Abstract

Turbulent-ribbed channels are extensively used in turbomachinery to enhance convective heat transfer in internally cooled components such as turbine blades. One of the key aspects of such a problem is the distribution of the heat transfer coefficient (HTC) in fully developed flows, and many studies have addressed this problem by the use of computational fluid dynamics (CFD). In the present document, large eddy simulation (LES) is performed for a configuration from a test-rig at the Von Karman Institute representing a square channel with periodic square ribs. The whole channel is computed in an attempt to better understand HTC maps in this specific configuration. Resulting mean and unsteady flow features are captured, and predictions are used to further explain the obtained HTC distribution. More specifically turbulent structures are seen to bring cold gas from the main flow to the wall. A statistical analysis of these events using the joint velocity-temperature probability density function (PDF), and quadrant method allows to define four types of events happening at every location of the channel and which can then be linked to the HTC distribution. First, the HTC is very high where the flow impacts the wall with cold temperature whereas it is lower where the hot gas is ejected to the main flow. In an attempt to link the HTC trace on the channel wall with structures in the flow field far-off the wall, the main modes are identified performing power spectral density (PSD) analysis of the velocity along the channel. Dynamic mode decomposition (DMD) of the flow field data is then used to present the spatio-temporal characteristics of two of the identified most dominant modes: a vortex-street mode linked to the first rib and a rib-to-rib mode appearing because of the quasi-periodicity of the configuration. However, DMD analysis of the HTC trace on the wall does not emphasize any dominant mode. This indicates a weak link between the main flow large scale features and the instantaneous and more local HTC distribution.

References

1.
Han
,
J.
, and
Park
,
J. S.
,
1988
, “
Developing Heat Transfer in Rectangular Channels With Rib Turbulators
,”
Int. J. Heat. Mass. Transfer.
,
31
(
1
), pp.
183
195
.
2.
Liou
,
T.-M.
, and
Hwang
,
J.-J.
,
1992
, “
Turbulent Heat Transfer Augmentation and Friction in Periodic Fully Developed Channel Flows
,”
ASME J. Heat. Transfer.
,
114
(
1
), pp.
56
64
.
3.
Han
,
J.-C.
,
Dutta
,
S.
, and
Ekkad
,
S.
,
2012
,
Gas Turbine Heat Transfer and Cooling Technology
,
CRC Press
,
Boca Raton, FL
.
4.
Promvonge
,
P.
, and
Thianpong
,
C.
,
2008
, “
Thermal Performance Assessment of Turbulent Channel Flows Over Different Shaped Ribs
,”
Int. Commun. Heat Mass Trans.
,
35
(
10
), pp.
1327
1334
.
5.
Rau
,
G.
,
Cakan
,
M.
,
Moeller
,
D.
, and
Arts
,
T.
,
1996
, “
The Effect of Periodic Ribs on the Local Aerodynamic and Heat Transfer Performance of a Straight Cooling Channel
,”
ASME 1996 International Gas Turbine and Aeroengine Congress and Exhibition
,
Birmingham, UK
,
June 10–13
,
American Society of Mechanical Engineers
, p.
V004T09A061
.
6.
Mochizuki
,
S.
,
Murata
,
A.
, and
Fukunaga
,
M.
,
1997
, “
Effects of Rib Arrangements on Pressure Drop and Heat Transfer in a Rib-Roughened Channel With a Sharp 180 Deg Turn
,”
ASME J. Turbomach.
,
119
(
3
), pp.
610
616
.
7.
Han
,
J.
,
1984
, “
Heat Transfer and Friction in Channels with Two Opposite Rib-roughened Walls
,”
ASME J. Heat. Transfer.
,
106
(
4
), pp.
774
781
.
8.
Viswanathan
,
A. K.
, and
Tafti
,
D. K.
,
2006
, “
Detached Eddy Simulation of Flow and Heat Transfer in Fully Developed Rotating Internal Cooling Channel With Normal Ribs
,”
Int. J. Heat Fluid Flow
,
27
(
3
), pp.
351
370
.
9.
Coletti
,
F.
,
Cresci
,
I.
, and
Arts
,
T.
,
2012
, “
Time-resolved PIV Measurements of Turbulent Flow in Rotating Rib-Roughened Channel With Coriolis and Buoyancy Forces
,”
ASME Turbo Expo 2012: Turbine Technical Conference and Exposition
,
Copenhagen, Denmark
,
June 11–15
,
American Society of Mechanical Engineers Digital Collection
, pp.
553
562
.
10.
Iacovides
,
H.
, and
Raisee
,
M.
,
1999
, “
Recent Progress in the Computation of Flow and Heat Transfer in Internal Cooling Passages of Turbine Blades
,”
Int. J. Heat Fluid Flow
,
20
(
3
), pp.
320
328
.
11.
Jang
,
Y.-J.
,
Chen
,
H.-C.
, and
Han
,
J.-C.
,
2000
, “
Flow and Heat Transfer in a Rotating Square Channel with 45 Deg Angled Ribs by Reynolds Stress Turbulence Model
,”
ASME J. Turbomach.
,
123
(
1
), pp.
124
132
.
12.
Borello
,
D.
,
Salvagni
,
A.
, and
Hanjalić
,
K.
,
2015
, “
Effects of Rotation on Flow in An Asymmetric Rib-Roughened Duct: Les Study
,”
Int. J. Heat Fluid Flow
,
55
, pp.
104
119
.
13.
Mayo
,
I.
,
Arts
,
T.
, and
Gicquel
,
L. Y.
,
2018
, “
The Three-Dimensional Flow Field and Heat Transfer in a Rib-Roughened Channel At Large Rotation Numbers
,”
Int. J. Heat. Mass. Transfer.
,
123
, pp.
848
866
.
14.
Sewall
,
E. A.
, and
Tafti
,
D. K.
,
2004
, “
Large Eddy Simulation of the Developing Region of a Rotating Ribbed Internal Turbine Blade Cooling Channel
,”
ASME Turbo Expo 2004: Power for Land, Sea, and Air
,
Vienna, Austria
,
June 14–17
,
American Society of Mechanical Engineers Digital Collection
, pp.
749
764
.
15.
Cui
,
J.
,
Patel
,
V. C.
, and
Lin
,
C.-L.
,
2003
, “
Large-eddy Simulation of Turbulent Flow in a Channel With Rib Roughness
,”
Int. J. Heat Fluid Flow
,
24
(
3
), pp.
372
388
.
16.
Fransen
,
R.
,
Vial
,
L.
, and
Gicquel
,
L. Y.
,
2013
, “
Large Eddy Simulation of Rotating Ribbed Channel
,”
ASME Turbo Expo 2013: Turbine Technical Conference and Exposition
,
San Antonio, TX
,
June 3–7
,
American Society of Mechanical Engineers Digital Collection
.
17.
Fransen
,
R.
,
Gourdain
,
N.
, and
Gicquel
,
L. Y.
,
2012
, “
Steady and Unsteady Modeling for Heat Transfer Predictions of High Pressure Turbine Blade Internal Cooling
,”
ASME Turbo Expo 2012: Turbine Technical Conference and Exposition
,
Copenhagen, Denmark
,
June 11–15
,
American Society of Mechanical Engineers Digital Collection
, pp.
563
572
.
18.
Grosnickel
,
T.
,
Duchaine
,
F.
,
Gicquel
,
L. Y.
, and
Koupper
,
C.
,
2017
, “
Large Eddy Simulations of Static and Rotating Ribbed Channels in Adiabatic and Isothermal Conditions
,”
ASME Turbo Expo 2017: Turbomachinery Technical Conference and Exposition
,
Charlotte, NC
,
June 26–30
,
American Society of Mechanical Engineers Digital Collection
.
19.
Mayo
,
I.
,
Lahalle
,
A.
,
Gori
,
G. L.
, and
Arts
,
T.
,
2015
, “
Aerothermal Characterization of a Rotating Ribbed Channel at Engine Representative Conditions: Part II-Detailed LCT Measurements
,”
ASME Turbo Expo 2015: Turbine Technical Conference and Exposition
,
Montreal, Quebec, Canada
,
June 15–19
,
American Society of Mechanical Engineers Digital Collection
.
20.
Mayo
,
I.
,
Gori
,
G. L.
,
Lahalle
,
A.
, and
Arts
,
T.
,
2016
, “
Aerothermal Characterization of a Rotating Ribbed Channel at Engine Representative Conditions-Part I: High-Resolution Particle Image Velocimetry Measurements
,”
ASME J. Turbomach.
,
138
(
10
), p.
101008
.
21.
Di Sante
,
A.
,
Theunissen
,
R.
, and
Van den Braembussche
,
R. A.
,
2008
, “
A New Facility for Time-resolved Piv Measurements in Rotating Channels
,”
Exp. Fluids
,
44
(
2
), pp.
179
188
.
22.
Mayo
,
I.
,
Arts
,
T.
,
El-Habib
,
A.
, and
Parres
,
B.
,
2015
, “
Two-Dimensional Heat Transfer Distribution of a Rotating Ribbed Channel At Different Reynolds Numbers
,”
ASME J. Turbomach.
,
137
(
3
), p.
031002
.
23.
Schönfeld
,
T.
, and
Rudgyard
,
M.
,
1999
, “
Steady and Unsteady Flow Simulations Using the Hybrid Flow Solver Avbp
,”
AIAA J.
,
37
(
11
), pp.
1378
1385
.
24.
Colin
,
O.
, and
Rudgyard
,
M.
,
2000
, “
Development of High-Order Taylor-Ggalerkin Schemes for LES
,”
J. Comput. Phys.
,
162
(
2
), pp.
338
371
.
25.
Nicoud
,
F.
, and
Ducros
,
F.
,
1999
, “
Subgrid-Scale Stress Modelling Based on the Square of the Velocity Gradient Tensor
,”
Flow, Turbulence Combust.
,
62
(
3
), pp.
183
200
.
26.
Duchaine
,
F.
,
Maheu
,
N.
,
Moureau
,
V.
,
Balarac
,
G.
, and
Moreau
,
S.
,
2014
, “
Large-eddy Simulation and Conjugate Heat Transfer Around a Low-Mach Turbine Blade
,”
ASME J. Turbomach.
,
136
(
5
), p.
051015
.
27.
Koupper
,
C.
,
2015
, “
Unsteady Multi-Component Simulations Dedicated to the Impact of the Combustion Chamber on the Turbine of Aeronautical Gas Turbines
,”
Ph.D. thesis
,
Institut National Polytechnique de Toulouse
,
Toulouse, France
.
28.
Papadogiannis
,
D.
,
2015
, “
Coupled Large Eddy Simulations of Combustion Chamber-Turbine Interactions
,”
Ph.D. thesis
,
Institut National Polytechnique de Toulouse
,
Toulouse, France
.
29.
Gicquel
,
L. Y.
,
Staffelbach
,
G.
, and
Poinsot
,
T.
,
2012
, “
Large Eddy Simulations of Gaseous Flames in Gas Turbine Combustion Chambers
,”
Prog. Energy. Combust. Sci.
,
38
(
6
), pp.
782
817
.
30.
Fransen
,
R
,
2013
, “
Les Based Aerothermal Modeling of Turbine Blade Cooling Systems
,”
Ph.D. thesis
,
Institut National Polytechnique de Toulouse
,
Toulouse, France
.
31.
Duchaine
,
F.
,
Gicquel
,
L.
,
Grosnickel
,
T.
, and
Koupper
,
C.
,
2019
, “
Large Eddy Simulation of the Flow Developing in Static and Rotating Ribbed Channels
,”
ASME Turbo Expo 2019: Turbomachinery Technical Conference and Exposition
,
Phoenix, AZ
,
June 17–21
,
American Society of Mechanical Engineers Digital Collection
.
32.
Poinsot
,
T. J.
, and
Lele
,
S.
,
1992
, “
Boundary Conditions for Direct Simulations of Compressible Viscous Flows
,”
J. Comput. Phys.
,
101
(
1
), pp.
104
129
.
33.
Granet
,
V.
,
Vermorel
,
O.
,
Léonard
,
T.
,
Gicquel
,
L.
, and
Poinsot
,
T.
,
2010
, “
Comparison of Nonreflecting Outlet Boundary Conditions for Compressible Solvers on Unstructured Grids
,”
AIAA J.
,
48
(
10
), pp.
2348
2364
.
34.
Pope
,
S. B.
,
2000
,
Turbulent Flows
,
Cambridge University Press
,
Cambridge, UK
.
35.
Webb
,
R.
,
Eckert
,
E.
, and
Goldstein
,
R.
,
1971
, “
Heat Transfer and Friction in Tubes With Repeated-rib Roughness
,”
Int. J. Heat. Mass. Transfer.
,
14
(
4
), pp.
601
617
.
36.
Liou
,
T.-M.
,
Wu
,
Y.-Y.
, and
Chang
,
Y.
,
1993
, “
Ldv Measurements of Periodic Fully Developed Main and Secondary Flows in a Channel with Rib-disturbed Walls
,”
J. Fluid. Eng.
,
115
(
1
), pp.
109
114
.
37.
Hirota
,
M.
,
Yokosawa
,
H.
, and
Fujita
,
H.
,
1992
, “
Turbulence Kinetic Energy in Turbulent Flows Through Square Ducts With Rib-Roughened Walls
,”
Int. J. Heat Fluid Flow
,
13
(
1
), pp.
22
29
.
38.
Grosnickel
,
T
,
2019
, “
Simulations Des Grandes échelles Pour La Prédiction Des écoulements De Refroidissement Des Pales De Turbines
,”
Ph.D. thesis
,
Institut National Polytechnique de Toulouse
,
Toulouse, France
.
39.
Aillaud
,
P.
,
Duchaine
,
F.
,
Gicquel
,
L.
, and
Didorally
,
S.
,
2016
, “
Secondary Peak in the Nusselt Number Distribution of Impinging Jet Flows: A Phenomenological Analysis
,”
Phys. Fluids
,
28
(
9
), p.
095110
.
40.
Okajima
,
A.
,
1982
, “
Strouhal Numbers of Rectangular Cylinders
,”
J. Fluid. Mech.
,
123
, pp.
379
398
.
41.
Schmid
,
P. J.
,
2010
, “
Dynamic Mode Decomposition of Numerical and Experimental Data
,”
J. Fluid. Mech.
,
656
, pp.
5
28
.
You do not currently have access to this content.