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Aerospace Hyperbolic Equation Instability

  1. Jun 29, 2011 #1
    Hello,

    I'm trying to calculate the following equation which is the derivative in 'x' of a distribution function:
    d(dxF)/dt = d(Efield.(dvxF))/dx

    The problem comes because the right hand of the equation is solved by using central difference, but there is a zone where there is a discontinuity in the electric field. The electric field is not exactly the same on each point (but more or less the same order of magnitude) but there is a zone where I have in increment so the difference between two adjacent grid is so big that creates an instability. Is there any way to smooth the numerical scheme?

    = (E[i+1][j]. dvxF[i+1][j]-E[i-1][j].dvxF[i-1][j])/dx

    This is more or less how it goes. Imagine there is a point where the difference between E[i+1][j] and E[i-1][j] is so big that, creating a big gradient in the dxF value.

    I've been studying the MUSCL and TVD schemes but i don't quite understand well the procedure
     
  2. jcsd
  3. Jun 29, 2011 #2

    boneh3ad

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    Did you really mean to put this in the aerospace engineering forum?
     
  4. Jun 29, 2011 #3
    Yes because I'm simulating an MHD accelerator, is just a specific problem I have. But if its not the correct place I can post it in another forum. Sorry about that
     
  5. Jun 29, 2011 #4

    boneh3ad

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    No I was just curious. It is just not something I am familiar with I suppose. Then again, I am not a numerical methods guy.
     
  6. Jun 29, 2011 #5

    minger

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    TVD schemes are a good place to start. If you search on CFD "Shock Capturing" Schemes, you'll find a lot of resources that should be applicable.

    Essentially, at the core, what you would like to do is use local gradients to switch between your central differencing scheme (no numerical dissipation) and a low-order upwinding scheme (lots of numerical dissipation).

    As a first cut, try solving using both methods and use a weighted average of a local gradient to determine the weightings. At that point near your discontinuity, force your solver to use the low-order scheme; this could help your stability.
     
  7. Jun 30, 2011 #6
    minger, thank you very much for your advise
     
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