Predicting the Thermal Conductivity of AlSi/Polyester Abradable Coatings: Effects of the Numerical...
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Transcript of Predicting the Thermal Conductivity of AlSi/Polyester Abradable Coatings: Effects of the Numerical...
European Workshop on New Aero Engine ConceptsMunich, 30 June – 1 July 2010
Predicting the thermal conductivity of AlSi/polyester abradable coatings:
effects of the numerical method
NEWAC is an Integrated Project Co-funded by the European Commission within the Sixth Framework Programme(2002-2006) under Thematic Priority 4 Aeronautics and Space. 1
Presenter : Rodolphe BOLOT, UTBM – LERMPS
Authors : Rodolphe BOLOT, Jean-Louis SEICHEPINE,Jiang-Hao QIAO, Christian CODDET, UTBM – LERMPS
European Workshop on New Aero Engine ConceptsMunich, 30 June – 1 July 2010
Introduction
First results(2008)
New developments
Role of UTBM – LERMPS in NEWAC:WP 5.4: Blade/casing rub management for tight tip c learancesTask: Numerical modelling of abradable coatings
Abradable coatings are used as seals between the st atic and rotating parts of aero engines
Scope of the present study: to model the effective properties
NEWAC is an Integrated Project Co-funded by the European Commission within the Sixth Framework Programme(2002-2006) under Thematic Priority 4 Aeronautics and Space. 2
New results
ConclusionsPerspectives
Scope of the present study: to model the effective propertiesof AlSi/polyester abradable coatings
In order to predict these propertiesfrom micrographs, numerical studieswere performed Blade tip
Abradable coatingon casing
European Workshop on New Aero Engine ConceptsMunich, 30 June – 1 July 2010
2 different codes were applied to estimate the effe ctive thermal conductivity of AlSi/polyester abradable se als
OOF2: Object Oriented Finite Element Analysis of Microstructures – software developed by NIST under L INUXMain drawback: requires much RAM (4 Gbytes: 0.4 mil lion of cells)(not possible to consider big images without geometric approximations, e.g. mesh with one cell/pixel not possible above 0.4 million of pixels)
Introduction
First results(2008)
New developments
NEWAC is an Integrated Project Co-funded by the European Commission within the Sixth Framework Programme(2002-2006) under Thematic Priority 4 Aeronautics and Space. 3
with one cell/pixel not possible above 0.4 million of pixels)
TS2C1 in-house (finite differences)� Real architecture of the coating structure� Image analysis (… choice of adequate thresholds)� Mesh = image (pixels = cells)� System of equations (size = number of pixels of the image)� Solving procedure (SOR or LSOR methods)� Main advantage :
no problem of RAM (about 32Mbytes for an image of 0.4 million of pixels)
1See Bolot et al. (Num. Heat Trans., 47(9), 2005)
New results
ConclusionsPerspectives
European Workshop on New Aero Engine ConceptsMunich, 30 June – 1 July 2010
OOF2Geometric
approximations
NEWAC is an Integrated Project Co-funded by the European Commission within the Sixth Framework Programme(2002-2006) under Thematic Priority 4 Aeronautics and Space. 4
European Workshop on New Aero Engine ConceptsMunich, 30 June – 1 July 2010
TS2CEach pixel of the original
image is a cell
NEWAC is an Integrated Project Co-funded by the European Commission within the Sixth Framework Programme(2002-2006) under Thematic Priority 4 Aeronautics and Space. 5
European Workshop on New Aero Engine ConceptsMunich, 30 June – 1 July 2010
Typical structure of an
Des
peck
le fi
lterin
g
ImageResolution
κ (W.m-1.K-1)
TS2C OOF2
100%* 0.467 0.485
75% 0.468 0.500
50% 0.458 0.511
Introduction
First results(2008)
New developments
Synthesis of the computed results
NEWAC is an Integrated Project Co-funded by the European Commission within the Sixth Framework Programme(2002-2006) under Thematic Priority 4 Aeronautics and Space. 6
Typical structure of anAlSi/polyester coating(SM Durabrade 1605 powder)
Simplified structure of the same AlSi/polyester coating
Des
peck
le fi
lterin
g
25% 0.402 0.549
* corresponding to an image of 756x541 (0.4 M of pixels)
0
0.1
0.2
0.3
0.4
0.5
0.6
20% 40% 60% 80% 100%
Image resolution
The
rmal
con
duct
ivity
(W.m
-1.K
-1)
TS2C
OOF2
New results
ConclusionsPerspectives
European Workshop on New Aero Engine ConceptsMunich, 30 June – 1 July 2010
Introduction
First results(2008)
New developments
Conclusions(ITSC Conference, Maastricht, 2008)
� Quite significant differences were noticed especially for low resolution images (difference of 30% at the lowest resolution of 25%)
� A converging tendency was obtained for the highest resolution (difference of 3-4% at the highest resolution level)
NEWAC is an Integrated Project Co-funded by the European Commission within the Sixth Framework Programme(2002-2006) under Thematic Priority 4 Aeronautics and Space. 7
New results
ConclusionsPerspectives
The reasons are now explained:� OOF2 uses a nodal approach whereas our original version
of TS2C uses a cell-centered approach� A nodal version of TS2C was developed during 2009 as well
as a "split pixel" formulation (4 cells or more per pixel)� Complementary results could be obtained for simplified or
non simplified coating structures (i.e. with and without applying the Despeckle filtering)
European Workshop on New Aero Engine ConceptsMunich, 30 June – 1 July 2010
•
2D heat conduction equation:
0=
∂∂
∂∂−
∂∂
∂∂−
yT
yxT
xκκ
T(i,j) T(i+1,j)T(i-1,j)
T(i,j+1)
T(i,j-1)
Pix(i,j)
Pix(i,j+1)
Pix(i+1,j)
Pix(i+1,j+1)
T(i,j)T(i-1,j) T(i+1,j)
T(i,j+1)
T(i,j-1)Y
Introduction
First results(2008)
New developments
Centered and nodal formulations
NEWAC is an Integrated Project Co-funded by the European Commission within the Sixth Framework Programme(2002-2006) under Thematic Priority 4 Aeronautics and Space. 8
Linearized equation:
( ) ( ) ( ) ( )
( ) ( ) ( ) ( ) ( )1j,iAyj,iAyj,1iAxj,iAxj,iAp
with
1i,jκ
1i,jκ
12
Ay(i,j) and
,j1iκ1
i,jκ
12
Ax(i,j)
:nformulatio Centered
+++++=
−+
=
−+
=
)1,()1,()1,(),(),1(),1(),1(),(),(),( +++−++++−= jiTjiAyjiTjiAyjiTjiAxjiTjiAxjiTjiAp
1 linear equation per pixel
X
( ) ( ) ( ) ( )
( ) ( ) ( ) ( ) ( )1j,iAyj,iAyj,1iAxj,iAxj,iAp
with2
,j1iκi,jκAy(i,j) and
21i,jκi,jκ
Ax(i,j)
:nformulatioNodal
+++++=
++=++=
New results
ConclusionsPerspectives
European Workshop on New Aero Engine ConceptsMunich, 30 June – 1 July 2010
Introduction
First results(2008)
New developments
0.50.60.7
Pre
dict
ed th
erm
al
cond
uctiv
ity
Complementary results produced with the nodal version of TS2C
Additional results for the 200% resolution(i.e. 4 cells/pixel )
NEWAC is an Integrated Project Co-funded by the European Commission within the Sixth Framework Programme(2002-2006) under Thematic Priority 4 Aeronautics and Space. 9
New results
ConclusionsPerspectives
00.10.20.30.4
0% 50% 100% 150% 200%
Image resolution
Pre
dict
ed th
erm
al
cond
uctiv
ity
TS2C
TS2C_NF
OOF2
Assumed properties:κAlSi=130 W.m-1.K-1
κPolyester=0.17 W.m-1.K-1
European Workshop on New Aero Engine ConceptsMunich, 30 June – 1 July 2010
Powder Image type
TS2Cversion
Picture resolution
50% 100% 200%
Durabrade 1605
Binary CC 0.561 0.614 0.634
NF 0.852 0.725 0.701
Ternary CC 0.507 0.551 0.574
� Synthesis of the computed thermal conductivities
DurabradeGrey level
Introduction
First results(2008)
New developments
No application of the Despeckle filtering
NEWAC is an Integrated Project Co-funded by the European Commission within the Sixth Framework Programme(2002-2006) under Thematic Priority 4 Aeronautics and Space. 10
Ternary CC 0.507 0.551 0.574
NF 0.791 0.669 0.641
Metco601 NS
Binary CC 0.421 0.486 0.500
NF 0.619 0.562 0.545
Ternary CC 0.395 0.455 0.471
NF 0.593 0.537 0.518
CC stands for Cell-Centered versionNF stands for Nodal FormulationThe measured value was about 0.53 W.m-1.K-1
With Despeckle filter: 0.47 / 0.48 W.m-1.K-1 for the coatings produced with Durabrade 1605
DurabradeTernary
DurabradeBinary
New results
ConclusionsPerspectives
European Workshop on New Aero Engine ConceptsMunich, 30 June – 1 July 2010
0.400
0.600
0.800
1.000
Pre
dict
ed th
erm
al c
ondu
ctiv
ity(W
.m-1
.K-1
)
1: Measure=0.53
2: Dura_Des_OOF2
3: Dura_Des_CC
4: Dura_Des_NF
5: Dura_bin_CC
6: Dura_bin_NF
7: Dura_ter_CC
Introduction
First results(2008)
New developments
Graphical representation of the results
NEWAC is an Integrated Project Co-funded by the European Commission within the Sixth Framework Programme(2002-2006) under Thematic Priority 4 Aeronautics and Space. 11
0.000
0.200
0.400
0% 50% 100% 150% 200%
Picture resolution
Pre
dict
ed th
erm
al c
ondu
ctiv
ity(W
.m-1
.K-1
)
7: Dura_ter_CC
8: Dura_ter_NF
9: Metco_bin_CC
10: Metco_bin_NF
11: Metco_ter_CC
12: Metco_ter_NF
New results
ConclusionsPerspectives
Conclusion: Results obtained with the nodal and centered formulations tend to converge when using high resolution images or when splitting the pixels (4 cells per pixel)
European Workshop on New Aero Engine ConceptsMunich, 30 June – 1 July 2010
Introduction
First results(2008)
New developments
Example 1 of effective elasticity moduli calculated from the tensile test simulation with OOF2 for different mag nification levels and in both directions
NEWAC is an Integrated Project Co-funded by the European Commission within the Sixth Framework Programme(2002-2006) under Thematic Priority 4 Aeronautics and Space. 12
Assumed properties:EAlSi=17.5 GPa, ν=0.23Epolyester=0.75 GPa, v=0.3
New results
ConclusionsPerspectives
(1Ref ECM UTBM/WP5.4/2007/2R1)
European Workshop on New Aero Engine ConceptsMunich, 30 June – 1 July 2010
Introduction
First results(2008)
New developments
OOF2 and TS2C tend to provide similar predictions o f the effective thermal conductivity of AlSi/polyester ab radable coatings if the nodal version of TS2C is used .
The differences become noticeable if the Cell-Cente red version of TS2C is used especially for low resoluti on images .
In all cases the computed results present a converg ing
NEWAC is an Integrated Project Co-funded by the European Commission within the Sixth Framework Programme(2002-2006) under Thematic Priority 4 Aeronautics and Space. 13
New results
ConclusionsPerspectives
In all cases the computed results present a converg ing tendency with the increase in the picture resolutio n.
The development of a "split pixel" formulation contr ibuted to provide converging results (i.e. that do not vary a nymore with the picture resolution)
There is no more need to use simplified structures produced for example by applying successive Despeckle filter ing
European Workshop on New Aero Engine ConceptsMunich, 30 June – 1 July 2010
Introduction
First results(2008)
New developments
Up to now, all mechanical calculations were perform ed with OOF2 (or with ANSYS for the simulation of tests)
An in-house mechanical code based on a finite volum e approach is under development to preserve memory fo r considering large images without simplification
Comparisons will be performed with results provided with OOF2: each pixel will be considered as a cell
NEWAC is an Integrated Project Co-funded by the European Commission within the Sixth Framework Programme(2002-2006) under Thematic Priority 4 Aeronautics and Space. 14
New results
ConclusionsPerspectives Example of deformation of
a 10 cm by 10 cm steel piece for a compressive
test (amplification factor of the displacements x20)
Data: E=210 GPa, v=0.3
OOF2: each pixel will be considered as a cell