Add files using upload-large-folder tool

case_1631/design_parameter_sample_1631.json

@@ -0,0 +1,117 @@
+{
+    "inputs": [
+        {
+            "description": "",
+            "name": "Dihedral angle",
+            "type": "real",
+            "units": "deg",
+            "value": 3.7676733937887623
+        },
+        {
+            "description": "",
+            "name": "Max Wing Blend",
+            "type": "real",
+            "units": "mm",
+            "value": 401.9845693139844
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 1",
+            "type": "real",
+            "units": "deg",
+            "value": 12.826301694259266
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 2",
+            "type": "real",
+            "units": "deg",
+            "value": 5.268498863476112
+        },
+        {
+            "description": "",
+            "name": "Wing Position",
+            "type": "real",
+            "value": 0.30296900322386094
+        },
+        {
+            "description": "",
+            "name": "Rear Point",
+            "type": "point",
+            "units": "mm",
+            "value": [
+                6227.852204817536,
+                0.0,
+                0.0
+            ]
+        },
+        {
+            "description": "",
+            "name": "Inlet Location",
+            "type": "real",
+            "value": 0.3704203206333193
+        },
+        {
+            "description": "",
+            "name": "NACA 4-digit code",
+            "type": "text",
+            "value": "4412"
+        },
+        {
+            "description": "",
+            "name": "Fore Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 5.061739776945558
+        },
+        {
+            "description": "",
+            "name": "Aft Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 17.490181697882644
+        },
+        {
+            "description": "",
+            "name": "Top Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 134.52289297030165
+        },
+        {
+            "description": "",
+            "name": "Bottom Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 145.976072432337
+        },
+        {
+            "description": "",
+            "name": "Wing span",
+            "type": "real",
+            "units": "mm",
+            "value": 14124.965657949851
+        },
+        {
+            "description": "",
+            "name": "Rear tail offset",
+            "type": "real",
+            "units": "mm",
+            "value": 1095.2809202833573
+        },
+        {
+            "description": "",
+            "name": "Root Chord",
+            "type": "real",
+            "units": "mm",
+            "value": 1998.7478626101529
+        },
+        {
+            "description": "",
+            "name": "Tail Root chord",
+            "type": "real",
+            "units": "mm",
+            "value": 1165.9591778582108
+        }
+    ]
+}

case_1631/param_10.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1631_10",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 108.34268563344042,
+  "alpha": 6.407703936254855,
+  "beta": 0,
+  "altitude_m": 9754.46208231108,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      6.407703936254855
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_1631/param_2.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1631_2",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 100.98403911788017,
+  "alpha": -4.672857970706648,
+  "beta": 0,
+  "altitude_m": 3421.078476843793,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      -4.672857970706648
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_1631/param_3.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1631_3",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 159.26218739892659,
+  "alpha": 9.120342706797068,
+  "beta": 0,
+  "altitude_m": 7160.869356767719,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      9.120342706797068
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_1631/param_5.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1631_5",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 151.76156739065067,
+  "alpha": -7.63441649847702,
+  "beta": 0,
+  "altitude_m": 6688.645276081024,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      -7.63441649847702
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_1631/param_6.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1631_6",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 58.8499330355179,
+  "alpha": 5.745957718530905,
+  "beta": 0,
+  "altitude_m": 3626.851117060984,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      5.745957718530905
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_1631/param_7.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1631_7",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 74.78627208885152,
+  "alpha": -6.558888862129827,
+  "beta": 0,
+  "altitude_m": 5584.35431882966,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      -6.558888862129827
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_1631/param_8.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1631_8",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 52.397343106041724,
+  "alpha": -2.767970508913425,
+  "beta": 0,
+  "altitude_m": 6104.027482964522,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      -2.767970508913425
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_1631/params.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1631_1",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 112.16432460560037,
+  "alpha": -6.714151960198319,
+  "beta": 0,
+  "altitude_m": 9618.396972959394,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      -6.714151960198319
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_1631/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": 3.7676733937887623
+        },
+        {
+            "description": "",
+            "name": "Max Wing Blend",
+            "type": "real",
+            "units": "mm",
+            "value": 401.9845693139844
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 1",
+            "type": "real",
+            "units": "deg",
+            "value": 12.826301694259266
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 2",
+            "type": "real",
+            "units": "deg",
+            "value": 5.268498863476112
+        },
+        {
+            "description": "",
+            "name": "Wing Position",
+            "type": "real",
+            "value": 0.30296900322386094
+        },
+        {
+            "description": "",
+            "name": "Rear Point",
+            "type": "point",
+            "units": "mm",
+            "value": [
+                6227.852204817536,
+                0.0,
+                0.0
+            ]
+        },
+        {
+            "description": "",
+            "name": "Inlet Location",
+            "type": "real",
+            "value": 0.3704203206333193
+        },
+        {
+            "description": "",
+            "name": "NACA 4-digit code",
+            "type": "text",
+            "value": "4412"
+        },
+        {
+            "description": "",
+            "name": "Fore Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 5.061739776945558
+        },
+        {
+            "description": "",
+            "name": "Aft Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 17.490181697882644
+        },
+        {
+            "description": "",
+            "name": "Top Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 134.52289297030165
+        },
+        {
+            "description": "",
+            "name": "Bottom Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 145.976072432337
+        },
+        {
+            "description": "",
+            "name": "Wing span",
+            "type": "real",
+            "units": "mm",
+            "value": 14124.965657949851
+        },
+        {
+            "description": "",
+            "name": "Rear tail offset",
+            "type": "real",
+            "units": "mm",
+            "value": 1095.2809202833573
+        },
+        {
+            "description": "",
+            "name": "Root Chord",
+            "type": "real",
+            "units": "mm",
+            "value": 1998.7478626101529
+        },
+        {
+            "description": "",
+            "name": "Tail Root chord",
+            "type": "real",
+            "units": "mm",
+            "value": 1165.9591778582108
+        },
+        {
+            "description": "",
+            "name": "File Path_0",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/CCA_Drone/cases/case_1631/reference_area/../design_1631.stl"
+        },
+        {
+            "description": "",
+            "name": "File Surface Reference",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/CCA_Drone/cases/case_1631/reference_area/reference_area.txt"
+        }
+    ],
+    "title": "CCA_1_automated"
+}

case_1631/reference_area/mac.txt

@@ -0,0 +1 @@
+1.554581670919

case_1631/reference_area/reference_area.txt

@@ -0,0 +1 @@
+7296549.4630262386

case_1631/reference_area/reference_area_m2.txt

@@ -0,0 +1 @@
+14.593098926052

case_1631/results/alpha_-6.714151960198319/force_coefficents_corected.csv

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+,value
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+CMxSkinFriction,-3.29815376626581e-07
+CMySkinFriction,0.003064037001133429
+CMzSkinFriction,1.50235529004508e-05

case_1631/results/alpha_-6.714151960198319/force_coefficients.csv

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+,value
+CL,-5.666928912496182
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+CMySkinFriction,0.06951124625402015
+CMzSkinFriction,0.0003408267866501714

case_1631/results/alpha_-6.714151960198319/forces_actual.csv

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+,value_SI
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+MzSkinFriction,0.929093226866465

case_1631/results/alpha_-6.714151960198319/forces_summary.json

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+{
+  "case_id": "case-6e794378-bacc-4771-a274-bf7cde2795e4",
+  "case_name": "alpha_case",
+  "case_status": "Flow360Status.COMPLETED",
+  "reference": {
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+    "reference_length_m": 1.0,
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+    "MzSkinFriction": 0.929093226866465
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+}

case_1631/results_3/alpha_9.120342706797068/force_coefficents_corected.csv

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+,value
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+CMySkinFriction,-0.0004873074920666232
+CMzSkinFriction,-6.44226893172684e-06

case_1631/results_3/alpha_9.120342706797068/force_coefficients.csv

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+,value
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+CMySkinFriction,-0.011055137738200225
+CMzSkinFriction,-0.0001461503702410371

case_1631/results_3/alpha_9.120342706797068/forces_actual.csv

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+,value_SI
+L,133324.94673970112
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case_1631/results_3/alpha_9.120342706797068/forces_summary.json

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case_1631/results_6/alpha_5.745957718530905/force_coefficients.csv

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case_1631/results_6/alpha_5.745957718530905/forces_actual.csv

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case_1631/results_7/alpha_-6.558888862129827/force_coefficents_corected.csv

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