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V.M. Goloviznin, M.A. Zaitsev, S.A. Karabasov
Mathematical modelling of
unsteady problems of mechanics
of continua using the CABARET
method in OpenFOAM framework
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Contents:
- Mathematical modelling of unsteady problems using the
CABARET(case for elastic media)
- Development of unified algorithms of fluid-structure
interaction problem solution including acoustics applictions
- Calculation results including hybrid hexa & tetra mesh
Problem solved:
- unsteady backstep flow
- unsteady t-junction flow
- unsteady jet flow of mixing multicomponent gas
- unsteady acoustic emission of oscillating beam
Mathematical modelling of unsteady problems of
mechanics of continua using the CABARET method in
OpenFOAM framework
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xyxx xz
xy yy yz
yzxz zz
u
t x y z
v
t x y z
w
t x y z
- density; u, v, w velocity components; x, y, z
coordinates; ij–componets of Cauchy stress tensor.
OpenFOAM formulation for time step dt2:
u=u-dt2*fvc::surfaceIntegrate(ss & mesh.Sf())/Rofon;
ss - stress tensor defined at faces(surfaceTensorField ss);
Rofon – density
mesh.Sf() – face vector
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2
2
2
xx
yy
zz
xy
xz
yz
u u v w
t x x y z
v u v w
t y x y z
w u v w
t z x y z
u v
t y x
u w
t z x
v w
t z y
- Lame constans of elastic media;
OpenFOAM formulation for time step dt2:
volTensorField gradU = fvc::surfaceIntegrate(us*mesh.Sf());
s=s-dt2*(2.0*mu*symm(gradU)+lambda*I*tr(gradU));
s – stress tensor in cells;
us - velocity vector in faces(surfaceVectorField us);
lambda, mu – Lame constans
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Plane problem in X direction
1 10 0 0 0 0 0 0 0
1 10 0 0 0 0 0 0 0
2 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0
0 0 0 0 0 2 0 0 0
xx xx xx
xy xy xy
yy yy yy
u u u
v v v
t x y
0
10 0 0 0
10 0 0 0
det 0
2 0 0 0 0
0 0 0 0
0 0 0 0
5 3
2
1 1( 3 ) ( 2 ) 0
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1
1
2
2
xx
xx
xy
xy
I uc
I uc
J vc
J vc
Eigen values are equal positive and negative values of
longitudinal and transverse wave velocity. Zero eigen value
is for Y-direction stress invariant.
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OpenFOAM formulation:
Time loop
Phase 1;
Phase 2;
Phase 3;
Loop end
Phase 2 is external function.
Boundaries are OpenFOAM
codedMixed type.
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6
1
6
1
2
1
xx xy xz x
xy yy yz y
k
xz yz zz znew
x y z
k
u u St
v v SV
w w S
u u u
x y zu
v v vv S S S
x y z Vw
w w w
x y z
2
22
2
xx xx
xy xy
xz xz
yy yy
yz yz
zz zznew
u v w
x y z
u
x
u v
y x
u w
z xt
v
y
v w
z y
w
z
V – cell volume, Δt – time step.
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max
min
max max
min max
min min
max( , , ) 2( ) ( )
min( , , ) 2( ) ( )
2
2 2
2
b cb csb cb b
b cb csb cb b
csb b
new
csb b csb b
csb b
tI I I I I I с I I
l
tI I I I I I с I I
l
I I I I
I I I I I I I
I I I I
max
min
max max
min max
min min
max( , , ) 2( ) ( )
min( , , ) 2( ) ( )
2
2 2
2
f cf csf cf f
f cf csf cf f
csb b
new
csf f csb b
csb b
tI I I I I I с I I
l
tI I I I I I с I I
l
I I I I
I I I I I I I
I I I I
c – invariant value, l – distance
to opposite face, indices b и f
are for backward and forward
face invariant value, сb и сf are
for backward and forward cell
invariant value, сsb и сsf are
for backward and forward cell
invariant value on intermediate
time step.
New velocity values –half summ of invariants with indices “+” and
“-”. Stresses – half difference, multiplied by factor ρc.
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Linear compressible fluid
p=p-dt2*rss*fvc::surfaceIntegrate(mesh.Sf() & us);
u=u-dt2*fvc::surfaceIntegrate((mesh.Sf() & us)*us+ps*mesh.Sf()/Rofon)
+dt2*fvc::laplacian(nu, u)+g*dt2*t;
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Linear compressible fluid
p=p-dt2*rss*fvc::surfaceIntegrate(mesh.Sf() & us);
t=t-dt2*fvc::surfaceIntegrate((mesh.Sf() & us)*ts)
+dt2*fvc::laplacian(kappa, t);
u=u-dt2*fvc::surfaceIntegrate((mesh.Sf() & us)*us+ps*mesh.Sf()/Rofon)
+dt2*fvc::laplacian(nu, u)+g*dt2*t;
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Ideal gas
r=r-dt2*fvc::surfaceIntegrate(rnews*(mesh.Sf() & unews));
e=(e*r-dt2*fvc::surfaceIntegrate((mesh.Sf() &
unews)*(rnews*Cv*tnews+pnews)))/r
u=(u*r-dt2*fvc::surfaceIntegrate((mesh.Sf() &
unews)*unews*rnews+pnews*mesh.Sf()))/r
+dt2*fvc::laplacian(nu, u);
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Multicomponent ideal gas
rnew=r-dt2*fvc::surfaceIntegrate(rnews*(mesh.Sf() & unews));
hnew=h-dt2*fvc::surfaceIntegrate(hnews*(mesh.Sf() & unews));
wnew=w-dt2*fvc::surfaceIntegrate(wnews*(mesh.Sf() & unews));
unews)*rnews*enews))/rnew
enew=(e*r-dt2*fvc::surfaceIntegrate((mesh.Sf() & unews)*(((rnews-hs-
ws)*Cva+Cvh*hs+Cvw*w
dt2*fvc::laplacian(kappa, ((r-h-w)*Cva+Cvh*h+Cvw*w)*t))/r;
unew=(u*r-dt2*fvc::surfaceIntegrate((mesh.Sf() &
unews)*unews*rnews+pnews*mesh.Sf()))/rnew
+dt2*fvc::laplacian(nu, u)+g*dt2;
pnew=((Cph-Cvh)*hnew+(Cpw-Cvw)*wnew+(Cpa-Cva)*(rnew-hnew-
wnew))/
(Cvh*hnew+Cvw*wnew+Cva*(rnew-hnew-wnew))
*rnew*(enew-mag(unew)*mag(unew)/2);
<------>tnew=pnew/((Cph-Cvh)*hnew+(Cpw-Cvw)*wnew+(Cpa-
Cva)*(rnew-hnew-wnew));
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Elastic media
volTensorField gradU = fvc::surfaceIntegrate(us*mesh.Sf());
s=s-dt2*(2.0*mu*symm(gradU)+lambda*I*tr(gradU));
u=u-dt2*fvc::surfaceIntegrate(ss & mesh.Sf())/Rofon;
Left and right ends of beam are fully constrained. Uniform
pressure is applied at top surface.
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Beam has uniform horizontal velocity of
value 0.1 m/sec at initial time.
OpenFOAM data structure
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V.M. Goloviznin, M.A. Zaitsev and S.A.
Karabasov, "A highly scalable hybrid mesh
CABARET MILES method for MATIS-H
problem," Proc. of the CFD4NRS-4
WORKSHOP, p. 104, Daejon, South Korea
(2012).
Parallel computations were made on mesh
up to 40 millions cells on 4096 processors
cores.
Program Program name Problem Processor core
number Cell
number Operating
speed
Linear
compressible fluid rhoCabaretFoam t-junction 64 231517 9.95243373
Ideal gas gasCabaretFoam jet flow 32 400000 16.7
Elastic media solidCabaretFoam beam vibration 1 1000 7.5
Multicomponent
gas mixingCabaretFoa
m multicomponent
jet 32 9588 50
Fluid structure
interaction fsiCabaretFoam
acoustic
emission of
oscillating beam 1 26600 34.54
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Opposite face value is only for hexa cell. To make uniform
computations it needs to define fictive opposite face value.
Gorbachev D.J., “Adaptation of Cabaret method for abitrary mesh
cells”, //Scientific conference “Tichonovskie chtenija”, Moscow State
University, Moscow, Oct. 2017.
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1. CABARET method realization in OpenFOAM framework for
linear compressible fluid, ideal gas and elastic media have
the same unique features that differentiate it from the
another realizations.
2. CABARET method realization in OpenFOAM framework for
linear compressible fluid structure interaction allows to
create new uniform numerical algorithm with high quality
computations including interface regions.
3. Operating speed in OpenFOAM framework is compatible with
the same FORTRAN version of programs. Parallel numerical
algorithms have parallel cluster scalability.
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