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case_13/design_parameter_sample_13.json

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+{
+    "inputs": [
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+            "description": "",
+            "name": "Dihedral angle",
+            "type": "real",
+            "units": "deg",
+            "value": 3.7301185974848914
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+        {
+            "description": "",
+            "name": "Max Wing Blend",
+            "type": "real",
+            "units": "mm",
+            "value": 138.55520059275574
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+        {
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+            "name": "Inlet Angle 1",
+            "type": "real",
+            "units": "deg",
+            "value": 1.6668815693874381
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 2",
+            "type": "real",
+            "units": "deg",
+            "value": 1.8026785511142847
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+        {
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+            "name": "Wing Position",
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+            "value": 0.4929566687116197
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+            "name": "Rear Point",
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+            "value": 0.29213708980985853
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+        {
+            "description": "",
+            "name": "NACA 4-digit code",
+            "type": "text",
+            "value": "4412"
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+            "type": "real",
+            "units": "deg",
+            "value": 9.004997529379326
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+            "name": "Aft Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 15.962350033732566
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+        {
+            "description": "",
+            "name": "Top Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 75.6204785743539
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+        {
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+            "name": "Bottom Height Aft",
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+            "value": 51.92698615830007
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+            "name": "Wing span",
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+            "value": 11120.90680001996
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+        {
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+            "name": "Rear tail offset",
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+            "units": "mm",
+            "value": 1468.2195938506432
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+            "name": "Root Chord",
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+            "value": 2297.675464850542
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+        {
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+            "name": "Tail Root chord",
+            "type": "real",
+            "units": "mm",
+            "value": 1123.5324893424506
+        }
+    ]
+}

case_13/param_2.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_13_2",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
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+  "velocity_magnitude": 145.28483368477666,
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+    "values": [
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+    "unit": "fl.u.deg"
+  }
+}

case_13/param_3.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_13_3",
+  "max_steps": 3500,
+  "volume_mesh_params": {
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+    "unit": "fl.u.deg"
+  }
+}

case_13/param_6.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_13_6",
+  "max_steps": 3500,
+  "volume_mesh_params": {
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+    "values": [
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+    "unit": "fl.u.deg"
+  }
+}

case_13/param_7.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_13_7",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
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+  "alpha": 5.764872943345708,
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+    "values": [
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+    "unit": "fl.u.deg"
+  }
+}

case_13/param_9.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_13_9",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
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+  "sweep_schema": {
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+    "values": [
+      4.153032655892364
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_13/params.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_13_1",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
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+  "altitude_m": 823.8910726798073,
+  "sweep_schema": {
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+    "values": [
+      5.065377088486768
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+    "unit": "fl.u.deg"
+  }
+}

case_13/reference_area/input.json

@@ -0,0 +1,131 @@
+{
+    "description": "CCA Demo\n\nPresented in 7/17 webinar\n\nAntonsen 2025",
+    "inputs": [
+        {
+            "description": "",
+            "name": "Dihedral angle",
+            "type": "real",
+            "units": "deg",
+            "value": 3.7301185974848914
+        },
+        {
+            "description": "",
+            "name": "Max Wing Blend",
+            "type": "real",
+            "units": "mm",
+            "value": 138.55520059275574
+        },
+        {
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+            "name": "Inlet Angle 1",
+            "type": "real",
+            "units": "deg",
+            "value": 1.6668815693874381
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 2",
+            "type": "real",
+            "units": "deg",
+            "value": 1.8026785511142847
+        },
+        {
+            "description": "",
+            "name": "Wing Position",
+            "type": "real",
+            "value": 0.4929566687116197
+        },
+        {
+            "description": "",
+            "name": "Rear Point",
+            "type": "point",
+            "units": "mm",
+            "value": [
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+                0.0,
+                0.0
+            ]
+        },
+        {
+            "description": "",
+            "name": "Inlet Location",
+            "type": "real",
+            "value": 0.29213708980985853
+        },
+        {
+            "description": "",
+            "name": "NACA 4-digit code",
+            "type": "text",
+            "value": "4412"
+        },
+        {
+            "description": "",
+            "name": "Fore Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 9.004997529379326
+        },
+        {
+            "description": "",
+            "name": "Aft Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 15.962350033732566
+        },
+        {
+            "description": "",
+            "name": "Top Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 75.6204785743539
+        },
+        {
+            "description": "",
+            "name": "Bottom Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 51.92698615830007
+        },
+        {
+            "description": "",
+            "name": "Wing span",
+            "type": "real",
+            "units": "mm",
+            "value": 11120.90680001996
+        },
+        {
+            "description": "",
+            "name": "Rear tail offset",
+            "type": "real",
+            "units": "mm",
+            "value": 1468.2195938506432
+        },
+        {
+            "description": "",
+            "name": "Root Chord",
+            "type": "real",
+            "units": "mm",
+            "value": 2297.675464850542
+        },
+        {
+            "description": "",
+            "name": "Tail Root chord",
+            "type": "real",
+            "units": "mm",
+            "value": 1123.5324893424506
+        },
+        {
+            "description": "",
+            "name": "File Path_0",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/CCA_Drone/cases/case_13/reference_area/../design_13.stl"
+        },
+        {
+            "description": "",
+            "name": "File Surface Reference",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/CCA_Drone/cases/case_13/reference_area/reference_area.txt"
+        }
+    ],
+    "title": "CCA_1_automated"
+}

case_13/reference_area/mac.txt

@@ -0,0 +1 @@
+1.787080917106

case_13/reference_area/reference_area.txt

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+6754433.7541780556

case_13/reference_area/reference_area_m2.txt

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+13.508867508356

case_13/results/alpha_5.065377088486768/force_coefficents_corected.csv

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+CMySkinFriction,-9.183076930691854e-05
+CMzSkinFriction,8.485850764891139e-06

case_13/results/alpha_5.065377088486768/force_coefficients.csv

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+,value
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case_13/results/alpha_5.065377088486768/forces_actual.csv

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+,value_SI
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+MzSkinFriction,0.06592822721128441

case_13/results/alpha_5.065377088486768/forces_summary.json

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+{
+  "case_id": "case-4b84b155-8cc6-4d69-8ef9-4401730d3ce6",
+  "case_name": "alpha_case",
+  "case_status": "Flow360Status.COMPLETED",
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+    "MzSkinFriction": 0.06592822721128441
+  }
+}

case_13/results_2/alpha_-3.338428920839741/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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case_13/results_2/alpha_-3.338428920839741/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_13/results_2/alpha_-3.338428920839741/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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+MzPressure,15.473663972473613
+MzSkinFriction,-0.4574158434203343

case_13/results_2/alpha_-3.338428920839741/forces_summary.json

@@ -0,0 +1,64 @@
+{
+  "case_id": "case-60ee3892-dae2-49a4-ae78-9b7bd4306688",
+  "case_name": "alpha_case",
+  "case_status": "Flow360Status.COMPLETED",
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+}

case_13/results_3/alpha_9.50643115815668/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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+CMzSkinFriction,2.868193865747444e-06

case_13/results_3/alpha_9.50643115815668/forces_summary.json

@@ -0,0 +1,64 @@
+{
+  "case_id": "case-7c59a946-cbca-4851-8cf0-c93c3914219d",
+  "case_name": "alpha_case",
+  "case_status": "Flow360Status.COMPLETED",
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+}

case_13/results_6/alpha_1.4500172694270113/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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case_13/results_6/alpha_1.4500172694270113/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_13/results_6/alpha_1.4500172694270113/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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+MzSkinFriction,0.04835326638429209

case_13/results_6/alpha_1.4500172694270113/forces_summary.json

@@ -0,0 +1,64 @@
+{
+  "case_id": "case-3407251d-f205-4348-b8b5-48849c6a445b",
+  "case_name": "alpha_case",
+  "case_status": "Flow360Status.COMPLETED",
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+}

case_13/results_7/alpha_5.764872943345708/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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case_13/results_7/alpha_5.764872943345708/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_13/results_7/alpha_5.764872943345708/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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