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May 1, 2011, 23:42 
Poisson equation,Neumann BCs

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vivien
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Hi~all
I need to solve a pressure Poisson equation with only Neumann boundaries with F.D. method. Unfortunately, it leads to the sparse linear system equation Ax = b, where A is singular (because the Neumann BC in all boundaries).And I use matlab ....Any advise with possibility to solve singular linear systems? Thank you~ 

May 2, 2011, 02:35 

#2  
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Arjun
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pick any boundary cell treat it as fixed value of say 0. So all the boundary faces have neumann condition except for 1. if you do so, your equation will no longer be singular. Then use whatever matrix solver you want to solve the system. 

May 2, 2011, 20:09 

#3 
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I think that you can fix any point at the boundary (as mentioned by arjun) or anywhere within the computational domain.
__________________
 Julien de Charentenay 

May 3, 2011, 10:29 

#4 
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vivien
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Hi
I've tried it ,but it seems that it's still hard to solve the equations. In fact my problem is ∂²p/∂x²+∂²p/∂y²= ∂u(x,y)/∂x+∂v(x,y)/∂y u(x,y) and v(x,y) are known in all points with 1 Dirichlet BC on west and 3 N BCs on the others. (uu(x,y),vv(x,y))=( u(x,y), v(x,y) )(∂p/∂x,∂p/∂y) uu(x,y) and vv(x,y) have the same boudary with u(x,y) and v(x,y). And p(x,y) is N BCs according to the paper . But I don't know how to figure out the boundary conditions of p ...any advise?Thank you all~ 

May 3, 2011, 20:30 

#5  
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Arjun
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If you tried and it does not work then there are many possiblities: 1. You made mistake in implementing what is advised. 2. If matlab is using direct solver to solve that matrix system then point (1) is your only possiblity. 3. If matlab is using iterative method then it shall be noted that not all iterative solvers can solve all neumann problem (it also depends on size of your problem). As the size increases the difficulty in solving increases. 4. Usually though (3) only reduces rate of convergence that means you would observe some convergence but it would be converging very slowly. When the problem size increase after some point there will be virtually no convergence. PS: In the end if you are using finite difference and you mesh is cartesian mesh then have a look at fishpack and its routine called blktri . (But i think it can also not handle all neumann problem, but have a look to make sure). 

January 27, 2014, 12:00 
Implementing pure Neumann Boundary conditions for Poisson equations with FD method

#6  
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Patricio Cumsille
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Thank you very much in advance Best regards, Patricio Cumsille 

January 27, 2014, 14:56 

#7  
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Filippo Maria Denaro
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You can fix the value of the solution in anyone of the grid points. However, this is not necessary, the system admits infinite solutions and during a linear solver, your solution automatically sets a constant reference value. 

January 27, 2014, 19:23 

#8 
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adrin
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Not setting a Dirichlet BC for at least one point will not lead to a converged solution unless the implementation is noisy enough to remove the matrix singularity just enough (for convergence to take place).
On the other hand, setting a node value to a constant Dirichlet BC, as proposed in this thread, is a poor choice/strategy as well. Yes, it allows for the matrix to converge, but it yields a spike at, and in the immediate neighborhood of, the point the Dirichlet BC is applied. A few years ago, I'd developed (and published) a highly accurate and inexpensive solution, without a spike, in a boundary element methods setting. I've just begun searching for similarly accurate methods in a finitedifference/volume approach, but I haven't yet found an easytoimplement and/or inexpensive strategy! Adrin 

January 27, 2014, 21:45 

#9 
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Patricio Cumsille
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Thank you very much for the responses.
Adrin: Please, could you send to me your publication? I am interested! My email is pcumsill@gmail.com Thank you again! Best regards, PC 

January 28, 2014, 03:54 

#10  
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January 28, 2014, 04:36 

#11  
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Filippo Maria Denaro
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well, this is not an issue of CFD but a mathematical property... The Poisson equation Div Grad (phi) = q with Neumann BC.s admits a solution (apart a constant) provided that the compatibility relation is satisfied. This does not require complicate implementation of the BC.s but only the fact that: Int [S] d phi/dn dS = Int [S] q dS The CFD task consists in fulfill such relation in discrete sense. It is a common experience that fixing an arbitrary value leads to a slower convergence 

January 28, 2014, 06:03 

#12 
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My experience agrees with that of adrin, for scale resolving simulations (e.g., LES/DNS) pressure should not be fixed, otherwise you cannot get the right statistics from it. Still, there should be no problem for the momentum equations


January 28, 2014, 17:55 

#13 
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Filippo Maria Denaro
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Let me say that the correct way to fix a value must accord with the correct BCs otherwise you get convergence towards some uncorrect solution
Try to fix the value not in the interior but by entering it by means of the Neumann BCs, it should work correctly without spike. However, as I said, the convergence rate is slower. 

January 28, 2014, 18:12 

#14 
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adrin
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>>>it should work correctly without spike. However, as I said, the convergence rate is slower.
Well, I happen to be working on this problem these days, and I can say that a pure neumann BC without any other modifications will _not_ work! I'm using a multigrid preconditioned krylov solver (PCG), which converges in ~10 iterations (to error of order 1.E8) for the 3D poisson problem that I've tried. With a pure neumann BC the solution does not converge to even order 1.E3 for up to 3000 iterations, which is the upper limit I set. In contrast, setting one of the boundary nodes to zero (dirichlet BC) leads to convergence in 7 iterations! I agree that convergence doesn't necessarily mean convergence to a correct solution (but in this case it seems it does) Adrin 

January 28, 2014, 18:18 

#15  
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Filippo Maria Denaro
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Adrin, something in the BC implementation could be wrong... I assume you are working on the pressure problem derived from the continuity equation in which you substitute the Hodge decomposition. The same decomposition, projected along the normal direction to the boundaries provides the correct Neumann BC.s that fulfill the compatibility relation ensuring the convergence. I work usually with Neumann BC.s and it works.... Please, check if your BC.s satisfy numerically the relation Int [S] d phi/dn dS  Int [S] q.n dS=0 

January 28, 2014, 22:16 

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adrin
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>> could you point to the paper you published
A. Gharakhani and A. F. Ghoniem,"BEM Solution of the 3D Internal Neumann Problem and A Regularized Formulation for the Potential Velocity Gradients," International Journal of Numerical Methods in Fluids, Vol. 24, No. 1, pp. 81100, 1997. 

January 29, 2014, 09:24 

#17 
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I remember having a possibly identical problem with a Vortex panel method applied to closed surfaces with lift (in practice the outside potential is well defined by its behavior at infinity, but the inside one is not). However, there the problem can be easily solved by assigning the circulation value for a panel as, just like the pressure, the solution is in terms of differences of circulations among adjacent panels and not their absolute values. Still, i never had the chance to apply the method to multiple closed surfaces to see if it really doesn't matter in general...
Actually, Adrin himself helped me in solving my issue here on CFDONLINE (3D PANEL METHOD ). I should read your paper to check if the matter is exactly the same. Coming to the general issue, i guess that you both (Adrin and Filippo) are saying exactly the same thing, one of the equations should be switched to a global constraint instead of fixing it arbitrarily. However, there might possibly be differences in the single approaches. I guess that if pressure has infinitely many solutions, the solution should simply converge to one of them just like for the pressure checkerboard case the solution converge to a specific checkerboard pattern. My experience is that point GaussSeidel iterations can converge to machine accuracy (not so fast actually) if the global b.c. constraint is preserved. However, this global constraint implies a full coupling among the equations which might be difficult to solve in the context of an otherwise banded matrix. 

February 4, 2014, 18:02 

#18  
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Patricio Cumsille
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The problem I see is that the convergence rate is really slow. I have carried out some numerical tests and I got a convergence rate even less than 1!!! Or even worst, for certain problems (for certain data) I did not get convergence! Thus, the technique of fixing a value at a grid point is not good in general!!! 

February 6, 2014, 03:27 

#19  
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Yes, this was the main problem I faced when I tried to fix a single point for neumann. Even the additive corrective AMG was not that effective specially when case sizes were large. If you could use, try smoothed aggregation AMG. I ended up taking out additive corrective and replacing it with smoothed aggregation that worked well. Arjun 

March 25, 2014, 17:01 
Revisiting Neumann BC

#20 
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adrin
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It turns out that FMDenaro is correct. So long as the Neumann BC compatibility is satisfied _explicitly_ one need not set a Dirichlet BC at one node, and one can still get a solution. In my previous experiments in the finite volume formulation I was using a simple manufactured problem for benchmarking. It turns out that although compatibility was theoretically ensured it was _not_ satisfied numerically (in discrete form). So, a simple correction led to "a" solution. That solution shifts by a constant as a function of grid resolution, but that's not an issue. I still maintain the only reason any solution may be obtained with such an approach is sufficient numerical noise to remove the linear dependence of two arbitrary equations  this approach would fail in an "infinite accuracy" solution.
So, in summary, if the _discrete_ surface integral of the fluxes is not equal to the volume integral of the Poisson source term, perform the following preprocessing before assembling the matrix and RHS. Find the difference between the aforementioned two terms, and either (a) divide that difference by the total volume and then add the volume averaged error to the source term for every node, or (b) divide the difference by the total surface area and then add the surface averaged error to the fluxes on all surface nodes. Make sure the signs are such that compatibility is now satisfied. This yields a quick, converged solution! Adrin 

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neumann bcs, poisson equation 
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