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MRFZonesC questions what is the mesh_V and why only Coriolis force no centrifugal force

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Old   April 1, 2008, 02:09
Default hi every one! i have some
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hi every one!
i have some question about MRFZones.C
in void Foam::MRFZone::addCoriolis(fvVectorMatrix& UEqn) const:

Quote:
const labelList& cells = mesh_.cellZones()[cellZoneID_];
const scalarField& V = mesh_.V();Q1:what is the mesh_.V()?
....

forAll(cells, i)
\ {
Usource[cells[i]] -= V[cells[i]]*(Omega ^ U[cells[i]]);
Q2:here coriolis force is equal to "omega u",but i think it should be "1/2 * omega u" and also there is no centrifugal force which is "omega(omegar)",so if i want to calculate the flow in the turbins? would i need to modify the them both?
}
thanks
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Old   April 1, 2008, 07:12
Default Hi Wayne, I think that in an
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Hi Wayne,
I think that in an absolute velocity formulation, the Coriolis force (2rwxU_relative) and centripet force (rwxwxr) can be written as: rwxU

I hope this is helpful,
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Old   April 1, 2008, 07:13
Default ...and mesh_.V() retuns the ce
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...and mesh_.V() retuns the cell volume
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Old   April 1, 2008, 10:17
Default Hi Dragos: i don` think so.
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Hi Dragos:
i don` think so.if we write the moment equ in rotating frame, the velocity is relative velocity (W),and in the absolute frame the equation is without the coriolis force and centrifugal force.
in MRF:

rho*D(W_relative)/Dt=F(total,including pressure,viscosity)+omega(omegar)-2* omega u


in absolute frame:
rho*D(U_absolute)/Dt =F

according to you should be

rho*D(U_aboslute)/dt= F+ * omega U

i dont think it will be
rho*D(W_aboslute)/dt= F+ * omega U

for the solver just treat one velocity not two

thanks alot
yours wayne
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Old   April 1, 2008, 10:20
Default i am sorry, there is a "*" be
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i am sorry, there is a "*" before "omega U" for last two equ.it is typing error of mine

thanks
wayne
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Old   April 2, 2008, 02:22
Default I had a vague memory in the ba
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I had a vague memory in the back of my mind when I wrote the above post, but I've just dug for it and here it is...

In the absolute velocity formulation and for a steadily rotating frame the flow equations can be written as follows:
- continuity:
- momentum:
- energy:
where the relative velocity is:
and the transport velocity is:

You can also check the fluent user manual for it.

I hope this is helpful,
Dragos
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Old   April 2, 2008, 04:29
Default Hi Dragos thanks a lot! i
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Hi Dragos
thanks a lot!
i could understand it now!
the relative velocity is as calculating in the memeber function relativeflux,so moment eqution should be div(phi,u),is that right?

thanks
waye
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Old   April 2, 2008, 04:40
Default Hi Wayne, This is exactly wha
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Hi Wayne,
This is exactly what it is written in the momentum predictor:


tmp<fvvectormatrix> UEqn
(
<blockquote>fvm::div(phi, U)
+ turbulence->divR(U)
);
</blockquote>

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Old   April 3, 2008, 00:08
Default Hi Dragos but why the flow p
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Hi Dragos
but why the flow pattern of the result looks like U is relative velocity

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Old   April 3, 2008, 01:09
Default well Wayne, if it is like that
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well Wayne, if it is like that I agree with you: it is strange.
Can you post a picture with an example?

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Old   April 3, 2008, 02:41
Default Hi dragos the result of mixv
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Hi dragos
the result of mixvessl2D in tut looks likes the U is absolute velocity

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Old   April 3, 2008, 02:57
Default http://www.cfd-online.com/Open
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Old   April 3, 2008, 03:18
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Old   April 3, 2008, 03:19
Default http://www.cfd-online.com/Open
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Old   April 3, 2008, 03:35
Default Hi sorry i try a lot here i
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Hi sorry
i try a lot
here is the result of mixvessl2D(vector on the rotor),you can see clearly the velocity profile relative to the omega

and then is my case a 3d centrifugal impeller
a vector plot of U in the impeller z=1/2thick

b vector plot on the blade

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Old   April 3, 2008, 03:44
Default mix2d http://www.cfd-online.c
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mix2d

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Old   April 3, 2008, 03:49
Default http://www.cfd-online.com/Open
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Lots of tries!
Well in the picture I can see, the vectors look ok to me!
Be careful to have pictures with dimensions of less than 50kb.

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Old   April 3, 2008, 03:50
Default a vector plot of U in the impe
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a vector plot of U in the impeller z=1/2thick

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Old   April 3, 2008, 03:58
Default b vector plot on the blade ht
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b vector plot on the blade

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Old   April 3, 2008, 03:59
Default c relative velocity (at the s
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c relative velocity (at the same conditon) calculated by CFX

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