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cG(1)cG(1) Eulerian Navier Stokes Formulation on NACA0018 aerofoil Implementation

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Hi, I'm trying to implement the algorithm above. I've gotten pretty far but I'm getting stuck writing the functions for delta1 and delta2. I'm not quite sure where to go from here. The code is getting cut off so here's a link as well: http://s7.postimg.org/pjninect7/navstk.png

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asked May 8, 2015 by srij93 FEniCS Novice (120 points)
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