 CH-1950 Sion Switzerland F. Avellan EPFL Laboratory for Hydraulic Machines Av. de Cour 33bis CH-1007 Lausanne Switzerland C. Münch HES-SO Valais//Wallis School of Engineering Route du Rawyl 47 CH-1950 Sion Switzerland Abstract Free-surface flow numerical simulations in the tailrace canal of the Swiss Lavey run-of-river hydro powerplant and flow measurements are performed to investigate its isokinetic potential with the aim of installing new technologies to recover the energy of rivers and artificial channels. The canal is supplied by the draft tubes of three Kaplan turbines through the tailrace tunnels. Two different inlet operating conditions are addressed: nominal discharge at the three tailrace tunnels and, respectively, zero discharge at the first with nominal discharge at the second and the third tailrace tunnels. Numerical simulations are performed using the commercial code ANSYS CFX 14.5.7, solving the incompressible unsteady Reynolds-Averaged Navier-Stokes equations. The computational domain includes the full tailrace canal water passage from the inlet tunnels to the junction with the Rhône River. The results are validated with measured axial velocity profiles on 3 different cross sections and the water surface level at the inlet of the canal. The water surface level at the outlet of the canal is used as boundary condition. Then, the analysis is mainly focused on the flow configuration for the two different canal flow discharge. It is found that, depending on the number of turbines that operate at time, the flow configuration in the tailrace canal may vary a lot. These results are crucial for the selection of an optimal implantation location of an isokinetic turbine in order to recover a maximum of energy over the whole year for any operating condition. Keywords: run-of-river tailrace canal, free-surface flow, numerical modelling, experimental validation Nomenclature C x [m/s] Axial velocity Re [-] Reynolds number |C yz | [m/s] Magnitude of cross velocity S [m 2 ] Surface d t [s] Time step St [-] Strouhal number D h [m] Equivalent hydraulic diameter T [s] Time period f [Hz] Frequency x, y, z [m] Cartesian coordinates Fr [-] Froude number y + [-] Dimensionless sublayer-scale distance g [m·s -2 ] Gravity ε [m 2 ·s -3 ] Turbulent dissipation rate h [m] Water depth ε Q [%] Inlet to outlet relative discharge error k [m 2 ·s -2 ] Turbulent kinetic energy ʋ [m 2 ·s -1 ] Kinematic viscosity k t [%] Time coefficient ߩ[kg·m -3 ] Water density l [m] Canal bottom width ω [s -1 ] Specific dissipation rate L [m] Canal length p [Pa] Static pressure Superscripts P [m] Perimeter ¯ Average value Q [m 3 ·s -1 ] Discharge * Dimensionless value Q n [m 3 ·s -1 ] Nominal discharge Introduction Scheduled progressive shut-down of the Switzerland’s nuclear power plants requires the installation of new energy production units (Munch & Avellan [1]). In this context, alternative renewable energy sources must be reconsidered, including the unexploited small-hydro potential sites. The present work is related to the potential of the hydrokinetic energy of rivers and artificial channels. In the framework of the Hydro VS research project, the development of a new isokinetic turbine to recover the energy lost in rivers is conducted. The design and the optimization of the turbine are realized using numerical tools. The objective is the installation and testing of a prototype by the end of the year 2015. This study is mainly motivated by the need of knowing the full flow field in the pilot site, necessary for the development and, later, for the control of the prototype and the final products.

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Numerical Modelling of a Run-of-River Tailrace Canal

V. Hasmatuchi HES-SO Valais//Wallis School of Engineering Route du Rawyl 47 CH-1950 Sion Switzerland

F. Avellan EPFL Laboratory for Hydraulic Machines Av. de Cour 33bis CH-1007 Lausanne Switzerland

C. Münch HES-SO Valais//WallisSchool of Engineering Route du Rawyl 47 CH-1950 Sion Switzerland

Abstract Free-surface flow numerical simulations in the tailrace canal of the Swiss Lavey run-of-river hydro powerplant and flow measurements are performed to investigate its isokinetic potential with the aim of installing new technologies to recover the energy of rivers and artificial channels. The canal is supplied by the draft tubes of three Kaplan turbines through the tailrace tunnels. Two different inlet operating conditions are addressed: nominal discharge at the three tailrace tunnels and, respectively, zero discharge at the first with nominal discharge at the second and the third tailrace tunnels. Numerical simulations are performed using the commercial code ANSYS CFX 14.5.7, solving the incompressible unsteady Reynolds-Averaged Navier-Stokes equations. The computational domain includes the full tailrace canal water passage from the inlet tunnels to the junction with the Rhône River. The results are validated with measured axial velocity profiles on 3 different cross sections and the water surface level at the inlet of the canal. The water surface level at the outlet of the canal is used as boundary condition. Then, the analysis is mainly focused on the flow configuration for the two different canal flow discharge. It is found that, depending on the number of turbines that operate at time, the flow configuration in the tailrace canal may vary a lot. These results are crucial for the selection of an optimal implantation location of an isokinetic turbine in order to recover a maximum of energy over the whole year for any operating condition.

Keywords: run-of-river tailrace canal, free-surface flow, numerical modelling, experimental validation

Nomenclature Cx [m/s] Axial velocity Re [-] Reynolds number |Cyz| [m/s] Magnitude of cross velocity S [m2] Surface dt [s] Time step St [-] Strouhal number Dh [m] Equivalent hydraulic diameter T [s] Time period f [Hz] Frequency x, y, z [m] Cartesian coordinates Fr [-] Froude number y+ [-] Dimensionless sublayer-scale distance g [m·s-2] Gravity ε [m2·s-3] Turbulent dissipation rate h [m] Water depth εQ [%] Inlet to outlet relative discharge error k [m2·s-2] Turbulent kinetic energy ʋ [m2·s-1] Kinematic viscosity kt [%] Time coefficient [kg·m-3] Water density l [m] Canal bottom width ω [s-1] Specific dissipation rate L [m] Canal length p [Pa] Static pressure Superscripts P [m] Perimeter ¯ Average value Q [m3·s-1] Discharge * Dimensionless value Qn [m3·s-1] Nominal discharge

Introduction Scheduled progressive shut-down of the Switzerland’s nuclear power plants requires the installation of new energy production units (Munch & Avellan [1]). In this context, alternative renewable energy sources must be reconsidered, including the unexploited small-hydro potential sites. The present work is related to the potential of the hydrokinetic energy of rivers and artificial channels. In the framework of the Hydro VS research project, the development of a new isokinetic turbine to recover the energy lost in rivers is conducted. The design and the optimization of the turbine are realized using numerical tools. The objective is the installation and testing of a prototype by the end of the year 2015. This study is mainly motivated by the need of knowing the full flow field in the pilot site, necessary for the development and, later, for the control of the prototype and the final products.

The meththe flow fthe first evaluatiodischargethe draft configuraTo this eperformeconditionat the firseach tailroutlet ofmeasured

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The preseof the ncomputatsimulatioqualitativscenarios

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hodology applfield in the whinstance, starn of the isok

e and water letubes of 3

ation (especialend, numericad in the full

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d to the expe-effective mea, Chevallet et e restricted onor even to supin order to co

mulating open& Nichols [3] s calculated iny to deal wite (Godderidgthe simulation

ent work intronumerical simtional domainons are then vve comparativs.

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lied in this stuhole canal. Thrting from inikinetic potentevels availableKaplan turbinlly at the upstal simulationscanal (includ

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rimental appran to explore

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oduces in a firsmulation moden, spatial discvalidated usinve analysis is

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tream dam hoposed by fourximum derivedvers the hydray connected wre reaching ag

Fig. 1. Schemat

udy consists ohe full 3D CAitial (dating fial of the can

e at its inlet annes, dependintream side of s of unsteadyding the tailraminal dischargt the second acondition, w

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roach, numericthe flow hydr

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olds back the Rr windows of d discharge ofaulic power frwith the tailracgain the natura

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y incompressiace tunnels) age at the three

and the third tawhereas the me

on results ary at the inlet, th

cal simulationrodynamics anamples that st

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ommercial CFee-surface. Inde main advantsurface shaperived modelswhen the gas

e case study, fo provided, id boundary ceasurements o

he flow config

al of the Laveyen as pilot siriver dam, annal.

Rhône’s water6 m x 14 m, f 220 m3/s. F

from 34 m to ce canal. The al course of th

on of the Lavey

erimental and of the Lavey ts) and recentperformed u

ions. With thevailable dischaot only may vaible homogenat prototype e tailrace tunnailrace tunneleasured waterre validated whe middle and

n presents thend to evaluatetates that, nowts, but are alses, experimenmerical model

FD codes basedeed, the volutages consist es, with the d

(e.g. Hänschis entrained u

followed by thncluding: turonditions. Thon 3 cross seguration in th

y run-of-riverite. Started-up

n underground

r at a height odisplaced on t

Fed by the hea42 m head. latest, presen

he river.

y run-of-river hy

numerical tootailrace canal 2D drawing

sing synchrone tailrace canaarge of the Rary a lot, but

neous multiphscale. Two d

nels and, respes. A constant r free surface with experimd the outlet of

e advantage ofe the hydrauliwadays, 3D hyo much more

ntal validation ls.

ed on the voluume fraction oon the methodrawback of h et al. [5]) hunder the free-

he operating crbulence modhe results of tections. Finalle whole cana

powerplant, ip in 1950, th

d headrace gal

of 8m above ththe right backadrace galleryThe flow exi

nts a regular tr

ydropower plan

ols to fully chhas been perf

gs. Then, a prnised measural randomly suRhône River,also remains

hase turbulentdifferent inlet ectively, zero discharge at tlevel is impo

mental velocityf the canal.

f being a relaic performancydraulic mode

e commonly oremains advi

ume of fluid mof each fluid inod robustness

being compuhave been pr-surface.

conditions. Andel, numericathe unsteady ly, the quanti

al for the two

installed in thhe Lavey hydllery of 4 km

he river bed ([k of the river y, the three veits the draft turapezoidal cro

nt.

haracterise formed, in reliminary ements of upplied by the flow unknown.

t flow are operating discharge

the inlet of osed at the y profiles

atively fast ces. In this els are not

operated to ised, when

method use n a control and on its utationally roposed to

n overview l scheme, numerical tative and simulated

he Western droelectric length, an

[6] & [7]). (Müller et

ertical-axis ubes by 3

oss section

1.2 The tailrace canal layout

In Fig. 2, the full 3D CAO geometry of the Lavey tailrace canal reconstructed from initial (dating from the 50’s) and recent 2D drawings is provided. One may be noticed that the canal presents a strong narrowing at the inlet section downstream the tailrace galleries. The upstream bridge is supported by the two piers that separate the three galleries. The downstream bridge is supported by 2 rectangular piers fixed in the river bed. Finally, in red – a fourth gallery and the modified inlet section of the canal (planed to be realised in the framework of the Lavey+ project [9]). The latest, remains available for a future hydrodynamic investigation and do not make the object of the current work.

Fig. 2. Lavey tailrace canal – isometric view of full 3D CAD reconstruction and photograph.

Fig. 3. Lavey tailrace canal – main geometrical dimensions and reference cross sections coordinates.

Fig. 4. Lavey tailrace canal – bottom coordinates.

The mainscaled wigreen – isections, computat

In Fig. 4length. Tdefined retrapezoidpiers of tare in goo 1.3 Wat

Time histdischargedischargethe two otime. Theenergy re

n geometrical ith the canal binlet and outlP1, P2 and P

tional domain

, the bottom The canal botteference cross

dal section, excthe downstreaod agreement

er depth and

tory of the cae values are ses over the saoperating condese conditionsecovery using

Fig. 6

dimensions obottom width,let water dept3; in black – outlet section

Fig. 5. Lav

coordinates (tom slope is s sections is pcepting the inm bridge are with the 3D g

d discharge

anal’s averagescaled with thme 3-year per

ditions consides are selected aisokinetic tec

6. Time history ov

f the canal are, l. The positith measuremezero referenc

n Sout.

vey tailrace can

scaled again babout 3/10’00

presented in Filet section Sm

shown. Finallgeometry reco

e daily dischahe nominal diriod. The timered in this stuas representathnologies.

∙100 %

of average dailyver a 3-year pe

e sketched in ion of severalent sections, ce section, Sre

nal – geometry o

by the canal 00 and is conig. 5. One ma

min where it is rly, on P1..3 sec

onstructed usin

arge over 3 yischarge of on

me coefficient udy are met retive in terms o

% - time coe

ly discharge (leferiod in the Lav

Fig. 3 from a l cross referenSm in and Sm

ef, downstream

of reference cro

bottom widthnstant. Moreoay notice that trectangular. Octions, the meng old and rec

ears is represne Kaplan turis defined in espectively aroof flow config

efficient

eft) and the rankvey tailrace can

top view persnce sections is

out; in blue –m bridge posi

oss sections.

h) are providever, the geomthe canal gene

On the Sbridge seeasured canal cent 2D drawin

ented in the lrbine. In the rEq. ( 1 ). Oneound 50% (2x

guration and v

ked discharges al.

spective. The s marked as f

– velocity meition section

ed along withmetry of the perally exhibitsection, the lefbed position ngs.

left side of Fright side – te may be obsxQn) and 30%velocity potent

(right)

values are follows: in asurement Sbridge and

h the canal previously s a regular ft and right and shape

ig. 6. The the ranked served that (3xQn) of tial for the

( 1 )

The lineaSm out, anscaled witurbine Qsections oby linear well.

1.4 Oper

The summzero dischdischargenumbers developedin the can

2. Mod2.1 Num

Numericafull canal2. The AAveragedusing the two-equaable to s(preferredbased on (Menter ein time) a[14], the

ar relationshipnd the total caith the canal bQn. In the righof the canal Δregression, ar

Fig. 7. Measu

rating condit

mary of the oharge at the f

e at the three are computed

d turbulent flonal, for both o

delling merical schem

al simulationsl (including th

ANSYS CFX d Navier-Stok finite volume

ation turbulencselect the optid in the bounda blending fu

et al. [13]). Anare used. The mtwo phases (a

p between the anal hourly disbottom width lht figure - thΔh*

Sm in-out withre represented

ured water depth

tions

operating condfirst with nomtailrace tunned at the P1 reow, whilst onperating cond

C

1

2

me

s of unsteady ihe tailrace tun14.5.7 comm

kes (URANS)e method (seece model andimal turbulendary layer) at unction that con advection scmultiphase fre

air and water)

measured wascharge is prol, whilst the d

he variation oh the dischargd in red. The e

h-discharge rel

ditions for theminal dischargels (case 2). Teference secti

n the other handitions.

∙∙

∙ ∙ ∙

Table 1

Case Q*inlet

Q1 = 0

Q2 = Q3

Q = 2·Qn

Q1 = Q2

Q = 3·Qn

incompressiblnnels) at protot

mercial code [1 equations in Launder & Sthe Shear Str

nce model betany location iomputes the dcheme (2nd ordee-surface is sshare the sam

ater depth at tovided in the discharge Q* isof the water dge Q*. The aveequations of t

lationship at the

e two scenarioge at the seconThe dimensionion. On the ond the Froude

∙ - Re

- Froud

1. Operating co

[-] R

= Qn

n

6’

= Q3 = Qn

n 9’

le homogeneotype scale. A 10] has been

n their conservSpalding [11])ress Transportween the k-εinto the domadistance from der in space) asolved using t

me flow field,

the inlet and oleft side of F

s scaled with tdepth differenerage water dthe correspond

e inlet and outl

os considered nd and the thinless Reynoldone hand, thee number show

eynolds numb

de number

nditions

Re [-] Fr

’852’664 0.1

’784’556 0.1

ous multiphasesummary of temployed to

vative form a). The set of eqrt (SST) modeε (preferred iain. The select

the wall usinand the backwhe homogenothe transporte

outlet sectionsFig. 7. The wathe nominal d

nce between tepth – discharding linear var

et of the Lavey

in this study ird tailrace tunds (Eq. ( 2 )) e Reynolds nuws a subcritica

er

[-]

49

89

e turbulent flothe numerical solve both th

and the mass quations is cloel (Menter [12n the free strtion of the mong the solutionward Euler impus model. As

ed quantities b

s of the canalater depth valdischarge of othe inlet and rge variations

ariations are pr

tailrace canal.

is provided innnels (case 1)and Froude (

umber suggesal flow regim

ow are performl setup is givenhe Unsteady conservation osed and solv2]). Indeed, thream regions)ost appropriaten of a Poisson

mplicit scheme stated in Harr

being the same

, Sm in and lues h* are ne Kaplan the outlet

s, obtained rovided as

n Table 1: ); nominal (Eq. ( 3 )) sts a fully

me (Fr < 1)

( 2 )

( 3 )

med in the n in Table Reynolds-equations

ed using a he latest is ) and k-ω e model is n equation (2nd order

rison et al. e for both.

The volumfor each.

The Stroustructureson this cois selecte

2.2 Com

As illustrscale - frhexahedr

me of fractionFinally, the v

uhal number, s developing iomputation. Cd.

mputational d

rated in Fig. 8rom the inlet ral cells (see F

n is specific tviscosity and th

Eq. ( 4 ), hain the wake o

Concerning the

Tab

Simulation ty

Numerical m

Physical mod

Turbulence m

Time step

Convergence

domain and sp

8, the computtunnels to the

Fig. 9) has bee

Fig. 8. Co

o the phase, the density are

as been used of the downstre convergence

le 2. Main para

ype

ethod

del

model

criteria

patial discret

tational domae junction witen generated u

mputational do

Fig. 9.

the free surface volume fract

to determine ream bridge pe, the RMSmax

ameters of the n

Un

Fin

Mu

SS

0.1

RM

tization

ain includes thth the Rhône

using the ANS

omain of the ful

Spatial discret

ce being tracktion averaged

- Strouh

the expectedpiers. A time sx < 10-3 criteri

numerical simul

nsteady

nite volume

ultiphase homo

ST

1 [s]

MSmax < 10-3

he full tailraceRiver. An ad

SYS ICEM com

ll 3D Lavey tail

tisation.

ked by solvingin the transpo

hal number

d vortex frequstep of 0.1 s iion with 10 in

ation

ogeneous

e canal water dapted mesh ummercial soft

race canal.

g the transporort equations.

uency of the ais finally selecnternal coeffic

r passage - at using mostly tware.

rt equation

( 4 )

alternative cted based cient loops

prototype structured

The geneused for applied inresiduals

2.3 Boun

The detaiconstant measureda free slipsurfaces:

3. Resu3.1 Conv

The RMSmomentuduration trailing e(exceptinvalue onl

Case

1

2

eral mesh sizeboth cases. Tn order to copconvergence

ndary conditi

iled boundarydischarge at t

d water free sup wall conditicanal banks,

ults and anavergence

Smax < 10-3 haum for the two– see the res

edge of the dng the vortex ily after around

Simulation st

Initial

First refineme

Final (second

Initial

First refineme

Final (second

e information Then, two autpe with the neand realistic w

ions

y conditions imthe inlet of eaurface level alion is used. Ficanal bottom,

Surfa

Inlet

Outle

Top

Solid

alysis

as been impoo cases (final iduals history

downstream binduced fluctud 100 seconds

Table 3

tep

nt

d refinement)

nt

d refinement)

is provided intomatic refineeed of a finerwater surface

mposed on theach tailrace tunlong with a hyinally, smooth upstream and

Table 4

ace

et

surfaces

sed as convermesh refinem

y in Fig. 10. Obridge piers ruations), the is – see Fig. 11

Fig. 10. R

3. Spatial discre

Mesh type

Structured

Structured

n Table 3. Onement steps, br mesh at the solution.

e computationnnel is used aydrostatic presh no-slip walld downstream

4. Boundary con

Boundary

Inlet Q1 = 0 / Qn

Q2 = Q3 = Q

Outlet hout = hSm ou

pout = ·g·z

Free slip wa

Smooth no-

ergence criteriment) exhibit rOn the other remains relatiinlet to outlet .

RMS convergen

etisation

e Numb

d

4’

5’

6’

d

4’

5’

6’

ne may be notbased on the free-surface.

nal domain areas inlet conditssure profile il condition is

m bridge piers.

nditions

condition

[m3/s]

Qn [m3/s]

ut [m] [Pa]

all

-slip wall

ion. On the orelatively stabhand, despitevely constantrelative disch

nce history.

ber of nodes

559’076

957’681

574’673

559’076

940’509

652’480

ticed that an iwater volumeThis step is c

e provided in Ttion. At the ouis imposed. Onselected for th

one hand, the ble values ovee the fact thatt over the totharge error εQ

y+mean

488.398

651.966

identical initiae fraction critcritical in term

Table 4. Accoutlet of the do

On the top of thhe remaining

RMS of the er the whole st the water letal simulation

Q reaches a sm

al mesh is terion, are

ms of both

ordingly, a omain, the he domain solid wall

mass and simulation evel at the n duration mall stable

Fig. 11. Convergence history of mass conservation (left) and the water level at the trailing edge of the downstream bridge piers (right).

3.2 Experimental validation

Experimental measurements of flow velocity have been performed at the P1, P2 and P3 sections (see Fig. 3 ) using an Acoustic Doppler Current Profiler (ADCP) mounted on a radio-controlled boat equipped with a GPRS system. In Fig. 12, the axial velocity, scaled with the discharge velocity at the P1 section, is represented in comparison between the experimental measurements and instantaneous numerical simulation results. It may be noticed that the velocity profiles obtained by numerical simulation feet relatively well the measurements at the P2 and P3 sections. Nonetheless, at the P1 section, the numerical axial velocity profile is still similar to the experimental one at the right bank side, whilst being different on the left bank side. This inconsistence may be explained by some lack in the measurement data, since disturbances have been noticed at that region during the measurement process.

Fig. 12. Experimental validation – dimensionless axial velocity profiles.

Fig. 13. Experimental validation – water surface level in streamwise direction.

Finally, in Fig. 13, one may be stated that the water surface level obtained by numerical simulations is in good agreement with the one obtained from previous measurement data analysis (see Fig. 7). The slightly lower water surface level in the numerical simulation may be explained by the fact that the roughness of the real canal is not taken in consideration; therefore, the losses in the canal are lower with a direct impact on the water surface level. 3.3 Flow analysis for different canal flow discharge

The resulting water free-surface is illustrated in Fig. 14 for the two numerical simulations with the help of an iso-surface of water volume fraction. The streamlines projected on the water surface indicates a very different flow configuration in the canal depending on the number of turbines that operates at time. On the one hand, when all the three turbines operate at the same regime (case 2) the flow exiting the tailrace canal converge smoothly to the regular trapezoidal section of the canal. On the other hand, a large stagnation/recirculation region is noticed at the left bank side in front of the first tailrace tunnel since the discharge of the latest is zero. Indeed, this stagnation region is also observed on the axial velocity profile at the P1 section (see Fig. 12). Then, once arrived in the downstream regular section of the canal, there is no significant flow configuration difference between the two simulated scenarios.

Fig. 14. Free surface and velocity streamlines in the tailrace canal for two operating situations.

In Fig. 15, the axial velocity contours, scaled with the discharge velocity at the P1 section, are provided for both cases at the P1, P2 and P3 sections. In Fig. 16, the magnitude of the cross velocity |Cyz|, scaled again with the discharge velocity at the P1 section, demonstrates an almost completely axial flow configuration on the whole canal length. However, a large magnitude of the secondary flow is observed on the inlet section for the case where the discharge of the first tailrace tunnel is zero (case 1). This is explained by the presence of the stagnation/recirculation region on that section.

Fig. 15. Case 1 vs. case 2 – dimensionless axial velocity profiles.

Finally, astructureshas been has not bare not op

3.4 Disc

Boundarymultiphasmesh refiunsteady)numericacomparedcomplete the free-scomputat

The presescenariosto facilitalatest preperforman

F

as expected, ws is evidencedalready detec

been pushed fuptimised to all

Fig. 17. E

ussion

y conditions se problems (einement in the) comes to com

al result. Wrod to a comple set of numer

surface regiontional domains

ent work endss at the pilot siate the integresents the ad

ances.

Fig. 16. Case 1 v

when focusingd in the wake cted in the histfurther since tlow a fully pe

Evidence of Kar

play an impoe.g. free-surfae free-surface mplete the setong numericaetely unreal srical tests perfn may conducts.

s up with valiite. The compation into the

dvantage of c

vs. case 2 – dim

g on the downof the piers u

tory of the wahe constructe

ertinent quanti

rman vortices de

ortant role inace flow), the

region is a cat of parameteral setup may solution. Thisformed duringt to mass cons

idated free-suputational dome domain of acapturing the

mensionless mag

nstream bridgusing the λ2 cater level flucted spatial discification.

evelopment in t

n the numericcorrect setting

apital setting ars that makes t

conduct to ds statement isg this study. Iservation inco

urface flow numains and the a completely

free-surface

gnitude of cross

ge region (see riterion. Anywtuations, plottecretisation and

the wake of the

cal simulationg of boundaryas well. In thethe differencedivergence, ws not only baIt has been exonsistence, esp

umerical simuspatial discreimmerged isoeffects on th

s velocity profil

Fig. 17), a dway, the preseed in Fig. 11. d the choice o

downstream br

n setup. Whey conditions ise end, the sim between a fal

which is mayased on the lixperienced thapecially when

ulations for twtisation have bokinetic horizhe turbine op

les.

development oence of these The frequenc

of the turbulen

ridge piers.

en attemptings even crucial.

mulation type (alse and a fullyybe not the witerature, but at a too coarsen dealing with

wo canal flow been already

zontal-axis turperation and

of Karman structures

cy analysis nce model

g to solve . The right (steady vs. y pertinent worst case

also on a e mesh on very long

discharge conceived rbine. The hydraulic

Conclusions Free-surface flow numerical simulations in the tailrace canal of the Lavey run-of-river hydro powerplant have been performed to investigate its isokinetic potential in the view of installing new technologies to recover energy of rivers and artificial channels. The numerical simulation is performed using the ANSYS CFX 14.5.7 commercial code, solving the incompressible unsteady Reynolds-Averaged Navier-Stokes equations. The computational domain includes the full tailrace canal water passage from the inlet tunnels to the junction with the Rhône River. Depending on the number of Kaplan turbines operating at time, two different inlet operating conditions have been selected: nominal discharge at the three tailrace tunnels; zero discharge at the first with nominal discharge at the second and the third tailrace tunnels. The boundary conditions are completed with the measured water surface level imposed at the outlet of the canal. Finally, measured axial velocity profiles on 3 different cross sections of the canal as well as the water surface level at the inlet of the canal have been used to validate the results.

To sum up, it is found that, depending on the number of turbines that operate at time, the flow configuration in the tailrace canal may vary a lot. These results are crucial for the selection of the optimal implantation location of an isokinetic turbine in order to recover a maximum of energy over the whole year for any operating condition. In addition, the computational domain and the numerical setup allow, later on, including in the simulation the full isokinetic turbine as well. Acknowledgements

The present numerical investigation was carried out in the framework of Hydro VS applied research project, in partnership with the Laboratory for Hydraulic Machines from École Polytechnique Fédérale de Lausanne, Switzerland, granted by the program The Ark Energy of the Ark – the foundation for innovation in Valais, Switzerland.

The authors would like to address a special thank to the “Services Industriels de Lausanne” and “Usine de Lavey” industrial partners for their approval and technical support in using the Lavey powerplant as case study. The Hydro Exploitation industrial partner is also thanked for the technical support in performing the velocity measurements. References 1. Münch-Alligné C., Avellan F., “Exploitation du potentiel de la petite hydraulique : Situation actuelle et exemple de

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ANSYS CFX”, SimHydro 2012: New trends in simulation, Sophia Antipolis, France, September 12-14, 2012 3. Hirt C.V., Nichols B.D., “Volume of Fluid (VOF) Method for the Dynamics of Free Boundaries”, Journal of

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7. Services Industriels de la Ville de Lausanne, “Lavey – Usine Hydro-Electrique de la Ville de Lausanne”, Ed. Annuaire Vaudois S.A., Lausanne, Switzerland, 1951

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9. Services Industriels de Lausanne, “Présentation du projet Lavey+”, 2012 source: http://www.fishfinder.ch/deutsch/news/2012/infotag/Amenagement%20hydroelectrique%20Lavey%20plus.pdf - accessed on august 2014

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pp. 1598-1605, 1994 13. Menter F.R., Kuntz M., Langtry R., “Ten Years of Industrial Experience with the SST Turbulence Model”, Turbulence,

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The Authors

Vlad Hasmatuchi graduated in 2007 at the Faculty of Mechanical Engineering, Hydraulic Machinery Branch from “Politehnica” University of Timisoara, Romania. In the same year, Vlad Hasmatuchi joined the Laboratory for Hydraulic Machines from the École Polytechnique Fédérale de Lausanne (EPFL), Switzerland, to achieve a doctoral work in the field of hydraulic turbomachinery. In 2012 he got his Doctoral Degree in Engineering from the EPFL. Since 2012 he is Senior Research Assistant in the hydraulic energy research team at the HES-SO Valais//Wallis, School of Engineering in Sion, Switzerland. He is in charge mainly of experimental investigations, as well as of numerical simulations. His main research interests are the hydrodynamics of turbines, pumps and pump-turbines, including design and evaluation of hydraulic performance.

Prof. François Avellan graduated in Hydraulic Engineering from INPG, École Nationale Supérieure d'Hydraulique, Grenoble France, in 1977 and, in 1980, got his doctoral degree in engineering from University of Aix-Marseille II, France. Research associate at EPFL in 1980, he is director of the Laboratory for Hydraulic Machines since 1994 and was appointed Ordinary Professor in 2003.

Cécile Münch was born in Strasbourg in 1979. She obtained an engineering degree from INPG, École Nationale Supérieure d'Hydraulique, Grenoble France ENSHMG, department of Numerical and Modelling of Fluids and Solids in 2002. Then, she got her doctoral degree in 2005 at the INPG on numerical simulation of turbulence. From 2006 to 2010, she worked as a research associate in the Laboratory of Hydraulics Machines at EPFL on flow numerical simulations in hydraulic turbines. Since 2010, she is professor at the HES-SO Valais//Wallis, School of Engineering in Sion, Switzerland and head of the hydraulic energy research team.