[Nek5000-users] Pipe with expansion

nek5000-users at lists.mcs.anl.gov nek5000-users at lists.mcs.anl.gov
Fri Jan 31 08:10:48 CST 2014


Hi Neks,

I tried to simulated steady flow by setting the logical operator IFTRAN 
= F but the simulation still runs in transient mode, How do I get a 
steady time independent solution so that I can use it as my Initial 
Condition ?

Thank you,
Kamal


On 29/01/2014 16:01, nek5000-users at lists.mcs.anl.gov wrote:
> Hello Paul,
>
> Thanks for the vorticity output and it worked.
>
>
> 1) I created a set-obj() for my pipe but how can I be sure that it has 
> taken the full pipe wall surface in to account ?
>     I have attached the divpipe.usr file for your reference could you 
> please take a look at it.
>
> 2) I even took torque_calc in to the .usr file and it gives out 
> something like this
>
>      200  1.00000000000E+00 -9.76942759878E-06 -8.98721249598E-06 
> -7.82215102801E-07      1torqx
>      200  1.00000000000E+00 -6.69169235606E-06 -6.35251009840E-06 
> -3.39182257669E-07      1torqy
>      200  1.00000000000E+00  9.50518561890E-10  1.50349344990E-13 
> 9.50368212545E-10       1torqz
>
> if I am not wrong are these the value of surface integral of viscous 
> force in three components of velocity along three directions taken in 
> the set_obj() ?
>
> because I would like to calculate this
>
> C_v =  F^v / ( d^2 * rho * U^2 ) =   double integral ( 1/Re * (du / 
> dr) ) dtheta dz
>
>
> Thank you,
>
> Kamal.
>
>
> On 24/01/2014 13:02, nek5000-users at lists.mcs.anl.gov wrote:
>>
>>
>>
>> Kamal,
>>
>> 1) yes
>>
>> 2) standard approach to seeing vorticity would be something
>>    like the following in userchk
>>
>>      parameter (lt=lx1*ly1*lz1*lelt)
>>      common /myjunk/ vort(lt,3),w1(lt),w2(lt)
>>      logical ifxyt
>>      integer ivout  ! flag to turn geometry on/off for VisIt
>>      save    ivout
>>      data    ivout /0/
>>
>>
>>      if (mod(istep,iostep).eq.0) then
>>         call comp_vort3(vort,w1,w2,vx,vy,vz)
>>
>>         ifxyt = ifxyo   ! put geometry into first vrt file
>>         ifxyo = .false.
>>         if (ivout.eq.0) ifxyo = .true.
>>         ivout = 1
>>
>>         call outpost(vort(1,1),vort(1,2),vort(1,3),pr,t,'vrt')
>>
>>         ifxyo = ifxyt   ! restore ifxyo flag to original state
>>
>>      endif
>>
>>
>> If your session name is blah, this piece of code will put
>> vorticity into a sequence of files vrtblah0.f0000n
>>
>> You can instead ignore the vrt prefix and the part about the
>> geometry with a simpler code
>>
>>      parameter (lt=lx1*ly1*lz1*lelt)
>>      common /myjunk/ vort(lt,3),w1(lt),w2(lt)
>>
>>      if (mod(istep,iostep).eq.0) then
>>         call comp_vort3(vort,w1,w2,vx,vy,vz)
>>         call outpost(vort(1,1),vort(1,2),vort(1,3),pr,t,'vrt')
>>      endif
>>
>> I usually go for this latter approach, but the choice is
>> totally up to you.
>>
>> Paul
>>
>>
>>
>>
>>
>> On Fri, 24 Jan 2014, nek5000-users at lists.mcs.anl.gov wrote:
>>
>>> Hello Paul,
>>>
>>> Thanks for your reply. I am looking into the .usr file for defining 
>>> the set_obj ().
>>>
>>> 1) Could you please tell me what is 'Enter the number of levels ?' 
>>> in n2to3
>>>
>>> is it the number of elements in Z direction ?
>>>
>>> 2) As you said about storing the computed vorticity in velocity 
>>> field to view in VisIT, I found the routine to compute the vorticity 
>>> but I am stuck about adding it to the velocity filed to VisIT ? 
>>> could you please tell me how it works or any example which stores 
>>> vorticity to the .fld file as a separate variable.
>>>
>>>
>>> Thank you
>>>
>>> Kamal
>>>
>>>
>>> On 22/01/2014 16:53, nek5000-users at lists.mcs.anl.gov wrote:
>>>> Axial viscous stress is given by torq_calc -- that's no problem 
>>>> whatsoever. You get a number as a
>>>> function of time.
>>>>
>>>> You can even get stresses on multiple subsets of the geometry 
>>>> (e.g., if you had multiple branches
>>>> in the domain or multiple cylinders.   The drag, which is a 
>>>> byproduct of the torque computation (which
>>>> you can ignore), is given in terms of the viscous and pressure 
>>>> components separately and as the
>>>> sum of the two.
>>>>
>>>> You can identify domain boundaries by checking the boundary 
>>>> conditions. Here, I recommend
>>>> looking at the set_obj routines in several of the /example cases.
>>>>
>>>>
>>>> ________________________________________
>>>> From: nek5000-users-bounces at lists.mcs.anl.gov 
>>>> [nek5000-users-bounces at lists.mcs.anl.gov] on behalf of 
>>>> nek5000-users at lists.mcs.anl.gov [nek5000-users at lists.mcs.anl.gov]
>>>> Sent: Wednesday, January 22, 2014 9:37 AM
>>>> To: nek5000-users at lists.mcs.anl.gov
>>>> Subject: Re: [Nek5000-users] Pipe with expansion
>>>>
>>>> Hello Paul
>>>>
>>>> I was thinking about taking the tangential velocity near to the 
>>>> wall so that I can figure out my length of the recirculation region.
>>>>
>>>> Is it possible for me to access the boundary elements of the mesh 
>>>> ??? so that I can take the boundary element and then obtain the 
>>>> velocity at that point so that I can figure out the length of my 
>>>> recirculation region.
>>>>
>>>> or take the *.fld file and read it to plot the datas I need.
>>>>
>>>>
>>>> I also want to calculate the axial viscous force acting on the 
>>>> entire pipe.
>>>>
>>>> which is given by
>>>>
>>>> C_v =  F^v / ( d^2 * rho * U^2 ) =   double integral ( 1/Re * (du / 
>>>> dr) ) dtheta dz
>>>>
>>>>
>>>> On Jan 22, 2014, at 4:07 PM, nek5000-users at lists.mcs.anl.gov wrote:
>>>>
>>>>> Hi Kamal,
>>>>>
>>>>> As I thought about it some more, if you're interested in the local 
>>>>> wall shear stress
>>>>> magnitude I'm quite certain you can get this by plotting the 
>>>>> magnitude of vorticity
>>>>> on the surface in question.   (Note that the sign of the WSS, 
>>>>> which in fact is a tensor
>>>>> or a vector when restricted to a given surface, is lost in this 
>>>>> process, but that might
>>>>> not be relevant for your needs.)   If that works, then you can 
>>>>> readily compute the
>>>>> vorticity using one of the routines in nek and store the result in 
>>>>> a velocity field, then
>>>>> view that field with VisIt.   Of course WSS will require 
>>>>> multiplication by viscosity.
>>>>>
>>>>> hth,
>>>>>
>>>>> Paul
>>>>>
>>>>> ________________________________________
>>>>> From: nek5000-users-bounces at lists.mcs.anl.gov 
>>>>> [nek5000-users-bounces at lists.mcs.anl.gov] on behalf of 
>>>>> nek5000-users at lists.mcs.anl.gov [nek5000-users at lists.mcs.anl.gov]
>>>>> Sent: Tuesday, January 21, 2014 10:33 AM
>>>>> To: nek5000-users at lists.mcs.anl.gov
>>>>> Subject: Re: [Nek5000-users] Pipe with expansion
>>>>>
>>>>> Hi paul,
>>>>>
>>>>> can I make this to be drag or shear quantities to be return to the a
>>>>> separate file so that it will easy for me to plot.
>>>>>
>>>>> By the way it gives the integral quantity. Think for example I 
>>>>> need to
>>>>> find the shear stress on the wall  from the inlet to outlet at a
>>>>> particular time = 2 . How can I do that ?
>>>>>
>>>>> Is there way to find the number of elements in x,y and z direction ?
>>>>>
>>>>> On 21/01/2014 17:32, nek5000-users at lists.mcs.anl.gov wrote:
>>>>>> Hi Kamal,
>>>>>>
>>>>>> Your integrated drag quantities should be written to the logfile
>>>>>> (stdout),
>>>>>> assuming you've set the arguments in the call to be .true.
>>>>>>
>>>>>> Paul
>>>>>>
>>>>>> On Tue, 21 Jan 2014, nek5000-users at lists.mcs.anl.gov wrote:
>>>>>>
>>>>>>> Hi Paul,
>>>>>>>
>>>>>>> I checked the set_obj subroutine and implemented one in my .USR 
>>>>>>> file.
>>>>>>> The code seem to run without any errors but I don't find where 
>>>>>>> these
>>>>>>> variables are getting stored.
>>>>>>>
>>>>>>> I use VisIT to visualize my output, even there was no change in it.
>>>>>>>
>>>>>>> do I have to define my own output file and write the variables 
>>>>>>> out ?
>>>>>>>
>>>>>>> Thanks,
>>>>>>>
>>>>>>> Kamal.
>>>>>>>
>>>>>>>
>>>>>>> On 20/01/2014 21:52, nek5000-users at lists.mcs.anl.gov wrote:
>>>>>>>> Hi Kamal,
>>>>>>>>
>>>>>>>> You'll need to compute your own tke by manipulating the
>>>>>>>> velocity fields.
>>>>>>>>
>>>>>>>> You can get running averages of the requisite quantities
>>>>>>>> via calls to "avg_all" which is found in navier5.f
>>>>>>>>
>>>>>>>> You can compute shear stress on the wall simply by computing
>>>>>>>> the drag on the wall, which can be done via a call to 
>>>>>>>> torque_calc(),
>>>>>>>> also found in navier5.f
>>>>>>>>
>>>>>>>> If you cd to /examples and type:
>>>>>>>>
>>>>>>>>       grep torq */*.usr
>>>>>>>>
>>>>>>>> you'll find many examples of calls to torque_calc. You simply
>>>>>>>> need to prescribe the surfaces on which shear is to be integrated.
>>>>>>>>
>>>>>>>> I typically write a routine "set_obj" to identify such surfaces
>>>>>>>> on the first call to usrchk.
>>>>>>>>
>>>>>>>>       grep set_obj */*.usr
>>>>>>>>
>>>>>>>> will show similar examples.
>>>>>>>>
>>>>>>>> I would recommend trying this for laminar Poiseiulle flow in
>>>>>>>> a very simple channel just to check that your calls are properly
>>>>>>>> set.
>>>>>>>>
>>>>>>>> Best,
>>>>>>>>
>>>>>>>> Paul
>>>>>>>>
>>>>>>>>
>>>>>>>> On Mon, 20 Jan 2014, nek5000-users at lists.mcs.anl.gov wrote:
>>>>>>>>
>>>>>>>>> Hi Paul,
>>>>>>>>>
>>>>>>>>> Thanks and that helped.
>>>>>>>>>
>>>>>>>>> Where can I find the variables like Turbulent KE , shear 
>>>>>>>>> stress on
>>>>>>>>> the wall. ?
>>>>>>>>>
>>>>>>>>> Do i have to activate some parameters for calculating them ?
>>>>>>>>>
>>>>>>>>> If I had to plot them.
>>>>>>>>>
>>>>>>>>> Thanks,
>>>>>>>>> Kamal
>>>>>>>>>
>>>>>>>>>
>>>>>>>>> On Jan 20, 2014, at 5:41 AM, nek5000-users at lists.mcs.anl.gov 
>>>>>>>>> wrote:
>>>>>>>>>
>>>>>>>>>> Kamal,
>>>>>>>>>>
>>>>>>>>>> Looks good.
>>>>>>>>>>
>>>>>>>>>> I'm guessing that one further refinement would be:
>>>>>>>>>>
>>>>>>>>>> if (z.gt.z0) scale = 1 + (smax-1)*(z-z0)/(z1-z0)
>>>>>>>>>> if (z.gt.z1) scale = smax
>>>>>>>>>>
>>>>>>>>>> which would yield
>>>>>>>>>>
>>>>>>>>>>   scale = 1 when z=z0
>>>>>>>>>>   scale = smax when z >= z1
>>>>>>>>>>
>>>>>>>>>> Paul
>>>>>>>>>>
>>>>>>>>>>
>>>>>>>>>>
>>>>>>>>>> On Sun, 19 Jan 2014, nek5000-users at lists.mcs.anl.gov wrote:
>>>>>>>>>>
>>>>>>>>>>> Hi paul,
>>>>>>>>>>>
>>>>>>>>>>> The code works fine, but there should be a small change 
>>>>>>>>>>> thats has
>>>>>>>>>>> to be done
>>>>>>>>>>>
>>>>>>>>>>>
>>>>>>>>>>> if (z.gt.z0) scale = 1 + (z /(z1-z0 )))
>>>>>>>>>>> if (z.gt.z1) scale = smax
>>>>>>>>>>>
>>>>>>>>>>> This creates a perfect diverging pipe.
>>>>>>>>>>>
>>>>>>>>>>> Thanks for the help paul.
>>>>>>>>>>>
>>>>>>>>>>> Kamal
>>>>>>>>>>>
>>>>>>>>>>> On Jan 20, 2014, at 12:09 AM, 
>>>>>>>>>>> nek5000-users at lists.mcs.anl.gov wrote:
>>>>>>>>>>>
>>>>>>>>>>>> Hi paul,
>>>>>>>>>>>>
>>>>>>>>>>>> If I am not wrong,
>>>>>>>>>>>> I make a mesh with three straight pipes( inlet, divergent,
>>>>>>>>>>>> outlet ) connected together via n2to3 so that I know the 
>>>>>>>>>>>> element
>>>>>>>>>>>> connectivity places of the divergent section (z0,z1) and 
>>>>>>>>>>>> use the
>>>>>>>>>>>> section what you gave
>>>>>>>>>>>>
>>>>>>>>>>>> Thank you for the code
>>>>>>>>>>>>
>>>>>>>>>>>> Kamal
>>>>>>>>>>>>
>>>>>>>>>>>> On Jan 19, 2014, at 8:45 PM, 
>>>>>>>>>>>> nek5000-users at lists.mcs.anl.gov wrote:
>>>>>>>>>>>>
>>>>>>>>>>>>> Kamal,
>>>>>>>>>>>>>
>>>>>>>>>>>>> I would do the following in usrdat2():
>>>>>>>>>>>>>
>>>>>>>>>>>>>    n=nx1*ny1*nz1*nelt
>>>>>>>>>>>>>
>>>>>>>>>>>>>    do i=1,n
>>>>>>>>>>>>>       x=xm1(i,1,1,1)
>>>>>>>>>>>>>       y=ym1(i,1,1,1)
>>>>>>>>>>>>>       z=ym1(i,1,1,1)
>>>>>>>>>>>>>       scale = 1.
>>>>>>>>>>>>>       if (z.gt.z0) scale = smax*(z-z0/(z1-z0)
>>>>>>>>>>>>>       if (z.gt.z1) scale = smax
>>>>>>>>>>>>>       xm1(i,1,1,1) = scale*x
>>>>>>>>>>>>>       ym1(i,1,1,1) = scale*y
>>>>>>>>>>>>>    enddo
>>>>>>>>>>>>>
>>>>>>>>>>>>> Paul
>>>>>>>>>>>>>
>>>>>>>>>>>>> Make certain that z1 and z0 correspond to z values
>>>>>>>>>>>>> that precisely coincide with element interfaces.
>>>>>>>>>>>>>
>>>>>>>>>>>>>
>>>>>>>>>>>>> On Sun, 19 Jan 2014, nek5000-users at lists.mcs.anl.gov wrote:
>>>>>>>>>>>>>
>>>>>>>>>>>>>> Hi Paul,
>>>>>>>>>>>>>>
>>>>>>>>>>>>>> I looked into the Peris example but It is so what same like
>>>>>>>>>>>>>> the stenosis example with a Cosine deformation.
>>>>>>>>>>>>>>
>>>>>>>>>>>>>> In my case it is a pipe with conical divergent. I tried to
>>>>>>>>>>>>>> play around the variables Xm1, Ym1 and Zm1 but the mapping
>>>>>>>>>>>>>> doesn't go well.
>>>>>>>>>>>>>>
>>>>>>>>>>>>>> Could you please help me with this.
>>>>>>>>>>>>>>
>>>>>>>>>>>>>> Thank you,
>>>>>>>>>>>>>>
>>>>>>>>>>>>>> Kamal
>>>>>>>>>>>>>>
>>>>>>>>>>>>>>
>>>>>>>>>>>>>> On Jan 18, 2014, at 7:26 PM, nek5000-users at lists.mcs.anl.gov
>>>>>>>>>>>>>> wrote:
>>>>>>>>>>>>>>
>>>>>>>>>>>>>>> Hi Paul,
>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>> I looked at the Helix and stenosis example but they are 
>>>>>>>>>>>>>>> using
>>>>>>>>>>>>>>> cosine functions to deform
>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>> I tried to use a tangent function but it bends the whole 
>>>>>>>>>>>>>>> pipe.
>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>> I dint look at peris example .
>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>> I will take a look at it and let you know.
>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>> Thank you
>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>> Kamal
>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>> On Jan 18, 2014, at 7:22 PM, 
>>>>>>>>>>>>>>> nek5000-users at lists.mcs.anl.gov
>>>>>>>>>>>>>>> wrote:
>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>> Kamal,
>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>> Have you looked at the peris example? The usr file there
>>>>>>>>>>>>>>>> shows how to deform
>>>>>>>>>>>>>>>> a pipe geometry.
>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>> Paul
>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>> From: nek5000-users-bounces at lists.mcs.anl.gov
>>>>>>>>>>>>>>>> [nek5000-users-bounces at lists.mcs.anl.gov] on behalf of
>>>>>>>>>>>>>>>> nek5000-users at lists.mcs.anl.gov
>>>>>>>>>>>>>>>> [nek5000-users at lists.mcs.anl.gov]
>>>>>>>>>>>>>>>> Sent: Saturday, January 18, 2014 12:17 PM
>>>>>>>>>>>>>>>> To: nek5000-users at lists.mcs.anl.gov
>>>>>>>>>>>>>>>> Subject: Re: [Nek5000-users] Pipe with expansion
>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>> Dear Paul,
>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>> I tried many ways to map my straight pipe geometry but it
>>>>>>>>>>>>>>>> does not seem to work properly
>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>> I used something like
>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>> X = X + Z * tan ( alpha )
>>>>>>>>>>>>>>>> Y = Y + Z* tan (alpha )
>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>> even that dint work. could please help me with this
>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>> Thank you
>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>> Kamal.
>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>> On Jan 17, 2014, at 2:24 PM, 
>>>>>>>>>>>>>>>> nek5000-users at lists.mcs.anl.gov
>>>>>>>>>>>>>>>> wrote:
>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>> Hi Paul,
>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>> Thanks paul. I tried working with the diverging mesh
>>>>>>>>>>>>>>>>> modification.
>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>> I tried to use this form of equation to modify the mesh
>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>> z = mx + b
>>>>>>>>>>>>>>>>> z = ny  + c
>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>> x = ( z - b ) / m
>>>>>>>>>>>>>>>>> y = (z - c)  / n
>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>> Do you think would work ? or is there any other way to
>>>>>>>>>>>>>>>>> input that ?
>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>> Thanks,
>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>> Kamal
>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>> On 17/01/2014 14:14, 
>>>>>>>>>>>>>>>>> nek5000-users at lists.mcs.anl.govwrote:
>>>>>>>>>>>>>>>>>> Kamal,
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> 1) To check for convergence, run your simulation for
>>>>>>>>>>>>>>>>>> increasing polynomial orders ( lx1 in the SIZE file) and
>>>>>>>>>>>>>>>>>> measure some consistent quantity (drag, TKE, etc).  You
>>>>>>>>>>>>>>>>>> can plot this quantity against lx1 and this should give
>>>>>>>>>>>>>>>>>> you a good picture of how you are converging (without
>>>>>>>>>>>>>>>>>> needing to change the physical mesh).
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> 2) If you weren't using temperature in your simulation,
>>>>>>>>>>>>>>>>>> you could do put the following code snippet in your 
>>>>>>>>>>>>>>>>>> userchk
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> c-------------------------------------------
>>>>>>>>>>>>>>>>>> integer i, ntot
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> ntot = nx1*ny1*nz1*nelv  ! total number of points in
>>>>>>>>>>>>>>>>>> simulation (on THIS processor)
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> do i = 1,ntot
>>>>>>>>>>>>>>>>>> t(i,1,1,1,1) = 0.5*(vx(i,1,1,1)**2 + vy(i,1,1,1)**2 +
>>>>>>>>>>>>>>>>>> vz(i,1,1,1)**2)
>>>>>>>>>>>>>>>>>> enddo
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> ifto = .true.
>>>>>>>>>>>>>>>>>> c-------------------------------------------
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> I've assumed here that your density is unity. This
>>>>>>>>>>>>>>>>>> computed kinetic energy point-wise and stores it in the
>>>>>>>>>>>>>>>>>> temperature field. The part "ifto = .true." tells Nek to
>>>>>>>>>>>>>>>>>> output the temperature field whenever it outputs a field
>>>>>>>>>>>>>>>>>> file.  You could then view this in visit just like you
>>>>>>>>>>>>>>>>>> would the velocity field.
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> Hope this helps!
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> Josh
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> On Wed, Jan 15, 2014 at 9:52 AM,
>>>>>>>>>>>>>>>>>> <nek5000-users at lists.mcs.anl.gov> wrote:
>>>>>>>>>>>>>>>>>> Hi Paul,
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> I will try that mapping, I created a straight pipe to do
>>>>>>>>>>>>>>>>>> some simulations.
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> 1) Is there a way to check my spectral convergence, so
>>>>>>>>>>>>>>>>>> that I can do some mesh convergence study?
>>>>>>>>>>>>>>>>>> 2) Is there a way to plot the kinetic energy in the 
>>>>>>>>>>>>>>>>>> flow ?
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> Thank you,
>>>>>>>>>>>>>>>>>> Kamal
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> On 15/01/2014 12:14, nek5000-users at lists.mcs.anl.gov 
>>>>>>>>>>>>>>>>>> wrote:
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> Hi Kamal,
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> For the geometry you describe, I would apply mesh 
>>>>>>>>>>>>>>>>>> morphing
>>>>>>>>>>>>>>>>>> to a standard straight pipe. You can create such a pipe
>>>>>>>>>>>>>>>>>> using a subset of the mkmesh script provided in the 
>>>>>>>>>>>>>>>>>> expansion
>>>>>>>>>>>>>>>>>> example.
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> If your transition region is conical, then I woud make
>>>>>>>>>>>>>>>>>> certain that the change in slope occurs at element
>>>>>>>>>>>>>>>>>> boundaries,
>>>>>>>>>>>>>>>>>> i.e., as in the half cross-section depicted below:
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> _______________
>>>>>>>>>>>>>>>>>>                           /| |      |
>>>>>>>>>>>>>>>>>>                         /  | |      |
>>>>>>>>>>>>>>>>>>                       /|   | |      |
>>>>>>>>>>>>>>>>>>     ________________/  |   | |      |
>>>>>>>>>>>>>>>>>>     |     |     |   |  |   | |      |
>>>>>>>>>>>>>>>>>>     |     |     |   |  |   | |      |
>>>>>>>>>>>>>>>>>> +-----+-----+---+--+---+------+------+----> z
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> Paul
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> On Wed, 15 Jan 2014, nek5000-users at lists.mcs.anl.gov 
>>>>>>>>>>>>>>>>>> wrote:
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> Hi Paul,
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> I looked at the example and it looks very helpful, 
>>>>>>>>>>>>>>>>>> but for
>>>>>>>>>>>>>>>>>> a sudden expansion we have only two parts (i.e) the 
>>>>>>>>>>>>>>>>>> inlet
>>>>>>>>>>>>>>>>>> pipe and the outlet pipe. Whereas in a diverging pipe we
>>>>>>>>>>>>>>>>>> have three section (i.e,) The inlet pipe, Diverging
>>>>>>>>>>>>>>>>>> section and the outlet pipe.
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> Is it possible for me to create a 2D diverging section
>>>>>>>>>>>>>>>>>> using mesh modification and revolve it around the centre
>>>>>>>>>>>>>>>>>> axis to get a 3d diverging pipe ?
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> or should I apply the mesh modification directly to 
>>>>>>>>>>>>>>>>>> the 3d
>>>>>>>>>>>>>>>>>> sudden expansion pipe using usrdat2() ?
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> Thanks,
>>>>>>>>>>>>>>>>>> Kamal
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> On 14/01/2014 21:09, nek5000-users at lists.mcs.anl.gov 
>>>>>>>>>>>>>>>>>> wrote:
>>>>>>>>>>>>>>>>>> Hi Paul,
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> Thanks a lot for the update. I will take a look at as 
>>>>>>>>>>>>>>>>>> soon
>>>>>>>>>>>>>>>>>> as possible and keep you updated with it.
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> Thank you,
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> Kamal
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> On Jan 14, 2014, at 9:04 PM,
>>>>>>>>>>>>>>>>>> nek5000-users at lists.mcs.anl.gov wrote:
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> Kamal,
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> I've added an example for a step-type expansion in a 
>>>>>>>>>>>>>>>>>> pipe.
>>>>>>>>>>>>>>>>>> New example directory
>>>>>>>>>>>>>>>>>> is nek5_svn/examples/expansion, with a README.
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> If you want a standard diffuser, I would use
>>>>>>>>>>>>>>>>>> mesh-morphing, as outlined in the
>>>>>>>>>>>>>>>>>> nek primer, which can be found on this page:
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> http://nek5000.mcs.anl.gov/index.php/UG#Documentation
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> I've also automated our turbulent outflow bc 
>>>>>>>>>>>>>>>>>> treatment --
>>>>>>>>>>>>>>>>>> one simply provides an
>>>>>>>>>>>>>>>>>> expansion factor (typically ~ 1.5) and two persistent
>>>>>>>>>>>>>>>>>> arrays to turb_outflow(), which
>>>>>>>>>>>>>>>>>> is now in navier5.f.    This can be useful when very
>>>>>>>>>>>>>>>>>> strong vortices are leaving the
>>>>>>>>>>>>>>>>>> domain, which is possible for certain diffuser flow
>>>>>>>>>>>>>>>>>> conditions (and others).
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> Paul
>>>>>>>>>>>>>>>>>> ________________________________________
>>>>>>>>>>>>>>>>>> From: nek5000-users-bounces at lists.mcs.anl.gov
>>>>>>>>>>>>>>>>>> [nek5000-users-bounces at lists.mcs.anl.gov] on behalf
>>>>>>>>>>>>>>>>>> ofnek5000-users at lists.mcs.anl.gov
>>>>>>>>>>>>>>>>>> [nek5000-users at lists.mcs.anl.gov]
>>>>>>>>>>>>>>>>>> Sent: Monday, January 13, 2014 3:35 AM
>>>>>>>>>>>>>>>>>> To: nek5000-users at lists.mcs.anl.gov
>>>>>>>>>>>>>>>>>> Subject: [Nek5000-users] Creating a Mesh
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> Hi
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> Can some one please help me in this because I am new 
>>>>>>>>>>>>>>>>>> to nek
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> 1) How can I create a .rea for a specific geometry 
>>>>>>>>>>>>>>>>>> say ' A
>>>>>>>>>>>>>>>>>> sudden
>>>>>>>>>>>>>>>>>> expansion pipe ' or a ' Diverging pipe '
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> 2) What tool I should use to create that mesh.
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> Thank you
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> kamal
>>>>>>>>>>>>>>>>>> _______________________________________________
>>>>>>>>>>>>>>>>>> Nek5000-users mailing list
>>>>>>>>>>>>>>>>>> Nek5000-users at lists.mcs.anl.gov
>>>>>>>>>>>>>>>>>> https://lists.mcs.anl.gov/mailman/listinfo/nek5000-users
>>>>>>>>>>>>>>>>>> _______________________________________________
>>>>>>>>>>>>>>>>>> Nek5000-users mailing list
>>>>>>>>>>>>>>>>>> Nek5000-users at lists.mcs.anl.gov
>>>>>>>>>>>>>>>>>> https://lists.mcs.anl.gov/mailman/listinfo/nek5000-users
>>>>>>>>>>>>>>>>>> _______________________________________________
>>>>>>>>>>>>>>>>>> Nek5000-users mailing list
>>>>>>>>>>>>>>>>>> Nek5000-users at lists.mcs.anl.gov
>>>>>>>>>>>>>>>>>> https://lists.mcs.anl.gov/mailman/listinfo/nek5000-users
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> _______________________________________________
>>>>>>>>>>>>>>>>>> Nek5000-users mailing list
>>>>>>>>>>>>>>>>>> Nek5000-users at lists.mcs.anl.gov
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>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> _______________________________________________
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>>>>>>>>>>>>>>>>>> _______________________________________________
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>>>>>>>>>>>>>>>>>> https://lists.mcs.anl.gov/mailman/listinfo/nek5000-users
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> -- 
>>>>>>>>>>>>>>>>>> Josh Camp
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> "All that is necessary for the triumph of evil is that
>>>>>>>>>>>>>>>>>> good men do nothing" -- Edmund Burke
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> _______________________________________________
>>>>>>>>>>>>>>>>>> Nek5000-users mailing list
>>>>>>>>>>>>>>>>>> Nek5000-users at lists.mcs.anl.gov
>>>>>>>>>>>>>>>>>> https://lists.mcs.anl.gov/mailman/listinfo/nek5000-users
>>>>>>>>>>>>>>>>> _______________________________________________
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>>>> _______________________________________________
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>>>
>>
>> On Fri, 24 Jan 2014, nek5000-users at lists.mcs.anl.gov wrote:
>>
>>> Hello Paul,
>>>
>>> Thanks for your reply. I am looking into the .usr file for defining 
>>> the set_obj ().
>>>
>>> 1) Could you please tell me what is 'Enter the number of levels ?' 
>>> in n2to3
>>>
>>> is it the number of elements in Z direction ?
>>>
>>> 2) As you said about storing the computed vorticity in velocity 
>>> field to view in VisIT, I found the routine to compute the vorticity 
>>> but I am stuck about adding it to the velocity filed to VisIT ? 
>>> could you please tell me how it works or any example which stores 
>>> vorticity to the .fld file as a separate variable.
>>>
>>>
>>> Thank you
>>>
>>> Kamal
>>>
>>>
>>> On 22/01/2014 16:53, nek5000-users at lists.mcs.anl.gov wrote:
>>>> Axial viscous stress is given by torq_calc -- that's no problem 
>>>> whatsoever. You get a number as a
>>>> function of time.
>>>>
>>>> You can even get stresses on multiple subsets of the geometry 
>>>> (e.g., if you had multiple branches
>>>> in the domain or multiple cylinders.   The drag, which is a 
>>>> byproduct of the torque computation (which
>>>> you can ignore), is given in terms of the viscous and pressure 
>>>> components separately and as the
>>>> sum of the two.
>>>>
>>>> You can identify domain boundaries by checking the boundary 
>>>> conditions. Here, I recommend
>>>> looking at the set_obj routines in several of the /example cases.
>>>>
>>>>
>>>> ________________________________________
>>>> From: nek5000-users-bounces at lists.mcs.anl.gov 
>>>> [nek5000-users-bounces at lists.mcs.anl.gov] on behalf of 
>>>> nek5000-users at lists.mcs.anl.gov [nek5000-users at lists.mcs.anl.gov]
>>>> Sent: Wednesday, January 22, 2014 9:37 AM
>>>> To: nek5000-users at lists.mcs.anl.gov
>>>> Subject: Re: [Nek5000-users] Pipe with expansion
>>>>
>>>> Hello Paul
>>>>
>>>> I was thinking about taking the tangential velocity near to the 
>>>> wall so that I can figure out my length of the recirculation region.
>>>>
>>>> Is it possible for me to access the boundary elements of the mesh 
>>>> ??? so that I can take the boundary element and then obtain the 
>>>> velocity at that point so that I can figure out the length of my 
>>>> recirculation region.
>>>>
>>>> or take the *.fld file and read it to plot the datas I need.
>>>>
>>>>
>>>> I also want to calculate the axial viscous force acting on the 
>>>> entire pipe.
>>>>
>>>> which is given by
>>>>
>>>> C_v =  F^v / ( d^2 * rho * U^2 ) =   double integral ( 1/Re * (du / 
>>>> dr) ) dtheta dz
>>>>
>>>>
>>>> On Jan 22, 2014, at 4:07 PM, nek5000-users at lists.mcs.anl.gov wrote:
>>>>
>>>>> Hi Kamal,
>>>>>
>>>>> As I thought about it some more, if you're interested in the local 
>>>>> wall shear stress
>>>>> magnitude I'm quite certain you can get this by plotting the 
>>>>> magnitude of vorticity
>>>>> on the surface in question.   (Note that the sign of the WSS, 
>>>>> which in fact is a tensor
>>>>> or a vector when restricted to a given surface, is lost in this 
>>>>> process, but that might
>>>>> not be relevant for your needs.)   If that works, then you can 
>>>>> readily compute the
>>>>> vorticity using one of the routines in nek and store the result in 
>>>>> a velocity field, then
>>>>> view that field with VisIt.   Of course WSS will require 
>>>>> multiplication by viscosity.
>>>>>
>>>>> hth,
>>>>>
>>>>> Paul
>>>>>
>>>>> ________________________________________
>>>>> From: nek5000-users-bounces at lists.mcs.anl.gov 
>>>>> [nek5000-users-bounces at lists.mcs.anl.gov] on behalf of 
>>>>> nek5000-users at lists.mcs.anl.gov [nek5000-users at lists.mcs.anl.gov]
>>>>> Sent: Tuesday, January 21, 2014 10:33 AM
>>>>> To: nek5000-users at lists.mcs.anl.gov
>>>>> Subject: Re: [Nek5000-users] Pipe with expansion
>>>>>
>>>>> Hi paul,
>>>>>
>>>>> can I make this to be drag or shear quantities to be return to the a
>>>>> separate file so that it will easy for me to plot.
>>>>>
>>>>> By the way it gives the integral quantity. Think for example I 
>>>>> need to
>>>>> find the shear stress on the wall  from the inlet to outlet at a
>>>>> particular time = 2 . How can I do that ?
>>>>>
>>>>> Is there way to find the number of elements in x,y and z direction ?
>>>>>
>>>>> On 21/01/2014 17:32, nek5000-users at lists.mcs.anl.gov wrote:
>>>>>> Hi Kamal,
>>>>>>
>>>>>> Your integrated drag quantities should be written to the logfile
>>>>>> (stdout),
>>>>>> assuming you've set the arguments in the call to be .true.
>>>>>>
>>>>>> Paul
>>>>>>
>>>>>> On Tue, 21 Jan 2014, nek5000-users at lists.mcs.anl.gov wrote:
>>>>>>
>>>>>>> Hi Paul,
>>>>>>>
>>>>>>> I checked the set_obj subroutine and implemented one in my .USR 
>>>>>>> file.
>>>>>>> The code seem to run without any errors but I don't find where 
>>>>>>> these
>>>>>>> variables are getting stored.
>>>>>>>
>>>>>>> I use VisIT to visualize my output, even there was no change in it.
>>>>>>>
>>>>>>> do I have to define my own output file and write the variables 
>>>>>>> out ?
>>>>>>>
>>>>>>> Thanks,
>>>>>>>
>>>>>>> Kamal.
>>>>>>>
>>>>>>>
>>>>>>> On 20/01/2014 21:52, nek5000-users at lists.mcs.anl.gov wrote:
>>>>>>>> Hi Kamal,
>>>>>>>>
>>>>>>>> You'll need to compute your own tke by manipulating the
>>>>>>>> velocity fields.
>>>>>>>>
>>>>>>>> You can get running averages of the requisite quantities
>>>>>>>> via calls to "avg_all" which is found in navier5.f
>>>>>>>>
>>>>>>>> You can compute shear stress on the wall simply by computing
>>>>>>>> the drag on the wall, which can be done via a call to 
>>>>>>>> torque_calc(),
>>>>>>>> also found in navier5.f
>>>>>>>>
>>>>>>>> If you cd to /examples and type:
>>>>>>>>
>>>>>>>>       grep torq */*.usr
>>>>>>>>
>>>>>>>> you'll find many examples of calls to torque_calc. You simply
>>>>>>>> need to prescribe the surfaces on which shear is to be integrated.
>>>>>>>>
>>>>>>>> I typically write a routine "set_obj" to identify such surfaces
>>>>>>>> on the first call to usrchk.
>>>>>>>>
>>>>>>>>       grep set_obj */*.usr
>>>>>>>>
>>>>>>>> will show similar examples.
>>>>>>>>
>>>>>>>> I would recommend trying this for laminar Poiseiulle flow in
>>>>>>>> a very simple channel just to check that your calls are properly
>>>>>>>> set.
>>>>>>>>
>>>>>>>> Best,
>>>>>>>>
>>>>>>>> Paul
>>>>>>>>
>>>>>>>>
>>>>>>>> On Mon, 20 Jan 2014, nek5000-users at lists.mcs.anl.gov wrote:
>>>>>>>>
>>>>>>>>> Hi Paul,
>>>>>>>>>
>>>>>>>>> Thanks and that helped.
>>>>>>>>>
>>>>>>>>> Where can I find the variables like Turbulent KE , shear 
>>>>>>>>> stress on
>>>>>>>>> the wall. ?
>>>>>>>>>
>>>>>>>>> Do i have to activate some parameters for calculating them ?
>>>>>>>>>
>>>>>>>>> If I had to plot them.
>>>>>>>>>
>>>>>>>>> Thanks,
>>>>>>>>> Kamal
>>>>>>>>>
>>>>>>>>>
>>>>>>>>> On Jan 20, 2014, at 5:41 AM, nek5000-users at lists.mcs.anl.gov 
>>>>>>>>> wrote:
>>>>>>>>>
>>>>>>>>>> Kamal,
>>>>>>>>>>
>>>>>>>>>> Looks good.
>>>>>>>>>>
>>>>>>>>>> I'm guessing that one further refinement would be:
>>>>>>>>>>
>>>>>>>>>> if (z.gt.z0) scale = 1 + (smax-1)*(z-z0)/(z1-z0)
>>>>>>>>>> if (z.gt.z1) scale = smax
>>>>>>>>>>
>>>>>>>>>> which would yield
>>>>>>>>>>
>>>>>>>>>>   scale = 1 when z=z0
>>>>>>>>>>   scale = smax when z >= z1
>>>>>>>>>>
>>>>>>>>>> Paul
>>>>>>>>>>
>>>>>>>>>>
>>>>>>>>>>
>>>>>>>>>> On Sun, 19 Jan 2014, nek5000-users at lists.mcs.anl.gov wrote:
>>>>>>>>>>
>>>>>>>>>>> Hi paul,
>>>>>>>>>>>
>>>>>>>>>>> The code works fine, but there should be a small change 
>>>>>>>>>>> thats has
>>>>>>>>>>> to be done
>>>>>>>>>>>
>>>>>>>>>>>
>>>>>>>>>>> if (z.gt.z0) scale = 1 + (z /(z1-z0 )))
>>>>>>>>>>> if (z.gt.z1) scale = smax
>>>>>>>>>>>
>>>>>>>>>>> This creates a perfect diverging pipe.
>>>>>>>>>>>
>>>>>>>>>>> Thanks for the help paul.
>>>>>>>>>>>
>>>>>>>>>>> Kamal
>>>>>>>>>>>
>>>>>>>>>>> On Jan 20, 2014, at 12:09 AM, 
>>>>>>>>>>> nek5000-users at lists.mcs.anl.gov wrote:
>>>>>>>>>>>
>>>>>>>>>>>> Hi paul,
>>>>>>>>>>>>
>>>>>>>>>>>> If I am not wrong,
>>>>>>>>>>>> I make a mesh with three straight pipes( inlet, divergent,
>>>>>>>>>>>> outlet ) connected together via n2to3 so that I know the 
>>>>>>>>>>>> element
>>>>>>>>>>>> connectivity places of the divergent section (z0,z1) and 
>>>>>>>>>>>> use the
>>>>>>>>>>>> section what you gave
>>>>>>>>>>>>
>>>>>>>>>>>> Thank you for the code
>>>>>>>>>>>>
>>>>>>>>>>>> Kamal
>>>>>>>>>>>>
>>>>>>>>>>>> On Jan 19, 2014, at 8:45 PM, 
>>>>>>>>>>>> nek5000-users at lists.mcs.anl.gov wrote:
>>>>>>>>>>>>
>>>>>>>>>>>>> Kamal,
>>>>>>>>>>>>>
>>>>>>>>>>>>> I would do the following in usrdat2():
>>>>>>>>>>>>>
>>>>>>>>>>>>>    n=nx1*ny1*nz1*nelt
>>>>>>>>>>>>>
>>>>>>>>>>>>>    do i=1,n
>>>>>>>>>>>>>       x=xm1(i,1,1,1)
>>>>>>>>>>>>>       y=ym1(i,1,1,1)
>>>>>>>>>>>>>       z=ym1(i,1,1,1)
>>>>>>>>>>>>>       scale = 1.
>>>>>>>>>>>>>       if (z.gt.z0) scale = smax*(z-z0/(z1-z0)
>>>>>>>>>>>>>       if (z.gt.z1) scale = smax
>>>>>>>>>>>>>       xm1(i,1,1,1) = scale*x
>>>>>>>>>>>>>       ym1(i,1,1,1) = scale*y
>>>>>>>>>>>>>    enddo
>>>>>>>>>>>>>
>>>>>>>>>>>>> Paul
>>>>>>>>>>>>>
>>>>>>>>>>>>> Make certain that z1 and z0 correspond to z values
>>>>>>>>>>>>> that precisely coincide with element interfaces.
>>>>>>>>>>>>>
>>>>>>>>>>>>>
>>>>>>>>>>>>> On Sun, 19 Jan 2014, nek5000-users at lists.mcs.anl.gov wrote:
>>>>>>>>>>>>>
>>>>>>>>>>>>>> Hi Paul,
>>>>>>>>>>>>>>
>>>>>>>>>>>>>> I looked into the Peris example but It is so what same like
>>>>>>>>>>>>>> the stenosis example with a Cosine deformation.
>>>>>>>>>>>>>>
>>>>>>>>>>>>>> In my case it is a pipe with conical divergent. I tried to
>>>>>>>>>>>>>> play around the variables Xm1, Ym1 and Zm1 but the mapping
>>>>>>>>>>>>>> doesn't go well.
>>>>>>>>>>>>>>
>>>>>>>>>>>>>> Could you please help me with this.
>>>>>>>>>>>>>>
>>>>>>>>>>>>>> Thank you,
>>>>>>>>>>>>>>
>>>>>>>>>>>>>> Kamal
>>>>>>>>>>>>>>
>>>>>>>>>>>>>>
>>>>>>>>>>>>>> On Jan 18, 2014, at 7:26 PM, nek5000-users at lists.mcs.anl.gov
>>>>>>>>>>>>>> wrote:
>>>>>>>>>>>>>>
>>>>>>>>>>>>>>> Hi Paul,
>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>> I looked at the Helix and stenosis example but they are 
>>>>>>>>>>>>>>> using
>>>>>>>>>>>>>>> cosine functions to deform
>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>> I tried to use a tangent function but it bends the whole 
>>>>>>>>>>>>>>> pipe.
>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>> I dint look at peris example .
>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>> I will take a look at it and let you know.
>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>> Thank you
>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>> Kamal
>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>> On Jan 18, 2014, at 7:22 PM, 
>>>>>>>>>>>>>>> nek5000-users at lists.mcs.anl.gov
>>>>>>>>>>>>>>> wrote:
>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>> Kamal,
>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>> Have you looked at the peris example? The usr file there
>>>>>>>>>>>>>>>> shows how to deform
>>>>>>>>>>>>>>>> a pipe geometry.
>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>> Paul
>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>> From: nek5000-users-bounces at lists.mcs.anl.gov
>>>>>>>>>>>>>>>> [nek5000-users-bounces at lists.mcs.anl.gov] on behalf of
>>>>>>>>>>>>>>>> nek5000-users at lists.mcs.anl.gov
>>>>>>>>>>>>>>>> [nek5000-users at lists.mcs.anl.gov]
>>>>>>>>>>>>>>>> Sent: Saturday, January 18, 2014 12:17 PM
>>>>>>>>>>>>>>>> To: nek5000-users at lists.mcs.anl.gov
>>>>>>>>>>>>>>>> Subject: Re: [Nek5000-users] Pipe with expansion
>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>> Dear Paul,
>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>> I tried many ways to map my straight pipe geometry but it
>>>>>>>>>>>>>>>> does not seem to work properly
>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>> I used something like
>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>> X = X + Z * tan ( alpha )
>>>>>>>>>>>>>>>> Y = Y + Z* tan (alpha )
>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>> even that dint work. could please help me with this
>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>> Thank you
>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>> Kamal.
>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>> On Jan 17, 2014, at 2:24 PM, 
>>>>>>>>>>>>>>>> nek5000-users at lists.mcs.anl.gov
>>>>>>>>>>>>>>>> wrote:
>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>> Hi Paul,
>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>> Thanks paul. I tried working with the diverging mesh
>>>>>>>>>>>>>>>>> modification.
>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>> I tried to use this form of equation to modify the mesh
>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>> z = mx + b
>>>>>>>>>>>>>>>>> z = ny  + c
>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>> x = ( z - b ) / m
>>>>>>>>>>>>>>>>> y = (z - c)  / n
>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>> Do you think would work ? or is there any other way to
>>>>>>>>>>>>>>>>> input that ?
>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>> Thanks,
>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>> Kamal
>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>> On 17/01/2014 14:14, 
>>>>>>>>>>>>>>>>> nek5000-users at lists.mcs.anl.govwrote:
>>>>>>>>>>>>>>>>>> Kamal,
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> 1) To check for convergence, run your simulation for
>>>>>>>>>>>>>>>>>> increasing polynomial orders ( lx1 in the SIZE file) and
>>>>>>>>>>>>>>>>>> measure some consistent quantity (drag, TKE, etc).  You
>>>>>>>>>>>>>>>>>> can plot this quantity against lx1 and this should give
>>>>>>>>>>>>>>>>>> you a good picture of how you are converging (without
>>>>>>>>>>>>>>>>>> needing to change the physical mesh).
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> 2) If you weren't using temperature in your simulation,
>>>>>>>>>>>>>>>>>> you could do put the following code snippet in your 
>>>>>>>>>>>>>>>>>> userchk
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> c-------------------------------------------
>>>>>>>>>>>>>>>>>> integer i, ntot
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> ntot = nx1*ny1*nz1*nelv  ! total number of points in
>>>>>>>>>>>>>>>>>> simulation (on THIS processor)
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> do i = 1,ntot
>>>>>>>>>>>>>>>>>> t(i,1,1,1,1) = 0.5*(vx(i,1,1,1)**2 + vy(i,1,1,1)**2 +
>>>>>>>>>>>>>>>>>> vz(i,1,1,1)**2)
>>>>>>>>>>>>>>>>>> enddo
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> ifto = .true.
>>>>>>>>>>>>>>>>>> c-------------------------------------------
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> I've assumed here that your density is unity. This
>>>>>>>>>>>>>>>>>> computed kinetic energy point-wise and stores it in the
>>>>>>>>>>>>>>>>>> temperature field. The part "ifto = .true." tells Nek to
>>>>>>>>>>>>>>>>>> output the temperature field whenever it outputs a field
>>>>>>>>>>>>>>>>>> file.  You could then view this in visit just like you
>>>>>>>>>>>>>>>>>> would the velocity field.
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> Hope this helps!
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> Josh
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> On Wed, Jan 15, 2014 at 9:52 AM,
>>>>>>>>>>>>>>>>>> <nek5000-users at lists.mcs.anl.gov> wrote:
>>>>>>>>>>>>>>>>>> Hi Paul,
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> I will try that mapping, I created a straight pipe to do
>>>>>>>>>>>>>>>>>> some simulations.
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> 1) Is there a way to check my spectral convergence, so
>>>>>>>>>>>>>>>>>> that I can do some mesh convergence study?
>>>>>>>>>>>>>>>>>> 2) Is there a way to plot the kinetic energy in the 
>>>>>>>>>>>>>>>>>> flow ?
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> Thank you,
>>>>>>>>>>>>>>>>>> Kamal
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> On 15/01/2014 12:14, nek5000-users at lists.mcs.anl.gov 
>>>>>>>>>>>>>>>>>> wrote:
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> Hi Kamal,
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> For the geometry you describe, I would apply mesh 
>>>>>>>>>>>>>>>>>> morphing
>>>>>>>>>>>>>>>>>> to a standard straight pipe. You can create such a pipe
>>>>>>>>>>>>>>>>>> using a subset of the mkmesh script provided in the 
>>>>>>>>>>>>>>>>>> expansion
>>>>>>>>>>>>>>>>>> example.
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> If your transition region is conical, then I woud make
>>>>>>>>>>>>>>>>>> certain that the change in slope occurs at element
>>>>>>>>>>>>>>>>>> boundaries,
>>>>>>>>>>>>>>>>>> i.e., as in the half cross-section depicted below:
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> _______________
>>>>>>>>>>>>>>>>>>                           /| |      |
>>>>>>>>>>>>>>>>>>                         /  | |      |
>>>>>>>>>>>>>>>>>>                       /|   | |      |
>>>>>>>>>>>>>>>>>>     ________________/  |   | |      |
>>>>>>>>>>>>>>>>>>     |     |     |   |  |   | |      |
>>>>>>>>>>>>>>>>>>     |     |     |   |  |   | |      |
>>>>>>>>>>>>>>>>>> +-----+-----+---+--+---+------+------+----> z
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> Paul
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> On Wed, 15 Jan 2014, nek5000-users at lists.mcs.anl.gov 
>>>>>>>>>>>>>>>>>> wrote:
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> Hi Paul,
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> I looked at the example and it looks very helpful, 
>>>>>>>>>>>>>>>>>> but for
>>>>>>>>>>>>>>>>>> a sudden expansion we have only two parts (i.e) the 
>>>>>>>>>>>>>>>>>> inlet
>>>>>>>>>>>>>>>>>> pipe and the outlet pipe. Whereas in a diverging pipe we
>>>>>>>>>>>>>>>>>> have three section (i.e,) The inlet pipe, Diverging
>>>>>>>>>>>>>>>>>> section and the outlet pipe.
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> Is it possible for me to create a 2D diverging section
>>>>>>>>>>>>>>>>>> using mesh modification and revolve it around the centre
>>>>>>>>>>>>>>>>>> axis to get a 3d diverging pipe ?
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> or should I apply the mesh modification directly to 
>>>>>>>>>>>>>>>>>> the 3d
>>>>>>>>>>>>>>>>>> sudden expansion pipe using usrdat2() ?
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> Thanks,
>>>>>>>>>>>>>>>>>> Kamal
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> On 14/01/2014 21:09, nek5000-users at lists.mcs.anl.gov 
>>>>>>>>>>>>>>>>>> wrote:
>>>>>>>>>>>>>>>>>> Hi Paul,
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> Thanks a lot for the update. I will take a look at as 
>>>>>>>>>>>>>>>>>> soon
>>>>>>>>>>>>>>>>>> as possible and keep you updated with it.
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> Thank you,
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> Kamal
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> On Jan 14, 2014, at 9:04 PM,
>>>>>>>>>>>>>>>>>> nek5000-users at lists.mcs.anl.gov wrote:
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> Kamal,
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> I've added an example for a step-type expansion in a 
>>>>>>>>>>>>>>>>>> pipe.
>>>>>>>>>>>>>>>>>> New example directory
>>>>>>>>>>>>>>>>>> is nek5_svn/examples/expansion, with a README.
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> If you want a standard diffuser, I would use
>>>>>>>>>>>>>>>>>> mesh-morphing, as outlined in the
>>>>>>>>>>>>>>>>>> nek primer, which can be found on this page:
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> http://nek5000.mcs.anl.gov/index.php/UG#Documentation
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> I've also automated our turbulent outflow bc 
>>>>>>>>>>>>>>>>>> treatment --
>>>>>>>>>>>>>>>>>> one simply provides an
>>>>>>>>>>>>>>>>>> expansion factor (typically ~ 1.5) and two persistent
>>>>>>>>>>>>>>>>>> arrays to turb_outflow(), which
>>>>>>>>>>>>>>>>>> is now in navier5.f.    This can be useful when very
>>>>>>>>>>>>>>>>>> strong vortices are leaving the
>>>>>>>>>>>>>>>>>> domain, which is possible for certain diffuser flow
>>>>>>>>>>>>>>>>>> conditions (and others).
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> Paul
>>>>>>>>>>>>>>>>>> ________________________________________
>>>>>>>>>>>>>>>>>> From: nek5000-users-bounces at lists.mcs.anl.gov
>>>>>>>>>>>>>>>>>> [nek5000-users-bounces at lists.mcs.anl.gov] on behalf
>>>>>>>>>>>>>>>>>> ofnek5000-users at lists.mcs.anl.gov
>>>>>>>>>>>>>>>>>> [nek5000-users at lists.mcs.anl.gov]
>>>>>>>>>>>>>>>>>> Sent: Monday, January 13, 2014 3:35 AM
>>>>>>>>>>>>>>>>>> To: nek5000-users at lists.mcs.anl.gov
>>>>>>>>>>>>>>>>>> Subject: [Nek5000-users] Creating a Mesh
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> Hi
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> Can some one please help me in this because I am new 
>>>>>>>>>>>>>>>>>> to nek
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> 1) How can I create a .rea for a specific geometry 
>>>>>>>>>>>>>>>>>> say ' A
>>>>>>>>>>>>>>>>>> sudden
>>>>>>>>>>>>>>>>>> expansion pipe ' or a ' Diverging pipe '
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> 2) What tool I should use to create that mesh.
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> Thank you
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> kamal
>>>>>>>>>>>>>>>>>> _______________________________________________
>>>>>>>>>>>>>>>>>> Nek5000-users mailing list
>>>>>>>>>>>>>>>>>> Nek5000-users at lists.mcs.anl.gov
>>>>>>>>>>>>>>>>>> https://lists.mcs.anl.gov/mailman/listinfo/nek5000-users
>>>>>>>>>>>>>>>>>> _______________________________________________
>>>>>>>>>>>>>>>>>> Nek5000-users mailing list
>>>>>>>>>>>>>>>>>> Nek5000-users at lists.mcs.anl.gov
>>>>>>>>>>>>>>>>>> https://lists.mcs.anl.gov/mailman/listinfo/nek5000-users
>>>>>>>>>>>>>>>>>> _______________________________________________
>>>>>>>>>>>>>>>>>> Nek5000-users mailing list
>>>>>>>>>>>>>>>>>> Nek5000-users at lists.mcs.anl.gov
>>>>>>>>>>>>>>>>>> https://lists.mcs.anl.gov/mailman/listinfo/nek5000-users
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> _______________________________________________
>>>>>>>>>>>>>>>>>> Nek5000-users mailing list
>>>>>>>>>>>>>>>>>> Nek5000-users at lists.mcs.anl.gov
>>>>>>>>>>>>>>>>>> https://lists.mcs.anl.gov/mailman/listinfo/nek5000-users
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> _______________________________________________
>>>>>>>>>>>>>>>>>> Nek5000-users mailing list
>>>>>>>>>>>>>>>>>> Nek5000-users at lists.mcs.anl.gov
>>>>>>>>>>>>>>>>>> https://lists.mcs.anl.gov/mailman/listinfo/nek5000-users
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> _______________________________________________
>>>>>>>>>>>>>>>>>> Nek5000-users mailing list
>>>>>>>>>>>>>>>>>> Nek5000-users at lists.mcs.anl.gov
>>>>>>>>>>>>>>>>>> https://lists.mcs.anl.gov/mailman/listinfo/nek5000-users
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> -- 
>>>>>>>>>>>>>>>>>> Josh Camp
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> "All that is necessary for the triumph of evil is that
>>>>>>>>>>>>>>>>>> good men do nothing" -- Edmund Burke
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>>
>>>>>>>>>>>>>>>>>> _______________________________________________
>>>>>>>>>>>>>>>>>> Nek5000-users mailing list
>>>>>>>>>>>>>>>>>> Nek5000-users at lists.mcs.anl.gov
>>>>>>>>>>>>>>>>>> https://lists.mcs.anl.gov/mailman/listinfo/nek5000-users
>>>>>>>>>>>>>>>>> _______________________________________________
>>>>>>>>>>>>>>>>> Nek5000-users mailing list
>>>>>>>>>>>>>>>>> Nek5000-users at lists.mcs.anl.gov
>>>>>>>>>>>>>>>>> https://lists.mcs.anl.gov/mailman/listinfo/nek5000-users
>>>>>>>>>>>>>>>> _______________________________________________
>>>>>>>>>>>>>>>> Nek5000-users mailing list
>>>>>>>>>>>>>>>> Nek5000-users at lists.mcs.anl.gov
>>>>>>>>>>>>>>>> https://lists.mcs.anl.gov/mailman/listinfo/nek5000-users
>>>>>>>>>>>>>>> _______________________________________________
>>>>>>>>>>>>>>> Nek5000-users mailing list
>>>>>>>>>>>>>>> Nek5000-users at lists.mcs.anl.gov
>>>>>>>>>>>>>>> https://lists.mcs.anl.gov/mailman/listinfo/nek5000-users
>>>>>>>>>>>>>>
>>>>>>>>>>>>> _______________________________________________
>>>>>>>>>>>>> Nek5000-users mailing list
>>>>>>>>>>>>> Nek5000-users at lists.mcs.anl.gov
>>>>>>>>>>>>> https://lists.mcs.anl.gov/mailman/listinfo/nek5000-users
>>>>>>>>>>>> _______________________________________________
>>>>>>>>>>>> Nek5000-users mailing list
>>>>>>>>>>>> Nek5000-users at lists.mcs.anl.gov
>>>>>>>>>>>> https://lists.mcs.anl.gov/mailman/listinfo/nek5000-users
>>>>>>>>>>> _______________________________________________
>>>>>>>>>>> Nek5000-users mailing list
>>>>>>>>>>> Nek5000-users at lists.mcs.anl.gov
>>>>>>>>>>> https://lists.mcs.anl.gov/mailman/listinfo/nek5000-users
>>>>>>>>>>>
>>>>>>>>>> _______________________________________________
>>>>>>>>>> Nek5000-users mailing list
>>>>>>>>>> Nek5000-users at lists.mcs.anl.gov
>>>>>>>>>> https://lists.mcs.anl.gov/mailman/listinfo/nek5000-users
>>>>>>>>> _______________________________________________
>>>>>>>>> Nek5000-users mailing list
>>>>>>>>> Nek5000-users at lists.mcs.anl.gov
>>>>>>>>> https://lists.mcs.anl.gov/mailman/listinfo/nek5000-users
>>>>>>>>>
>>>>>>>> _______________________________________________
>>>>>>>> Nek5000-users mailing list
>>>>>>>> Nek5000-users at lists.mcs.anl.gov
>>>>>>>> https://lists.mcs.anl.gov/mailman/listinfo/nek5000-users
>>>>>>> _______________________________________________
>>>>>>> Nek5000-users mailing list
>>>>>>> Nek5000-users at lists.mcs.anl.gov
>>>>>>> https://lists.mcs.anl.gov/mailman/listinfo/nek5000-users
>>>>>>>
>>>>>> _______________________________________________
>>>>>> Nek5000-users mailing list
>>>>>> Nek5000-users at lists.mcs.anl.gov
>>>>>> https://lists.mcs.anl.gov/mailman/listinfo/nek5000-users
>>>>> _______________________________________________
>>>>> Nek5000-users mailing list
>>>>> Nek5000-users at lists.mcs.anl.gov
>>>>> https://lists.mcs.anl.gov/mailman/listinfo/nek5000-users
>>>>> _______________________________________________
>>>>> Nek5000-users mailing list
>>>>> Nek5000-users at lists.mcs.anl.gov
>>>>> https://lists.mcs.anl.gov/mailman/listinfo/nek5000-users
>>>> _______________________________________________
>>>> Nek5000-users mailing list
>>>> Nek5000-users at lists.mcs.anl.gov
>>>> https://lists.mcs.anl.gov/mailman/listinfo/nek5000-users
>>>> _______________________________________________
>>>> Nek5000-users mailing list
>>>> Nek5000-users at lists.mcs.anl.gov
>>>> https://lists.mcs.anl.gov/mailman/listinfo/nek5000-users
>>>
>>> _______________________________________________
>>> Nek5000-users mailing list
>>> Nek5000-users at lists.mcs.anl.gov
>>> https://lists.mcs.anl.gov/mailman/listinfo/nek5000-users
>>>
>> _______________________________________________
>> Nek5000-users mailing list
>> Nek5000-users at lists.mcs.anl.gov
>> https://lists.mcs.anl.gov/mailman/listinfo/nek5000-users
>
>
>
> _______________________________________________
> Nek5000-users mailing list
> Nek5000-users at lists.mcs.anl.gov
> https://lists.mcs.anl.gov/mailman/listinfo/nek5000-users

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