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RANS - RAE2822 Regression Tests

Panel
titleGeneral Case Information

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

Panel
titleSpecific Test Case information

Section
Column
width50%
Panel
title+Subsonic - Uniform Adaptation+

Job File: naca_NavierStokes2d_Newton_GMRES_ILU_TEST.job

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

Job File: naca_NavierStokes2d_Newton_GMRES_ILUT_TEST.job*

  • Input Geometry:
  • Nonlinear solver:
    • Newton
  • Preconditioner:
    • Block Jacobi (right)
  • Adapted Geometry:
Section
Column
width50%
Panel
title+Cutcell - Subsonic - Uniform Adaptation+

Job File: naca_NavierStokes2d_AuxVariable_FluxCoeff_TEST.job

  • Input Geometry:
  • Nonlinear solver:
    • Newton
  • Preconditioner:
    • Block Jacobi (left)
Column
width50%
Panel
title+Not sure what this one is+

Job File: naca_NavierStokes2d_AuxVariable_Gradient_TEST.job

  • Input Geometry:
  • Nonlinear solver:
    • Newton
  • Preconditioner:
    • Block Jacobi (right)