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Let's test some of the ProjectX solvers for the case of a NACA0012 (? check ?) airfoil (2D) in compressible, inciscid flow:

Panel
titleParameters:
  • asdflk<html>M_</html>
  • dfd

< insert grid image here > < insert primal solution here >

Panel
titleSome solverNewton-Jacobi (Right)

what this solver tests
result

Panel
titleNewton-Jacobi

what this solver tests
result

Panel
titleNewton-ILU

what this solver tests
result

Panel
titleNewton-ILUTSome other solver

what this solver tests
result