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Panel
titleGeneral Case Information

Panel
  • Input Geometry:
    Image Removed Image Removed
  • Common Flow Parameters:
    • Freestream Mach number: M ∞ = ??
    • Angle of attack: α = ?? °
    • Reynolds Number: Re = ??
  • Common Solver Parameters:
    • blah
    • blah
    • blah
  • Representative Solution:

...

Section
Column
width50%
Panel
title+Newton-GMRES-ILUSubsonic - Uniform Adaptation+

Job File: naca_NavierStokes2d_Newton_GMRES_ILU_TEST.job

  • Input Geometry:
    Image Added Image Added
  • Nonlinear solver:
    • Newton
  • Preconditioner:
    • Block Jacobi (left)
  • Adapted Geometry:
    Image Added Image Added
Column
width50%
Panel
title+Newton-GMRES-ILUTTransonic - Uniform Adaptation+

Job File: naca_NavierStokes2d_Newton_GMRES_ILUT_TEST.job*

  • Input Geometry:
    Image Added Image Added
  • Nonlinear solver:
    • Newton
  • Preconditioner:
    • Block Jacobi (right)
Section
Column
width50%
Panel
title+Viscous Discretization (BR2) - Flux CoefficientCutcell - Subsonic - Uniform Adaptation+

Job File: naca_NavierStokes2d_AuxVariable_FluxCoeff_TEST.job

  • Input Geometry:
    Image Added Image Added
  • Nonlinear solver:
    • Newton
  • Preconditioner:
    • Block Jacobi (left)
Column
width50%
Panel
title+Viscous Discretization (BR2) - GradientNot sure what this one is+

Job File: naca_NavierStokes2d_AuxVariable_Gradient_TEST.job

  • Nonlinear solver:
    • Newton
  • Preconditioner:
    • Block Jacobi (right)
Section
50%
Column
width50%
Panel
title+Unified Adaptation+
Job File: naca_NavierStokes2d_UniAdapt_TEST.job
  • Input Geometry:
  • Nonlinear solver:
    • Newton
  • Preconditioner:
    • Block Jacobi (right)
Column
width