Dear Howe,

`Regarding 1., the main question is whether you added the 'mapping'`

`variable as the first arguments to all FEValues and FEFaceValues`

`constructors, to calls to VectorTools::interpolate* and`

`VectorTools::integrate_difference calls and the like, i.e., all routines`

`that internally construct an FEValues or FEFaceValues object. There is`

`defaults for many of those data structures using linear mappings,`

`MappingQ1, but you don't want to use them but rather the high order`

`description.`

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`Regarding 2, I guess you are using a curved boundary description as`

`explained in step-1? You need to tell the triangulation to use a curved`

`description.`

`Regarding 3, your mesh looks quite good. You would probably want to use`

`a volume manifold on the whole circular part of the domain, though. And`

`ideally a TransfiniteInterpolationManifold on the regions where you go`

`from the circle to the straight ends, but the latter is not yet`

`available in any of the releases yet, only the github code, and it is`

`not critical and you should get better results up to degree 3 at least.`

Best, Martin On 09.08.2017 10:06, Howe wrote:

Dear Martin, Thanks for your rapid response. 1.The MappingQ is set to be the same as the order of velocity, as isshown in the following code snippet:/template <int dim> //NS<dim>::NS (ParameterHandler &prm) //: // parameters (&prm), // degree (prm.get_integer("pressure degree")), // fe( FE_Q<dim>(QGaussLobatto<1>(degree+2)), dim, // FE_Q<dim>(QGaussLobatto<1>(degree+1)), 1), // fe_scalar (FE_Q<dim>(QGaussLobatto<1>(degree+2))), // dof_handler (triangulation), // dof_handler_scalar (triangulation), //mapping (degree+2), // computing_timer (std::cout, // TimerOutput::summary, // TimerOutput::wall_times)/I am not quite sure whether the computation of the lift/drag in mycode is right, and my implementation is almost the same as the one inthis post:https://groups.google.com/d/msg/dealii/rS6soTb69ig/C4QchAyEGwAJThe only change is the first line : /QGauss<dim-1> face_quadrature_formula(degree+2);/2. I am using deal.II 8.4.0 now, and I think i am not using manifolddescription in my code3. The mesh is shown as follows: <https://lh3.googleusercontent.com/-Vs0s6So28js/WYrCbyok9mI/AAAAAAAABSc/rfs-1D1TA8c71IQZpOEyOoU3C1idNr1DQCLcBGAs/s1600/Image.png> Best, Howe 在 2017年8月9日星期三 UTC+8下午3:25:20，Martin Kronbichler写道： Dear Howe, How did you run your simulation? From your picture, it appears that a higher order method is worse at higher degrees than a lower order method, which does not match with my experience. If that were the case, nobody would use high orders. However, you need to bring many pieces in place to really get to the benefit of the high order method for somewhat more complicated examples such as the flow around a cylinder. Here is a list of things to look at: - Do you use a high-order polynomial mapping MappingQ of the same or higher degree as the interpolation space? Do you use this mapping in all routines that evaluate quantities, such as the usual assembly, the computation of the lift/drag, and so on? - Do you use a manifold description that extends into the domain? (Look into TransfiniteInterpolationManifold.) Without, you will not get more than third order convergence. - Do you have a good mesh around the area of interest? Flows around cylinders tend to be really really sensitive to the mesh quality around the cylinder. For the Navier-Stokes equations around the cylinder, if everything is done right one gets significantly improved results in terms of accuracy over the number of degrees of freedom up to degree (6,5) (velocity,pressure). Beyond that picture is less clear. At least with the meshes that we tried in our group it was not worth to go beyond. You can have a look a our results in section 5.4 and Figs. 9 and 10 of this preprint: https://arxiv.org/pdf/1706.09252.pdf <https://arxiv.org/pdf/1706.09252.pdf> Best, Martin On 09.08.2017 09:01, Howe wrote:Dear Jaekwang Have you solved this problem? If yes, Could pls share your solution with us? I am simulating a steady state flow over a cylinder, and the drag/lift coefficient shows an unexpected trend of change as i increase the discretization order and refine the mesh. <https://lh3.googleusercontent.com/-Gz5932Zt6e0/WYqvbO3P-4I/AAAAAAAABSM/6hBHn1FO5W0P7X3SPfQ4iyRaldDYzOt3QCLcBGAs/s1600/Image.png> As is shown in the figure, the Cd increased as the cells increased for all the discretization orders, however, for a fixed cells, the Cd decreased as the discretization order increased. In my opinion, to increase the order and refine the mesh should both make the approximation more close to the exact solution, thus should have the same trend of change. 在 2016年9月18日星期日 UTC+8下午11:57:16，Jaekwang Kim写道： Hello, I am a starter of dealii and am learning a lot these days with the help of video lectures and tutorial examples. I modified step-22 code (stokes flow code) into my own problem, the flow around sphere. and I intend to evaluate the drag force (which is analytically given by stokes equation) My code reached quite close to the value since the absolute error : abs(drag_calculated-drag_exact)/drag_exact is around 10^(-3) However, I expected that if I input higher 'degree' I will receive more accurate result, but it didn't Obviously Q2 is better than Q1. and Q3 is better than Q2. But Q4 or Q4 is not better than Q2 or Q3? Is there any reason on this? (To be specific, if i say degree 2 , that mean I use (2+1) for velocity, (2) for pressure, and (2+2) for Gauss integral.... Thank you Jaekwang Kim--The deal.II project is located at http://www.dealii.org/For mailing list/forum options, see https://groups.google.com/d/forum/dealii?hl=en <https://groups.google.com/d/forum/dealii?hl=en> --- You received this message because you are subscribed to the Google Groups "deal.II User Group" group. To unsubscribe from this group and stop receiving emails from it, send an email to dealii+un...@googlegroups.com <javascript:>. 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