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Navier-Stokes NACA Regression Tests

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titleGeneral Case Information

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titleInputs:
  • Common flow parameters:
    • Freestream Mach number: M = 0.5
    • Angle of attack: α = 0 °
    • Total pressure: Pt =
    • Total temperature: Tt =
    • Static temperature:
    • CFL: 1030
  • Common solver parameters:
    • Preconditioning:
      • Outer GMRES iterations (no. restarts): 20
      • Inner GMRES iterations (no. Krylov vectors): 200
    • Solution order: 2
    • PSequencing: False
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title

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Inputs:

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  • Input Geometry:
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Common Flow Parameters
titleInputs:
  • Common flow parameters:
    • Freestream Mach number: M =
??
    • 0.5
    • Angle of attack: α =
??
    • 0 °
  • Reynolds Number: Re = ??
    • Common Solver Parameters:
      • blah
      • blah
      • blah
    Representative Solution:
    Image Removed
      • Total pressure: Pt =
      • Total temperature: Tt =
      • Static temperature:
      • CFL: 1030
    • Common solver parameters:
      • Preconditioning:
        • Outer GMRES iterations (no. restarts): 20
        • Inner GMRES iterations (no. Krylov vectors): 200
      • Solution order: 2
      • PSequencing: False
    Column
    width50%
    Panel
    titleInputs:

    Image Added

    • Representative Solution:

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    Panel
    titleSpecific Test Case information

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