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| This circle boundary layer case involves a heat source being applied to a vortex flow around a circular annulus of radius r = [ 1 , 2 ]. The numerical heat flux at the inner boundary is checked with the analytical heat flux at the inner boundary to a specified tolerance. All boundaries are set to a thermal condition which is a function of r and θ. The applied heat source is also a function of r and θ, and the initial condition is set to 1. |
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title | Temperature Distribution: |
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Case Specific Details
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title | Case 1 (Non-Adaptive): |
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| - Solution Order: 2
- Iterations to solve: 2
- All outputs tested to a tolerance of 10-12
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| - Solution Order = 1
- Additional tested outputs: Heat flux adjoint residual
- Adaptation parameters:
- Adaptation Iterations: 2
- Adaptation Method: Fixed fraction
- Output Adapted: Heat flux
- Anisotropy Method: Hessian
- Iterations to solve on each mesh: 2
- All outputs tested to a tolerance of 10-10
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title | Case 2 Adapted Meshes: |
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graphs:
what is tested?
- Heat Flux on Boundary Group 1
- L2 error of ExactSolutionFunction = ScalarBoundaryLayer2
equations
- Scalar 2D
- Solution order = 2
- Basis Type = Lagrange
flow conditions
- SourceFunction = ScalarBoundaryLayer2Source
- Viscosity = 1e-2
- VelocityFunction = Horizontal
numerical parameters
- CFL = 1e30
- # of Iterations = 5
- Nonlinear Solver = Newton
- Direct
- GMRES ILU
- Preconditioner = ILU
- Preconditioner Side = Left
- # GMRES outer iterations = 20
- # GMRES inner iterations = 20
- GMRES Jacobi
- Preconditioner = Jacobi
- Preconditioner Side = Left
- # GMRES outer iterations = 20
- # GMRES inner iterations = 200
results or convergence
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- Residual Norm = e-16 in 2 iterations
- Heat Flux converges to 3.745e-04 in 2 iterations
- L2Error converges to 2.533e-09 in 2 iterations
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Case Details
MixedMesh_Scalar2d_Direct
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