|
[Sponsors] |
November 1, 2016, 22:43 |
second order scheme problem
|
#1 |
New Member
Join Date: Nov 2016
Posts: 2
Rep Power: 0 |
Hi every one,
I'm solving a shock tube problem using a Roe scheme (structured grids) which works fine on first order accuracy. I want to improve the solution to higher order starting from second order. I simply extrapolate the solution from the cell centers to faces using the gradients: Uface=Ucenter+Grad_U*r where r is the distance between the face and center. using this second order Taylor series I manage to improve the solution in the expansion region but the shock capturing is exactly the same as the first order solution. I use a MidMode slope limiter for the second order solution. I can's see where the problem is. any experiences? |
|
Tags |
limiter, roe scheme, second order accuracy, shock-tube |
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
Differencing Scheme for Advection Problem | Simon Smokes | Main CFD Forum | 2 | April 8, 2015 10:59 |
Implementation of 2nd order upwind scheme | jaason | OpenFOAM Running, Solving & CFD | 4 | February 6, 2015 17:40 |
higher order discretisation scheme | Simon Smokes | Main CFD Forum | 2 | August 23, 2014 07:19 |
2nd order upwind vs 2nd order upwind!!! | Far | Main CFD Forum | 7 | March 14, 2013 12:29 |
Discretisation scheme in CFX-1st or 2nd order? | Pete | CFX | 10 | January 12, 2005 12:48 |