NACA Regression Tests
Let's test some of the ProjectX solvers for the case of a NACA0012 (? check ?) airfoil (2D) in compressible, inciscid flow:
Parameters:
- <html>M_</html>
- dfd
< insert grid image here > < insert primal solution here >
Newton-Jacobi (Right)
what this solver tests
result
Newton-Jacobi
what this solver tests
result
Newton-ILU
what this solver tests
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Newton-ILUT
what this solver tests
result