From e173066e175549a8b074921705f71e3cdbefa257 Mon Sep 17 00:00:00 2001 From: "Thomas D. Economon" Date: Sat, 1 Dec 2018 16:24:31 -0800 Subject: [PATCH 1/2] Removing options for DEFORM_TOL_FACTOR. --- Inviscid_2D_Unconstrained_NACA0012/inv_NACA0012_basic.cfg | 4 ++-- Inviscid_3D_Constrained_ONERAM6/inv_ONERAM6_adv.cfg | 4 ++-- Multi_Objective_Shape_Design/inv_wedge_ROE_multiobj_combo.cfg | 4 ++-- 3 files changed, 6 insertions(+), 6 deletions(-) diff --git a/Inviscid_2D_Unconstrained_NACA0012/inv_NACA0012_basic.cfg b/Inviscid_2D_Unconstrained_NACA0012/inv_NACA0012_basic.cfg index 7772636b..e5dada18 100644 --- a/Inviscid_2D_Unconstrained_NACA0012/inv_NACA0012_basic.cfg +++ b/Inviscid_2D_Unconstrained_NACA0012/inv_NACA0012_basic.cfg @@ -213,8 +213,8 @@ DEFORM_NONLINEAR_ITER= 1 % Print the residuals during mesh deformation to the console (YES, NO) DEFORM_CONSOLE_OUTPUT= YES % -% Factor to multiply smallest cell volume for deform tolerance (0.001 default) -DEFORM_TOL_FACTOR = 0.001 +% Minimum residual criteria for the linear solver convergence of grid deformation +DEFORM_LINEAR_SOLVER_ERROR= 1E-14 % % Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME, % WALL_DISTANCE, CONSTANT_STIFFNESS) diff --git a/Inviscid_3D_Constrained_ONERAM6/inv_ONERAM6_adv.cfg b/Inviscid_3D_Constrained_ONERAM6/inv_ONERAM6_adv.cfg index 1997c790..0742ea3e 100644 --- a/Inviscid_3D_Constrained_ONERAM6/inv_ONERAM6_adv.cfg +++ b/Inviscid_3D_Constrained_ONERAM6/inv_ONERAM6_adv.cfg @@ -312,8 +312,8 @@ DEFORM_LINEAR_SOLVER= FGMRES % Number of smoothing iterations for mesh deformation DEFORM_LINEAR_ITER= 500 % -% Factor to multiply smallest cell volume for deform tolerance (0.001 default) -DEFORM_TOL_FACTOR = 1E-6 +% Minimum residual criteria for the linear solver convergence of grid deformation +DEFORM_LINEAR_SOLVER_ERROR= 1E-14 % % Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME, % WALL_DISTANCE, CONSTANT_STIFFNESS) diff --git a/Multi_Objective_Shape_Design/inv_wedge_ROE_multiobj_combo.cfg b/Multi_Objective_Shape_Design/inv_wedge_ROE_multiobj_combo.cfg index 45231f4e..ab258ea1 100644 --- a/Multi_Objective_Shape_Design/inv_wedge_ROE_multiobj_combo.cfg +++ b/Multi_Objective_Shape_Design/inv_wedge_ROE_multiobj_combo.cfg @@ -337,8 +337,8 @@ DEFORM_NONLINEAR_ITER= 1 % Print the residuals during mesh deformation to the console (YES, NO) DEFORM_CONSOLE_OUTPUT= YES % -% Factor to multiply smallest cell volume for deform tolerance (0.001 default) -DEFORM_TOL_FACTOR = 1e-15 +% Minimum residual criteria for the linear solver convergence of grid deformation +DEFORM_LINEAR_SOLVER_ERROR= 1E-14 % % Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME, % WALL_DISTANCE, CONSTANT_STIFFNESS) From 24bd45e64f34b528079ea88aaef8b8b8413a4059 Mon Sep 17 00:00:00 2001 From: "Thomas D. Economon" Date: Wed, 13 Feb 2019 16:04:11 -0800 Subject: [PATCH 2/2] Adjusting transition case. --- .../transitional_BC_model_ConfigFile.cfg | 8 ++++++++ 1 file changed, 8 insertions(+) diff --git a/Transitional_Flat_Plate/transitional_BC_model_ConfigFile.cfg b/Transitional_Flat_Plate/transitional_BC_model_ConfigFile.cfg index a964bdc4..01ab967b 100644 --- a/Transitional_Flat_Plate/transitional_BC_model_ConfigFile.cfg +++ b/Transitional_Flat_Plate/transitional_BC_model_ConfigFile.cfg @@ -40,6 +40,14 @@ INC_DENSITY_INIT= 1.2 % % Initial velocity for incompressible flows (1.0,0,0 m/s by default) INC_VELOCITY_INIT= ( 50.1, 0.0, 0.0 ) +% +% List of inlet types for incompressible flows. List length must +% match number of inlet markers. Options: VELOCITY_INLET, PRESSURE_INLET. +INC_INLET_TYPE= VELOCITY_INLET +% +% List of outlet types for incompressible flows. List length must +% match number of outlet markers. Options: PRESSURE_OUTLET, MASS_FLOW_OUTLET +INC_OUTLET_TYPE= PRESSURE_OUTLET PRESSURE_OUTLET % --------------------------- VISCOSITY MODEL ---------------------------------% %