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LAMINAR THERMAL MIXING IN PLANE SHEAR FLOWLAMINAR THERMAL MIXING IN PLANE SHEAR FLOW
A. Haas1, M. Scholle1, H.M. Thompson2, R.W. Hewson2, N. Aksel1, P.H. Gaskell2
1University of BayreuthDepartment of Applied Mechanics and Fluid Dynamics
D-95440, Bayreuth, Germany
2University of LeedsEngineering Fluid Mechanics Research GroupEngineering Fluid Mechanics Research Group
School of Mechanical EngineeringLeeds, LS2 9JT, UK
Presented at the COMSOL Conference 2009 Milan
Problem formulationProblem formulation
• Two-dimensional • Sinusoidally corrugated substrateTwo dimensional• Steady• Periodic BC
Sinusoidally corrugated substrate• Constant , cp and
Parameters:• Wavelength:
T0• Wavelength: • Amplitude: • Mean gap width: • Lid velocity: u0
A
H T1y 0
• Temperature: T1>T0• Viscosity:
(T ) 0 1
*T
A. Haas, M. Scholle, R.W. Hewson, H.M. Thompson, N. Aksel, P.H. Gaskell
Non-dimensional model equationsNon-dimensional model equations
Continuity equation:
No buoyancy and no dissipationSimplifications:
0x zu w
* *Re 2 1 1x z x x x z z xuu wu p T u T u w
y q
Navier-Stokes equations:
x z
* *Re 2 1 1x z z z z x z xuw ww p T w T u w
Pe 0x z xx zzuT wT T T Temperature equation: x z xx zz
0 00 0Re Pe pu cu
p q
Dimensionless numbers:
A. Haas, M. Scholle, R.W. Hewson, H.M. Thompson, N. Aksel, P.H. Gaskell
0
Re Pe2 2
Methods of solutionMethods of solution
• Semi-analytical approach• Based on a variational formulation• Stokes flow limit Re 0• neglect of thermoviscosity coupling term
• Finite element methodsComsol® Multiphysics modules• Incompressible Navier-Stokesp• Heat transfer/convection
A. Haas, M. Scholle, R.W. Hewson, H.M. Thompson, N. Aksel, P.H. Gaskell
Stokes flow – equation setStokes flow – equation set
U il t ll l d t f tiUnilaterally coupled set of equations:
• Hydrodynamic field:
000
x z
x xx zz
u wp u u
u(x,a cos x) 0w(x,a cos x) 0
u(x, h) 10z xx zzp w w
( )w(x, h) 0
( , cos ) 1T x a x • Temperature field
di i l Pe 0x z xx zzuT wT T T
( , cos ) 1( , ) 0
T x a xT x h
Decoupling:
a: non-dimensional amplitude
h: non-dimensional gap-width
A. Haas, M. Scholle, R.W. Hewson, H.M. Thompson, N. Aksel, P.H. Gaskell
1) Isothermal flow 2) Heat conduction with convection
Stokes flow - HydrodynamicsStokes flow - Hydrodynamics
Lubrication approximation
Analytic solution for the assumption a 1
Finite element solution Lubrication approximation
Reasonable results even for moderate amplitudes 1a
A. Haas, M. Scholle, R.W. Hewson, H.M. Thompson, N. Aksel, P.H. Gaskell
p 1a
Stokes flow - Heat conduction & convectionStokes flow - Heat conduction & convection
Variational formulation: with non-local functional:0I
cos
: Pe ( , ) ( , ) ( , ) ( , ) d dh
a x
I T x z u T z T x z T z zx x x
Reproduces the heat conduction equation with convection:
Pe 0x z xx zzuT wT T T
Solution by Ritz‘s direct method with appropriate base functions.
A. Haas, M. Scholle, R.W. Hewson, H.M. Thompson, N. Aksel, P.H. Gaskell
Stokes flow - Temperature fieldStokes flow - Temperature fieldSemi-analytical solution Finite element solution
a 1 / 2h 3 / 4
Streamlines:
A. Haas, M. Scholle, R.W. Hewson, H.M. Thompson, N. Aksel, P.H. Gaskell
Stokes flow - Global heat transferStokes flow - Global heat transfer
Nusselt number vs. Peclét number
2 1Nu hQ
T T
0Pe2
pc u
a 1 / 2h 3 / 5h 3 / 5
Nu a 1 / 2h 3 / 4
a 1 / 2h 1
a 1 / 2
A. Haas, M. Scholle, R.W. Hewson, H.M. Thompson, N. Aksel, P.H. Gaskell
Pe
h 7 / 4
Stokes flow - Thermal feedbackStokes flow - Thermal feedback
*0( ) 1T T Thermoviscosity:
* 0
Hydrodynamic streamlines: Temperature field:
* 1 3
* 1 3
a 1 / 2
A. Haas, M. Scholle, R.W. Hewson, H.M. Thompson, N. Aksel, P.H. Gaskell
h 3 / 4Pe 100
Inertial effects – Flow structureInertial effects – Flow structureRe 0 Re = 100
a 1 / 2h 7 / 4
a 1 / 2h 1
a 1 / 2h 3 / 4
a 1 / 2h 3 / 5
A. Haas, M. Scholle, R.W. Hewson, H.M. Thompson, N. Aksel, P.H. Gaskell
h 3 / 5
Pe 100
Inertial Effects – Global Heat TransportInertial Effects – Global Heat Transport
a 1 / 2a 1 / 2h 3 / 5
Nu a 1 / 2Nu a 1 / 2h 3 / 4
a 1 / 2
a 1 / 2h 1
A. Haas, M. Scholle, R.W. Hewson, H.M. Thompson, N. Aksel, P.H. Gaskell
Pe
h 7 / 4
ConclusionsConclusions
• Stokes flow limit: Re 0 Global Heat transfer: Comparison between semi-analytical and finite element solution Influence of thermoviscosity
• Inertial effects on global heat transfer Competing kinematical and inertial effects.
A. Haas, M. Scholle, R.W. Hewson, H.M. Thompson, N. Aksel, P.H. Gaskell
PublicationsPublications
Available literature:
M. Scholle, A. Haas, R.W. Hewson, H.M. Thompson, P.H. Gaskell, N. Aksel, The effect of locally induced flow structure on global heat transfer for plane laminar shear flow. Int. J. Heat & Fluid Flow 30 175-185 (2009)& Fluid Flow 30, 175-185 (2009).
M. Scholle, A. Haas, M.C.T. Wilson, H.M. Thompson, P.H. Gaskell, N. Aksel, Eddy genesis and manipulation in plane shear flow. Phys. Fluids 21, 073602 (2009).
A. Haas, M. Scholle, R.W. Hewson, H.M. Thompson, N. Aksel, P.H. Gaskell