Note
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Ahmed Body External Aerodynamics Simulation#
Objective#
Ahmed body is a simplified car model used for studying the flow around it and to predict the drag and lift forces. The model consists of a slanted back and a blunt front.
In this example, PyFluent API is used to perform Ahmed Body external aerodynamics simulation. which includes typical workflow of CFD Simulation as follows:
Importing the geometry/CAD model.
Meshing the geometry.
Setting up the solver.
Running the solver.
Post-processing the results.

Import required libraries/modules#
import ansys.fluent.core as pyfluent
from ansys.fluent.core import examples
from ansys.fluent.visualization import set_config
import ansys.fluent.visualization.pyvista as pv
Configure specific settings for this example#
set_config(blocking=True, set_view_on_display="isometric")
Launch Fluent session with meshing mode and print Fluent version#
session = pyfluent.launch_fluent(mode="meshing", cleanup_on_exit=True)
print(session.get_fluent_version())
Meshing Workflow#
Initialize the Meshing Workflow#
workflow = session.workflow
geometry_filename = examples.download_file(
"ahmed_body_20_0degree_boi_half.scdoc",
"pyfluent/examples/Ahmed-Body-Simulation",
)
workflow.InitializeWorkflow(WorkflowType="Watertight Geometry")
workflow.TaskObject["Import Geometry"].Arguments = dict(FileName=geometry_filename)
workflow.TaskObject["Import Geometry"].Execute()
Add Local Face Sizing#
add_local_sizing = workflow.TaskObject["Add Local Sizing"]
add_local_sizing.Arguments = dict(
{
"AddChild": "yes",
"BOIControlName": "facesize_front",
"BOIFaceLabelList": ["wall_ahmed_body_front"],
"BOIGrowthRate": 1.15,
"BOISize": 8,
}
)
add_local_sizing.Execute()
add_local_sizing.InsertCompoundChildTask()
workflow.TaskObject["Add Local Sizing"].Execute()
add_local_sizing = workflow.TaskObject["Add Local Sizing"]
add_local_sizing.Arguments = dict(
{
"AddChild": "yes",
"BOIControlName": "facesize_rear",
"BOIFaceLabelList": ["wall_ahmed_body_rear"],
"BOIGrowthRate": 1.15,
"BOISize": 5,
}
)
add_local_sizing.Execute()
add_local_sizing.InsertCompoundChildTask()
workflow.TaskObject["Add Local Sizing"].Execute()
add_local_sizing = workflow.TaskObject["Add Local Sizing"]
add_local_sizing.Arguments = dict(
{
"AddChild": "yes",
"BOIControlName": "facesize_main",
"BOIFaceLabelList": ["wall_ahmed_body_main"],
"BOIGrowthRate": 1.15,
"BOISize": 12,
}
)
add_local_sizing.Execute()
Add BOI (Body of Influence) Sizing#
add_boi_sizing = workflow.TaskObject["Add Local Sizing"]
add_boi_sizing.InsertCompoundChildTask()
add_boi_sizing.Arguments = dict(
{
"AddChild": "yes",
"BOIControlName": "boi_1",
"BOIExecution": "Body Of Influence",
"BOIFaceLabelList": ["ahmed_body_20_0degree_boi_half-boi"],
"BOISize": 20,
}
)
add_boi_sizing.Execute()
add_boi_sizing.InsertCompoundChildTask()
Add Surface Mesh Sizing#
generate_surface_mesh = workflow.TaskObject["Generate the Surface Mesh"]
generate_surface_mesh.Arguments = dict(
{
"CFDSurfaceMeshControls": {
"CurvatureNormalAngle": 12,
"GrowthRate": 1.15,
"MaxSize": 50,
"MinSize": 1,
"SizeFunctions": "Curvature",
}
}
)
generate_surface_mesh.Execute()
generate_surface_mesh.InsertNextTask(CommandName="ImproveSurfaceMesh")
improve_surface_mesh = workflow.TaskObject["Improve Surface Mesh"]
improve_surface_mesh.Arguments.update_dict({"FaceQualityLimit": 0.4})
improve_surface_mesh.Execute()
Describe Geometry, Update Boundaries, Update Regions#
workflow.TaskObject["Describe Geometry"].Arguments = dict(
CappingRequired="Yes",
SetupType="The geometry consists of only fluid regions with no voids",
)
workflow.TaskObject["Describe Geometry"].Execute()
workflow.TaskObject["Update Boundaries"].Execute()
workflow.TaskObject["Update Regions"].Execute()
Add Boundary Layers#
add_boundary_layers = workflow.TaskObject["Add Boundary Layers"]
add_boundary_layers.AddChildToTask()
add_boundary_layers.InsertCompoundChildTask()
workflow.TaskObject["smooth-transition_1"].Arguments.update_dict(
{
"BLControlName": "smooth-transition_1",
"NumberOfLayers": 14,
"Rate": 1.15,
"TransitionRatio": 0.5,
}
)
add_boundary_layers.Execute()
Generate the Volume Mesh#
generate_volume_mesh = workflow.TaskObject["Generate the Volume Mesh"]
generate_volume_mesh.Arguments.update_dict({"VolumeFill": "poly-hexcore"})
generate_volume_mesh.Execute()
Switch to the Solver Mode#
session = session.switch_to_solver()
Mesh Visualization#


Solver Setup and Solve Workflow#
Define Constants#
density = 1.225
inlet_velocity = 30
inlet_area = 0.11203202
Define Materials#
session.tui.define.materials.change_create("air", "air", "yes", "constant", density)
session.settings.setup.models.viscous.model = "k-epsilon"
session.settings.setup.models.viscous.k_epsilon_model = "realizable"
session.settings.setup.models.viscous.options.curvature_correction = True
Define Boundary Conditions#
inlet = session.settings.setup.boundary_conditions.velocity_inlet["inlet"]
inlet.turbulence.turb_intensity = 0.05
inlet.momentum.velocity.value = inlet_velocity
inlet.turbulence.turb_viscosity_ratio = 5
outlet = session.settings.setup.boundary_conditions.pressure_outlet["outlet"]
outlet.turbulence.turb_intensity = 0.05
Define Reference Values#
session.settings.setup.reference_values.area = inlet_area
session.settings.setup.reference_values.density = density
session.settings.setup.reference_values.velocity = inlet_velocity
Define Solver Settings#
session.tui.solve.set.p_v_coupling(24)
session.tui.solve.set.discretization_scheme("pressure", 12)
session.tui.solve.set.discretization_scheme("k", 1)
session.tui.solve.set.discretization_scheme("epsilon", 1)
session.tui.solve.initialize.set_defaults("k", 0.000001)
session.settings.solution.monitor.residual.equations["continuity"].absolute_criteria = (
0.0001
)
session.settings.solution.monitor.residual.equations["x-velocity"].absolute_criteria = (
0.0001
)
session.settings.solution.monitor.residual.equations["y-velocity"].absolute_criteria = (
0.0001
)
session.settings.solution.monitor.residual.equations["z-velocity"].absolute_criteria = (
0.0001
)
session.settings.solution.monitor.residual.equations["k"].absolute_criteria = 0.0001
session.settings.solution.monitor.residual.equations["epsilon"].absolute_criteria = (
0.0001
)
Define Report Definitions#
session.settings.solution.report_definitions.drag["cd-mon1"] = {}
session.settings.solution.report_definitions.drag["cd-mon1"] = {
"zones": ["wall_ahmed_body_main", "wall_ahmed_body_front", "wall_ahmed_body_rear"],
"force_vector": [0, 0, 1],
}
session.parameters.output_parameters.report_definitions.create(name="parameter-1")
session.parameters.output_parameters.report_definitions["parameter-1"] = {
"report_definition": "cd-mon1"
}
session.settings.solution.monitor.report_plots.create(name="cd-mon1")
session.settings.solution.monitor.report_plots["cd-mon1"] = {"report_defs": ["cd-mon1"]}
Initialize and Run Solver#
session.settings.solution.run_calculation.iter_count = 5
session.settings.solution.initialization.initialization_type = "standard"
session.settings.solution.initialization.standard_initialize()
session.settings.solution.run_calculation.iterate(iter_count=5)
Post-Processing Workflow#
session.results.surfaces.iso_surface.create(name="xmid")
session.results.surfaces.iso_surface["xmid"].field = "x-coordinate"
session.results.surfaces.iso_surface["xmid"] = {"iso_values": [0]}
graphics_session1 = pv.Graphics(session)
contour1 = graphics_session1.Contours["contour-1"]
contour1.field = "velocity-magnitude"
contour1.surfaces_list = ["xmid"]
contour1.display("window-1")
contour2 = graphics_session1.Contours["contour-2"]
contour2.field.allowed_values
contour2.field = "pressure-coefficient"
contour2.surfaces_list = ["xmid"]
contour2.display("window-2")
Simulation Results Visualization#

Velocity Magnitude Contour

Pressure Coefficient Contour
Save the case file#
session.settings.file.write(file_type="case-data", file_name="ahmed_body_final.cas.h5")
Close the session#
session.exit()
References#
[1] S.R. Ahmed, G. Ramm, Some Salient Features of the Time-Averaged Ground Vehicle Wake,SAE-Paper 840300,1984