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Slip or Non-slip conditions?

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Old   March 7, 2018, 19:53
Default Slip or Non-slip conditions?
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nsi
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Dear CFD fellows!

Can I impose non-slip conditions at wall in an Euler equations solver (meaning, compressible and inviscid flow), or I MUST use slip conditions?

If latter, how do I impose slip conditions? I know for normal velocity, we have

vn = 0;

and for other primitive variables, we have

drho/dn = 0; dE/dn = 0 (dp/dn = 0);

but we still need two more.

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Old   March 8, 2018, 00:56
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Uwe Pilz
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It depends of what you try to simulate.

If thee are real walls, you need to use a non slip b.c.

If you have simply the borders at the region you want to simulate, but in reality the area/volume is more extended, use slip b.c.
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Old   March 8, 2018, 04:11
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Filippo Maria Denaro
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Euler equations are first order, therefore only one BC.s can be prescribed to be the problem well posed. If you would set no-slip BC.s how do you ensure the body is not-permeable?
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Old   March 13, 2018, 12:17
Default Boundary conditions for Euler equations
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Maybe this is obvious, but I would like to note that in implementing no-slip BC, it is not the same as in incompressible NS. For incompressible NS (assuming a collocated grid) you can literally set \mathbf{u} \cdot \mathbf{n} = 0. In my experience with compressible Euler equations you must use interpolation with a layer of ghost cells otherwise you run into problems. For the left BC: \frac{u_{1} + u_{-1}}{2} = u_{wall} \Rightarrow u_{1} = 2 u_{wall} - u_{-1}. In my experience (which could be due to programming errors) simplying setting u_{1} = 0, is not sufficient since you have to take into account the other primitive variables.
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Old   March 13, 2018, 15:54
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Quote:
Originally Posted by selig5576 View Post
Maybe this is obvious, but I would like to note that in implementing no-slip BC, it is not the same as in incompressible NS. For incompressible NS (assuming a collocated grid) you can literally set \mathbf{u} \cdot \mathbf{n} = 0. In my experience with compressible Euler equations you must use interpolation with a layer of ghost cells otherwise you run into problems. For the left BC: \frac{u_{1} + u_{-1}}{2} = u_{wall} \Rightarrow u_{1} = 2 u_{wall} - u_{-1}. In my experience (which could be due to programming errors) simplying setting u_{1} = 0, is not sufficient since you have to take into account the other primitive variables.
Thanks! What if it is not a left/right/top/bottom boundary, but an immersed body?
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Old   March 13, 2018, 23:09
Default BC for Euler equations
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Quote:
Originally Posted by nsi View Post
Thanks! What if it is not a left/right/top/bottom boundary, but an immersed body?
Unfortunately, I am not experienced in the immersed boundary method. I would look at the CFD book by Anderson or Versteeg. They might discuss type of situation. With that said, if I recall correctly Versteeg deals with more incompressible flow numerics.
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