integrate geometry, surface and volume mesher

examples/geometry_from_csm_file.py

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+import flow360 as fl
+from flow360.component.geometry import Geometry
+from flow360.examples import Airplane
+
+fl.Env.preprod.active()
+
+geometry_draft = Geometry.from_file(
+    Airplane.geometry,
+    name="testing-airplane-csm-geometry",
+)
+geometry = geometry_draft.submit()
+
+print(geometry)

examples/geometry_id_surface_volume_case_airplane_v1_from_3rd_party_geometry.py

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+import os
+
+import flow360 as fl
+
+fl.Env.preprod.active()
+
+from simulation_examples.cylinder_case import createBaseParams_cylinder
+
+from flow360.component.geometry import Geometry
+from flow360.component.meshing.params import Farfield, Volume, VolumeMeshingParams
+from flow360.examples import Cylinder
+
+# geometry
+geometry_draft = Geometry.from_file(Cylinder.geometry, name="testing-cylinder-3rd-party-geometry")
+geometry = geometry_draft.submit()
+print(geometry)
+
+# surface mesh
+params = fl.SurfaceMeshingParams(max_edge_length=0.5)
+
+surface_mesh_draft = fl.SurfaceMesh.create(
+    geometry_id=geometry.id,
+    params=params,
+    name="cylinder-surface-mesh-from-3rd-party-geometry-v1",
+)
+surface_mesh = surface_mesh_draft.submit()
+
+print(surface_mesh)
+
+# volume mesh
+params = fl.VolumeMeshingParams(
+    volume=Volume(
+        first_layer_thickness=1e-4,
+        growth_rate=1.2,
+    ),
+    farfield=Farfield(type="auto"),
+)
+
+volume_mesh_draft = fl.VolumeMesh.create(
+    surface_mesh_id=surface_mesh.id,
+    name="cylinder-volume-mesh-from-3rd-party-geometry-id-v1",
+    params=params,
+)
+volume_mesh = volume_mesh_draft.submit()
+print(volume_mesh)
+
+# case
+params = createBaseParams_cylinder()
+params.boundaries = {
+    "fluid/farfield": fl.FreestreamBoundary(),
+    "fluid/unspecified": fl.NoSlipWall(),
+}
+case_draft = volume_mesh.create_case(
+    "cylinder-case-from-egads-3rd-party-geometry-id-v1", params, solver_version="mesher-24.2.1"
+)
+case = case_draft.submit()

examples/geometry_id_surface_volume_case_airplane_v1_from_csm.py

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+import os
+
+import flow360 as fl
+
+fl.Env.preprod.active()
+
+from simulation_examples.airplane_case import createBaseParams_airplane
+
+from flow360.component.geometry import Geometry
+from flow360.component.meshing.params import Farfield, Volume, VolumeMeshingParams
+from flow360.examples import Airplane
+
+# geometry
+geometry_draft = Geometry.from_file(Airplane.geometry, name="testing-airplane-csm-geometry")
+geometry = geometry_draft.submit()
+print(geometry)
+
+# surface mesh
+params = fl.SurfaceMeshingParams(max_edge_length=0.16)
+
+surface_mesh_draft = fl.SurfaceMesh.create(
+    geometry_id=geometry.id,
+    params=params,
+    name="airplane-surface-mesh-from-geometry-id-v1",
+    solver_version="mesher-24.2.1",
+)
+surface_mesh = surface_mesh_draft.submit()
+
+print(surface_mesh)
+
+# volume mesh
+params = fl.VolumeMeshingParams(
+    volume=Volume(
+        first_layer_thickness=1e-5,
+        growth_rate=1.2,
+    ),
+    farfield=Farfield(type="auto"),
+)
+
+volume_mesh_draft = fl.VolumeMesh.create(
+    surface_mesh_id=surface_mesh.id,
+    name="airplane-volume-mesh-from-geometry-id-v1",
+    params=params,
+    solver_version="mesher-24.2.1",
+)
+volume_mesh = volume_mesh_draft.submit()
+print(volume_mesh)
+
+# case
+params = createBaseParams_airplane()
+params.boundaries = {
+    "fluid/farfield": fl.FreestreamBoundary(),
+    "fluid/fuselage": fl.NoSlipWall(),
+    "fluid/leftWing": fl.NoSlipWall(),
+    "fluid/rightWing": fl.NoSlipWall(),
+}
+case_draft = volume_mesh.create_case("airplane-case-from-csm-geometry-id-v1", params)
+case = case_draft.submit()

examples/geometry_id_surface_volume_case_airplane_v1_from_egads.py

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+import os
+
+import flow360 as fl
+
+fl.Env.preprod.active()
+
+from simulation_examples.airplane_case import createBaseParams_airplane
+
+from flow360.component.geometry import Geometry
+from flow360.component.meshing.params import Farfield, Volume, VolumeMeshingParams
+from flow360.examples import Airplane
+
+# geometry
+geometry_draft = Geometry.from_file(
+    "data/airplane_geometry.egads", name="testing-airplane-egads-geometry"
+)
+geometry = geometry_draft.submit()
+print(geometry)
+
+# surface mesh
+params = fl.SurfaceMeshingParams(max_edge_length=0.16)
+
+surface_mesh_draft = fl.SurfaceMesh.create(
+    geometry_id=geometry.id,
+    params=params,
+    name="airplane-surface-mesh-from-geometry-id-v1",
+    solver_version="mesher-24.2.1",
+)
+surface_mesh = surface_mesh_draft.submit()
+
+print(surface_mesh)
+
+# volume mesh
+params = fl.VolumeMeshingParams(
+    volume=Volume(
+        first_layer_thickness=1e-5,
+        growth_rate=1.2,
+    ),
+    farfield=Farfield(type="auto"),
+)
+
+volume_mesh_draft = fl.VolumeMesh.create(
+    surface_mesh_id=surface_mesh.id,
+    name="airplane-volume-mesh-from-geometry-id-v1",
+    params=params,
+    solver_version="mesher-24.2.1",
+)
+volume_mesh = volume_mesh_draft.submit()
+print(volume_mesh)
+
+# case
+params = createBaseParams_airplane()
+params.boundaries = {
+    "fluid/farfield": fl.FreestreamBoundary(),
+    "fluid/fuselage": fl.NoSlipWall(),
+    "fluid/leftWing": fl.NoSlipWall(),
+    "fluid/rightWing": fl.NoSlipWall(),
+}
+case_draft = volume_mesh.create_case("airplane-case-from-egads-geometry-id-v1", params)
+case = case_draft.submit()

examples/geometry_id_surface_volume_case_airplane_v2_from_3rd_party_geometry.py

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+import os
+
+os.environ["FLOW360_BETA_FEATURES"] = "1"
+import flow360 as fl
+
+fl.Env.preprod.active()
+
+from simulation_examples.cylinder_case import createBaseParams_cylinder
+
+from flow360.component.geometry import Geometry
+from flow360.component.meshing.params import Farfield, Volume, VolumeMeshingParams
+from flow360.examples import Cylinder
+
+# geometry
+geometry_draft = Geometry.from_file(Cylinder.geometry, name="testing-cylinder-3rd-party-geometry")
+geometry = geometry_draft.submit()
+print(geometry)
+
+# surface mesh
+params = fl.SurfaceMeshingParams(version="v2", max_edge_length=0.5)
+
+surface_mesh_draft = fl.SurfaceMesh.create(
+    geometry_id=geometry.id,
+    params=params,
+    name="cylinder-surface-mesh-from-3rd-party-geometry-v2",
+    solver_version="mesher-24.2.1",
+)
+surface_mesh = surface_mesh_draft.submit()
+
+print(surface_mesh)
+
+# volume mesh
+params = fl.VolumeMeshingParams(
+    version="v2",
+    volume=Volume(
+        first_layer_thickness=1e-4,
+        growth_rate=1.2,
+    ),
+    farfield=Farfield(type="auto"),
+)
+
+volume_mesh_draft = fl.VolumeMesh.create(
+    surface_mesh_id=surface_mesh.id,
+    name="cylinder-volume-mesh-from-3rd-party-geometry-id-v2",
+    params=params,
+    solver_version="mesher-24.2.1",
+)
+volume_mesh = volume_mesh_draft.submit()
+print(volume_mesh)
+
+# case
+params = createBaseParams_cylinder()
+params.boundaries = {
+    "farfield": fl.FreestreamBoundary(),
+    "unspecified": fl.NoSlipWall(),
+}
+case_draft = volume_mesh.create_case(
+    "cylinder-case-from-egads-3rd-party-geometry-id-v2", params, solver_version="mesher-24.2.1"
+)
+case = case_draft.submit()

examples/geometry_id_surface_volume_case_airplane_v2_from_csm.py

@@ -0,0 +1,60 @@
+import os
+
+os.environ["FLOW360_BETA_FEATURES"] = "1"
+import flow360 as fl
+
+fl.Env.preprod.active()
+
+from simulation_examples.airplane_case import createBaseParams_airplane
+
+from flow360.component.geometry import Geometry
+from flow360.component.meshing.params import Farfield, Volume, VolumeMeshingParams
+from flow360.examples import Airplane
+
+# geometry
+geometry_draft = Geometry.from_file(Airplane.geometry, name="testing-airplane-csm-geometry")
+geometry = geometry_draft.submit()
+print(geometry)
+
+# surface mesh
+params = fl.SurfaceMeshingParams(version="v2", max_edge_length=0.16)
+
+surface_mesh_draft = fl.SurfaceMesh.create(
+    geometry_id=geometry.id,
+    params=params,
+    name="airplane-surface-mesh-from-geometry-id-v2",
+    solver_version="mesher-24.2.1",
+)
+surface_mesh = surface_mesh_draft.submit()
+
+print(surface_mesh)
+
+# volume mesh
+params = fl.VolumeMeshingParams(
+    version="v2",
+    volume=Volume(
+        first_layer_thickness=1e-5,
+        growth_rate=1.2,
+    ),
+    farfield=Farfield(type="auto"),
+)
+
+volume_mesh_draft = fl.VolumeMesh.create(
+    surface_mesh_id=surface_mesh.id,
+    name="airplane-volume-mesh-from-geometry-id-v2",
+    params=params,
+    solver_version="mesher-24.2.1",
+)
+volume_mesh = volume_mesh_draft.submit()
+print(volume_mesh)
+
+# case
+params = createBaseParams_airplane()
+params.boundaries = {
+    "farfield": fl.FreestreamBoundary(),
+    "fuselage": fl.NoSlipWall(),
+    "leftWing": fl.NoSlipWall(),
+    "rightWing": fl.NoSlipWall(),
+}
+case_draft = volume_mesh.create_case("airplane-case-from-csm-geometry-id-v2", params)
+case = case_draft.submit()

examples/geometry_id_surface_volume_case_airplane_v2_from_egads.py

@@ -0,0 +1,62 @@
+import os
+
+os.environ["FLOW360_BETA_FEATURES"] = "1"
+import flow360 as fl
+
+fl.Env.preprod.active()
+
+from simulation_examples.airplane_case import createBaseParams_airplane
+
+from flow360.component.geometry import Geometry
+from flow360.component.meshing.params import Farfield, Volume, VolumeMeshingParams
+from flow360.examples import Airplane
+
+# geometry
+geometry_draft = Geometry.from_file(
+    "data/airplane_geometry.egads", name="testing-airplane-egads-geometry"
+)
+geometry = geometry_draft.submit()
+print(geometry)
+
+# surface mesh
+params = fl.SurfaceMeshingParams(version="v2", max_edge_length=0.16)
+
+surface_mesh_draft = fl.SurfaceMesh.create(
+    geometry_id=geometry.id,
+    params=params,
+    name="airplane-surface-mesh-from-geometry-id-v2",
+    solver_version="mesher-24.2.1",
+)
+surface_mesh = surface_mesh_draft.submit()
+
+print(surface_mesh)
+
+# volume mesh
+params = fl.VolumeMeshingParams(
+    version="v2",
+    volume=Volume(
+        first_layer_thickness=1e-5,
+        growth_rate=1.2,
+    ),
+    farfield=Farfield(type="auto"),
+)
+
+volume_mesh_draft = fl.VolumeMesh.create(
+    surface_mesh_id=surface_mesh.id,
+    name="airplane-volume-mesh-from-geometry-id-v2",
+    params=params,
+    solver_version="mesher-24.2.1",
+)
+volume_mesh = volume_mesh_draft.submit()
+print(volume_mesh)
+
+# case
+params = createBaseParams_airplane()
+params.boundaries = {
+    "farfield": fl.FreestreamBoundary(),
+    "fuselage": fl.NoSlipWall(),
+    "leftWing": fl.NoSlipWall(),
+    "rightWing": fl.NoSlipWall(),
+}
+case_draft = volume_mesh.create_case("airplane-case-from-egads-geometry-id-v2", params)
+case = case_draft.submit()