Boundary Names for other examples

trixi-framework · Mar 19, 2024 · a198ee0 · a198ee0
1 parent d914526
commit a198ee0
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diff --git a/examples/p4est_2d_dgsem/elixir_euler_subsonic_cylinder.jl b/examples/p4est_2d_dgsem/elixir_euler_subsonic_cylinder.jl
@@ -91,14 +91,14 @@ rho_inf = 1.4
 U_inf = 0.38
 linf = 1.0 # Diameter of circle
 
-drag_coefficient = AnalysisSurfaceIntegral(semi, boundary_condition_slip_wall,
+drag_coefficient = AnalysisSurfaceIntegral(semi, :x_neg,
                                            DragCoefficient(aoa, rho_inf, U_inf, linf))
 
-lift_coefficient = AnalysisSurfaceIntegral(semi, boundary_condition_slip_wall,
+lift_coefficient = AnalysisSurfaceIntegral(semi, :x_neg,
                                            LiftCoefficient(aoa, rho_inf, U_inf, linf))
 
 analysis_callback = AnalysisCallback(semi, interval = analysis_interval,
-                                     output_directory = "analysis_results",
+                                     output_directory = "out",
                                      save_analysis = true,
                                      analysis_integrals = (drag_coefficient,
                                                            lift_coefficient))

diff --git a/examples/p4est_2d_dgsem/elixir_navierstokes_NACA0012airfoil_mach08.jl b/examples/p4est_2d_dgsem/elixir_navierstokes_NACA0012airfoil_mach08.jl
@@ -115,16 +115,17 @@ summary_callback = SummaryCallback()
 
 analysis_interval = 2000
 
-drag_coefficient = AnalysisSurfaceIntegral(semi, boundary_condition_slip_wall,
+force_boundary_names = [:AirfoilBottom, :AirfoilTop]
+drag_coefficient = AnalysisSurfaceIntegral(semi, force_boundary_names,
                                            DragCoefficient(sw_aoa(), sw_rho_inf(),
                                                            sw_U_inf(equations), sw_linf()))
 
-lift_coefficient = AnalysisSurfaceIntegral(semi, boundary_condition_slip_wall,
+lift_coefficient = AnalysisSurfaceIntegral(semi, force_boundary_names,
                                            LiftCoefficient(sw_aoa(), sw_rho_inf(),
                                                            sw_U_inf(equations), sw_linf()))
 
 analysis_callback = AnalysisCallback(semi, interval = analysis_interval,
-                                     output_directory = "analysis_results",
+                                     output_directory = "out",
                                      save_analysis = true,
                                      analysis_integrals = (drag_coefficient,
                                                            lift_coefficient))