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NACA Regression Tests

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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
  • dfd

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

Panel
titleSome solver

what this solver tests
result

Panel
titleSome other solver

what this solver tests
result