NACA Regression Tests


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

  • M-\infty-
  • dfd

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

what this solver tests
result

what this solver tests
result

what this solver tests
result

what this solver tests
result