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-   -   2nd order TVD scheme (https://www.cfd-online.com/Forums/main/114561-2nd-order-tvd-scheme.html)

Wenjun March 13, 2013 08:03

2nd order TVD scheme
 
3 Attachment(s)
Hi, I am learning the second order TVD scheme which is listed in the attachment, and I want to verify the order of the scheme by the linear advection equation u_t+u_x=0, periodic BC, initial condition u0=sin(pi*x), x in [0, 2]. But the order I got is about 1.3, and the wave shape becomes flat at valley and peak. Why is the order less than 2 ? My code is in the attachment too. Thank you very much for your kind reply.Attachment 19828

Attachment 19829

Attachment 19830

cfdnewbie March 13, 2013 16:01

looks like your TVD limiter works as expected and cuts off your peaks when a grid point coincides with the maxima/minina.
Your initial projection looks ok, you should approach second order when refining the mesh. Order of convergence is a concept of h to zero, from your plot it looks like h is 2/6....

Wenjun March 13, 2013 20:45

Thank you for your consideration. But even if I choose the step h=2/6,2/12..., the order is almost the same as before. I don't know why. I have already checked my code for several times.

Wenjun March 13, 2013 20:55

I use the L1 error for order calculation, it confirms the second order accuracy. However, L_\infty does not work. Normally the two different measure both can confirm the order. Do you have some idea about this problem?

cfdnewbie March 14, 2013 02:06

The L infty will always be dominated by the limiter at the maxima, so since you are doing a first order approximation at the maxima (see your plot, the maxima are approximated by constants, not linears), the L infty will not give you second order. The L1 and L2 will converge to second order, since the influence of the "bad region" will decrease with increasing h!

k_tafazoli March 14, 2013 02:24

Hi, I've got a fortran code for solving flow over an airfoil with the method of first order van leer flux vector splitting . I have to change it to second order . Do you know how I can do that ? can you help me with it ?

Wenjun March 14, 2013 02:25

Yes, I understand now. I tried L1, it works. Thank you very much. It is my pleasure to meet you in the forum.

Wenjun March 14, 2013 02:51

Sorry, I only code by Matlab. I am a fresh guy in CFD and my problem is rather simple.

k_tafazoli March 14, 2013 12:31

Thanks anyway


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