CFD for pump design: a tutorial
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Transcript CFD for pump design: a tutorial
Pump CFD - performance prediction:
a tutorial
Niels P. Kruyt
Engineering Fluid Dynamics, Department of Mechanical Engineering,
University of Twente,
P.O. Box 217, 7500 AE Enschede, The Netherlands
[email protected]
www.ts.wb.utwente.nl/kruyt/
5th International Symposium on Pumping Machinery,
2005 ASME Fluids Engineering Division Summer Meeting and Exhibition,
19-23 June, Houston, TX, USA
CFD
CFD for
for pump
pump design:
design:
Pump CFD
- performance
prediction
pitfalls
and
opportunities
a magic bullet?
Overview of tutorial
Why is fluid dynamics important for pump design?
What is Computational Fluid Dynamics (CFD)?
Opportunities provided by CFD
Components of CFD
Essential fluid dynamics
Examples of performance prediction
Trends
“Do’s” and “don’t’s” of CFD
3
Characteristics of centrifugal pumps
4
Basics of pump design/analysis
One-dimensional flow model
Euler pump relation
gH
h
r2
2
1 Q
tan 2 2b2
– Slip factor is empirical
– Hydraulic efficiency is empirical
5
What is Computational Fluid
Dynamics (CFD)?
Determination of flow:
Analytical impossible
Experiments expensive
Numerical CFD
(“computer test-rig”)
6
Benefits of CFD for pump design
Improved designs
More reliable design methods
Cheaper design process
7
Design phases
Conceptual design
Preliminary design
Detailed design
Use different CFD-methods for different design
phases!
8
Components of CFD
Model formulation
– geometry
– flow model
– boundary conditions
Grid/mesh generation
Discretisation of governing equations
Solution of discretised equations
Interpretation
9
Selection of modelled geometry
Single channel of impeller
Full pump: impeller & volute/diffusor
– steady
– unsteady
Leakage-flow region
Piping system / pump intake
Single stage vs. multi-stage
10
Turbulent flow
11
Closure problem
Averaging over time Reynolds-averaged
Navier-Stokes equations (RANS)
Contains ‘Reynolds stresses’
uv
Extra quantities in equations ‘closure’
problem
Model required for Reynolds stresses in terms
of time-averaged velocities u, v
12
Turbulence models
Mixing-length model
k-e models (k-w
Reynolds-stress models
“Turbulent viscosity”
u
T l
y
T c k 2 e
2
m
Increasing complexity
turb,xy
u
uv T
y
Pope (2000); Bradshaw (1996)
13
Flow models
Stream-surface methods
Potential-flow model
Euler flow model
RANS-based models
Large-eddy simulations (LES)
Direct Navier-Stokes simulations (DNS)
Increasing complexity
14
Boundary layers
High Reynolds numbers
Main flow is inviscid
Boundary-layer flow is
viscous
Boundary-layer is thin
Large variation of velocity
in direction normal to wall
Re = 107:
L = 25 cm; d = 0.4 cm
L = 9.8 in; d0.1in
15
Logarithmic layer
Large variation of velocity
perpendicular to wall
many grid points
‘Universal’ behaviour near
wall “logarithmic layer”
“Wall functions” in RANSbased CFD-methods
boundary conditions
u
1
ln y B
Craft et al. (2002); Pope (2000)
16
Separation
Attached boundary-layer
Separated boundary-layer
17
Grid/mesh (1)
Structured
Unstructured
18
Viscous accuracy
Grid/mesh (2)
Structured
multi-block
Unstructured
Ease of use
Baker (2005)
19
Discretisation
Replace partial differential equations by a finite
set of equations
– Finite difference method
– Finite volume method
– Finite element method
Discretisation error
solution depends on grid/mesh size!
20
Sources of errors
in CFD-predictions
Modelling errors
– Geometrical uncertainties
– Limited validity of adopted flow model
– Uncertain boundary conditions
Numerical errors
– Discretisation error due to finite grid-size
– Lack of convergence in iterative solution process
– Insufficient mesh/grid quality
User/programmer errors
21
‘Around’ design
point
Cost
Choice of flow model
DNS
RSM
k, e
Potential
& B.L.
Potential
1D
Accuracy
22
Performance prediction with
potential-flow model
0.13
0.13
0.13
100
100
100
0.11
0.11
0.11
9090
90
0.09
0.09
0.09
YY
Y
0.07
0.07
0.07
8080
80
experiments
experiments
experiments
experiments
inviscid
inviscid
'' + leakage flow
experiments
inviscid
'''' ++ leakage
flow
disk friction
inviscid
'' + leakage flow
hydr.friction
losses
'''' ++ disk
7070
70
0.05
0.05
0.05
6060
60
0.03
0.03
0.03
4040
40
5050
50
4040
40
6060
60
8080
80
100
120
100
120
100
120
QQ[%BEP]
[%BEP]
Q [%BEP]
140
140
140
160
160
160
6060
60
8080
80
100 120
120
100
100
120
QQ[%BEP]
[%BEP]
Q [%BEP]
140
140
140
160
160
160
van Esch & Kruyt (2001)
23
Inviscid-viscous interaction methods
Outer flow inviscid flow equations
Boundary-layer flow boundary-layer equations
Coupled solution mildy separated flows
RAE101 wing
Milewski (1997)
24
Comparison of RANS-predictions
Different machines
Many contributors
Draft tube
Wing/body
25
Turbine draft tube
Turbine draft tube flow;
Engström et al. (2001)
Pressure recovery (local)
Loss coefficient (average)
0.2
1.8
Experimental
0.15
1.4
z
cp
1.6
0.1
1.2
0.05
1
0
1
2
3
4
5
6
7
Contributor
8
9
10 11
1
2
3
4
5
6
7
8
9
10 11
Contributor
26
Wing/body
DLR F6 wing/body study
Baker (2005)
27
Differences CFD
pump aerospace applications
Compressibility effects are absent; no shock waves
Cavitation is important
Rotating/stationary parts
More boundary layers need to be resolved
Flow separation more important for off-design
conditions
Effect rotation and curvature on turbulence
28
Implementation of CFD
in pump-design process
Integrate CFD in all design phases
Different CFD-models for each design phase
Simple models give more insight
Tune model parameters from database
RANS-methods require intense use
Set accuracy targets clearly
Be cautious of designs from CFD that deviate strongly
from experience
29
Trends
Maturing of commercial/general-purpose CFD-packages
Main problem remains turbulence modelling
Multi-phase CFD-methods
Adaptive mesh refinement
Open-source CFD-methods (“GNU-CFD”)
Verification of CFD-methods “blind” tests
Design-oriented CFD-methods
– Optimisation methods
– Inverse-design methods
30
Inverse-design method
Specified
– meridional plane
– duty
– “blade loading”
Obtained
– Blade angles
Westra et al. (2005)
[Click on figure to start movie]
31
“Don’t’s” of CFD
Use CFD-package as a black-box tool
Forget that turbulence needs to be modelled
Use RANS-methods for all design phases
32
“Do’s” of CFD
Choose right tool for the task
Analyse and interpret results
Use common-sense
Use/develop knowledge of fluid dynamics
Check grid/mesh convergence
Check sensitivity of results to model parameters
33
Conclusions
CFD is not a “magic bullet”
CFD is a powerful tool
Many pitfalls; many opportunities
CFD does not replace a smart designer
CFD provides great potential for improved
pump-design process
CFD is (still) an art
34
Questions and comments
Thank you for your attention!
Questions and comments?
Presentation can be downloaded from:
www.ts.wb.utwente.nl/kruyt/asme2005.pps
E-mail:
[email protected]
35
Literature
Baker, T.J. (2005). “Mesh generation: art or science”, Progress in Aerospace Sciences 41 29-63.
Craft, T.J. & Gerasimov, A.V. & Iacovides, H. & Launder, B.E. (2002). “Progress in the generalization of wallfunction treatments”, International Journal of Heat and Fluid Flow 23 148-160.
Bradshaw, P. (1996). “Turbulence modelling with application to turbomachinery”, Progress in Aerospace
Sciences 32 575-624.
Engström, T.F. & Gustavsson, L.H. & Karlsson, R.I. (2001). “Proceedings of Turbine 99 – Worskshop 2. The
second ERCOFTAC Workshop on draft tube flow”, http://www.sirius.luth.se/strl/Turbine-99/.
Esch, B.P.M. van & Kruyt, N.P. (2001). “Hydraulic performance of a mixed-flow pump: unsteady inviscid
computations and loss models”, Journal of Fluids Engineering 123 256-264.
Jameson, A. (2001). “A perspective on computational algorithms for aerodynamic analysis and design”,
Progress in Aerospace Sciences 37 197-243.
Milewski, W.M. (1997). “Three-dimensional viscous flow computations using the integral boundary-layer
equations simultaneously coupled with a low-order panel method”, Ph.D. Thesis, MIT, Cambridge, USA.
Westra, R.W. & Kruyt, N.P. & Hoeijmakers, H.W.M. (2005). “An inverse-design method for centrifugal pump
impellers”, 2005 ASME 5th International Symposium on Pumping Machinery, Paper FEDSM2005-77283.
Pope, S.B. (2000). “Turbulent flows”, Cambridge University Press, Cambridge, UK.
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Notes
37