Add files using upload-large-folder tool

case_14/design_parameter_sample_14.json

@@ -0,0 +1,117 @@
+{
+    "inputs": [
+        {
+            "description": "",
+            "name": "Dihedral angle",
+            "type": "real",
+            "units": "deg",
+            "value": 14.352503209691422
+        },
+        {
+            "description": "",
+            "name": "Max Wing Blend",
+            "type": "real",
+            "units": "mm",
+            "value": 477.2111371020032
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 1",
+            "type": "real",
+            "units": "deg",
+            "value": 43.7820033652251
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 2",
+            "type": "real",
+            "units": "deg",
+            "value": 9.913986251579392
+        },
+        {
+            "description": "",
+            "name": "Wing Position",
+            "type": "real",
+            "value": 0.44071751064413717
+        },
+        {
+            "description": "",
+            "name": "Rear Point",
+            "type": "point",
+            "units": "mm",
+            "value": [
+                5322.261015996084,
+                0.0,
+                0.0
+            ]
+        },
+        {
+            "description": "",
+            "name": "Inlet Location",
+            "type": "real",
+            "value": 0.29251585896645904
+        },
+        {
+            "description": "",
+            "name": "NACA 4-digit code",
+            "type": "text",
+            "value": "2408"
+        },
+        {
+            "description": "",
+            "name": "Fore Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 5.286254153987833
+        },
+        {
+            "description": "",
+            "name": "Aft Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 15.820328322568123
+        },
+        {
+            "description": "",
+            "name": "Top Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 187.95961520411208
+        },
+        {
+            "description": "",
+            "name": "Bottom Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 203.61961290746575
+        },
+        {
+            "description": "",
+            "name": "Wing span",
+            "type": "real",
+            "units": "mm",
+            "value": 15551.801371795918
+        },
+        {
+            "description": "",
+            "name": "Rear tail offset",
+            "type": "real",
+            "units": "mm",
+            "value": 1352.8200972141567
+        },
+        {
+            "description": "",
+            "name": "Root Chord",
+            "type": "real",
+            "units": "mm",
+            "value": 1600.641771362269
+        },
+        {
+            "description": "",
+            "name": "Tail Root chord",
+            "type": "real",
+            "units": "mm",
+            "value": 966.6284738364157
+        }
+    ]
+}

case_14/param_3.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_14_3",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 28.589692665414837,
+  "alpha": 6.872350597309135,
+  "beta": 0,
+  "altitude_m": 7012.009135877115,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      6.872350597309135
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_14/param_4.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_14_4",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 127.87645116897252,
+  "alpha": -6.329312371081949,
+  "beta": 0,
+  "altitude_m": 4602.547024628185,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      -6.329312371081949
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_14/param_5.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_14_5",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 78.75772020392758,
+  "alpha": -2.072973667413141,
+  "beta": 0,
+  "altitude_m": 9839.970712221557,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      -2.072973667413141
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_14/param_6.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_14_6",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 155.58958581776005,
+  "alpha": -2.276498317936232,
+  "beta": 0,
+  "altitude_m": 7737.188816667496,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      -2.276498317936232
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_14/params.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_14_1",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 109.72397136050196,
+  "alpha": -1.8878741998482926,
+  "beta": 0,
+  "altitude_m": 257.225800662016,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      -1.8878741998482926
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_14/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": 14.352503209691422
+        },
+        {
+            "description": "",
+            "name": "Max Wing Blend",
+            "type": "real",
+            "units": "mm",
+            "value": 477.2111371020032
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 1",
+            "type": "real",
+            "units": "deg",
+            "value": 43.7820033652251
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 2",
+            "type": "real",
+            "units": "deg",
+            "value": 9.913986251579392
+        },
+        {
+            "description": "",
+            "name": "Wing Position",
+            "type": "real",
+            "value": 0.44071751064413717
+        },
+        {
+            "description": "",
+            "name": "Rear Point",
+            "type": "point",
+            "units": "mm",
+            "value": [
+                5322.261015996084,
+                0.0,
+                0.0
+            ]
+        },
+        {
+            "description": "",
+            "name": "Inlet Location",
+            "type": "real",
+            "value": 0.29251585896645904
+        },
+        {
+            "description": "",
+            "name": "NACA 4-digit code",
+            "type": "text",
+            "value": "2408"
+        },
+        {
+            "description": "",
+            "name": "Fore Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 5.286254153987833
+        },
+        {
+            "description": "",
+            "name": "Aft Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 15.820328322568123
+        },
+        {
+            "description": "",
+            "name": "Top Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 187.95961520411208
+        },
+        {
+            "description": "",
+            "name": "Bottom Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 203.61961290746575
+        },
+        {
+            "description": "",
+            "name": "Wing span",
+            "type": "real",
+            "units": "mm",
+            "value": 15551.801371795918
+        },
+        {
+            "description": "",
+            "name": "Rear tail offset",
+            "type": "real",
+            "units": "mm",
+            "value": 1352.8200972141567
+        },
+        {
+            "description": "",
+            "name": "Root Chord",
+            "type": "real",
+            "units": "mm",
+            "value": 1600.641771362269
+        },
+        {
+            "description": "",
+            "name": "Tail Root chord",
+            "type": "real",
+            "units": "mm",
+            "value": 966.6284738364157
+        },
+        {
+            "description": "",
+            "name": "File Path_0",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/CCA_Drone/cases/case_14/reference_area/../design_14.stl"
+        },
+        {
+            "description": "",
+            "name": "File Surface Reference",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/CCA_Drone/cases/case_14/reference_area/reference_area.txt"
+        }
+    ],
+    "title": "CCA_1_automated"
+}

case_14/reference_area/mac.txt

@@ -0,0 +1 @@
+1.244943599948

case_14/reference_area/reference_area.txt

@@ -0,0 +1 @@
+6146367.2810652284

case_14/reference_area/reference_area_m2.txt

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+12.292734562130

case_14/results/alpha_-1.8878741998482926/force_coefficents_corected.csv

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+,value
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+CMySkinFriction,0.005037455117912086
+CMzSkinFriction,-1.687945015909534e-06

case_14/results/alpha_-1.8878741998482926/force_coefficients.csv

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+,value
+CL,-0.5090675362620258
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case_14/results/alpha_-1.8878741998482926/forces_actual.csv

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+,value_SI
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+MzSkinFriction,-0.18582745194305061

case_14/results/alpha_-1.8878741998482926/forces_summary.json

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+{
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+  "case_name": "alpha_case",
+  "case_status": "Flow360Status.COMPLETED",
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+}

case_14/results_3/alpha_6.872350597309135/force_coefficents_corected.csv

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case_14/results_3/alpha_6.872350597309135/force_coefficients.csv

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case_14/results_3/alpha_6.872350597309135/forces_actual.csv

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case_14/results_3/alpha_6.872350597309135/forces_summary.json

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+{
+  "case_id": "case-06986e34-f68c-42c8-b571-69943b88eb58",
+  "case_name": "alpha_case",
+  "case_status": "Flow360Status.COMPLETED",
+  "reference": {
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+}

case_14/results_4/alpha_-6.329312371081949/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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case_14/results_4/alpha_-6.329312371081949/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_14/results_4/alpha_-6.329312371081949/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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case_14/results_4/alpha_-6.329312371081949/forces_summary.json

@@ -0,0 +1,64 @@
+{
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+}

case_14/results_5/alpha_-2.072973667413141/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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case_14/results_5/alpha_-2.072973667413141/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_14/results_5/alpha_-2.072973667413141/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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case_14/results_5/alpha_-2.072973667413141/forces_summary.json

@@ -0,0 +1,64 @@
+{
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+}

case_14/results_6/alpha_-2.276498317936232/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
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case_14/results_6/alpha_-2.276498317936232/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_14/results_6/alpha_-2.276498317936232/forces_actual.csv

@@ -0,0 +1,25 @@
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case_14/results_6/alpha_-2.276498317936232/forces_summary.json

@@ -0,0 +1,64 @@
+{
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+    "MzSkinFriction": 0.0386813183307328
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+}

case_150/design_parameter_sample_150.json

@@ -0,0 +1,117 @@
+{
+    "inputs": [
+        {
+            "description": "",
+            "name": "Dihedral angle",
+            "type": "real",
+            "units": "deg",
+            "value": 10.852624963972447
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+            "name": "Max Wing Blend",
+            "type": "real",
+            "units": "mm",
+            "value": 81.94914532422573
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+        {
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+            "name": "Inlet Angle 1",
+            "type": "real",
+            "units": "deg",
+            "value": 5.18431698065478
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+        {
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+            "name": "Inlet Angle 2",
+            "type": "real",
+            "units": "deg",
+            "value": 1.9947082683581472
+        },
+        {
+            "description": "",
+            "name": "Wing Position",
+            "type": "real",
+            "value": 0.32353326707954777
+        },
+        {
+            "description": "",
+            "name": "Rear Point",
+            "type": "point",
+            "units": "mm",
+            "value": [
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+                0.0
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+        },
+        {
+            "description": "",
+            "name": "Inlet Location",
+            "type": "real",
+            "value": 0.5428120269897976
+        },
+        {
+            "description": "",
+            "name": "NACA 4-digit code",
+            "type": "text",
+            "value": "4412"
+        },
+        {
+            "description": "",
+            "name": "Fore Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 0.37735442458581187
+        },
+        {
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+            "name": "Aft Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 29.595432089008725
+        },
+        {
+            "description": "",
+            "name": "Top Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 120.85901526921656
+        },
+        {
+            "description": "",
+            "name": "Bottom Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 117.40709529022078
+        },
+        {
+            "description": "",
+            "name": "Wing span",
+            "type": "real",
+            "units": "mm",
+            "value": 12948.559796393984
+        },
+        {
+            "description": "",
+            "name": "Rear tail offset",
+            "type": "real",
+            "units": "mm",
+            "value": 1552.5597944151586
+        },
+        {
+            "description": "",
+            "name": "Root Chord",
+            "type": "real",
+            "units": "mm",
+            "value": 2263.4247517529047
+        },
+        {
+            "description": "",
+            "name": "Tail Root chord",
+            "type": "real",
+            "units": "mm",
+            "value": 845.7917321100383
+        }
+    ]
+}

case_150/param_10.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_150_10",
+  "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": 8752.986570460194,
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+    "values": [
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+    "unit": "fl.u.deg"
+  }
+}

case_150/param_2.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_150_2",
+  "max_steps": 3500,
+  "volume_mesh_params": {
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+    "values": [
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+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_150/param_3.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_150_3",
+  "max_steps": 3500,
+  "volume_mesh_params": {
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+    "values": [
+      -5.594514502829705
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+    "unit": "fl.u.deg"
+  }
+}

case_150/param_4.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_150_4",
+  "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": 6.323648517808124,
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+    "values": [
+      6.323648517808124
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_150/param_5.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_150_5",
+  "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": 51.90362224485697,
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+  "altitude_m": 1877.3830483052006,
+  "sweep_schema": {
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+    "values": [
+      -4.162584927245357
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_150/param_6.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_150_6",
+  "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": 97.5924726733642,
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+  "sweep_schema": {
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+    "values": [
+      2.9688677940290287
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_150/param_7.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_150_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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+  "velocity_magnitude": 43.014369423222206,
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+  "altitude_m": 8902.641943478451,
+  "sweep_schema": {
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+    "values": [
+      1.6025759468855263
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_150/param_8.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_150_8",
+  "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": 49.28619788451008,
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+  "altitude_m": 5986.463720943051,
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+    "values": [
+      3.6352839744684147
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_150/param_9.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_150_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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+  "velocity_magnitude": 88.99746524241115,
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+  "sweep_schema": {
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+    "values": [
+      2.238727361656739
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_150/params.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_150_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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+  "velocity_magnitude": 78.1160710641212,
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+  "altitude_m": 5214.301405716332,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      -7.0633048742682005
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_150/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": 10.852624963972447
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+        {
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+            "name": "Max Wing Blend",
+            "type": "real",
+            "units": "mm",
+            "value": 81.94914532422573
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+            "name": "Inlet Angle 1",
+            "type": "real",
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+            "value": 5.18431698065478
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+        {
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+            "name": "Inlet Angle 2",
+            "type": "real",
+            "units": "deg",
+            "value": 1.9947082683581472
+        },
+        {
+            "description": "",
+            "name": "Wing Position",
+            "type": "real",
+            "value": 0.32353326707954777
+        },
+        {
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+            "name": "Rear Point",
+            "type": "point",
+            "units": "mm",
+            "value": [
+                7191.4780198858825,
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+        },
+        {
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+            "name": "Inlet Location",
+            "type": "real",
+            "value": 0.5428120269897976
+        },
+        {
+            "description": "",
+            "name": "NACA 4-digit code",
+            "type": "text",
+            "value": "4412"
+        },
+        {
+            "description": "",
+            "name": "Fore Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 0.37735442458581187
+        },
+        {
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+            "name": "Aft Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 29.595432089008725
+        },
+        {
+            "description": "",
+            "name": "Top Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 120.85901526921656
+        },
+        {
+            "description": "",
+            "name": "Bottom Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 117.40709529022078
+        },
+        {
+            "description": "",
+            "name": "Wing span",
+            "type": "real",
+            "units": "mm",
+            "value": 12948.559796393984
+        },
+        {
+            "description": "",
+            "name": "Rear tail offset",
+            "type": "real",
+            "units": "mm",
+            "value": 1552.5597944151586
+        },
+        {
+            "description": "",
+            "name": "Root Chord",
+            "type": "real",
+            "units": "mm",
+            "value": 2263.4247517529047
+        },
+        {
+            "description": "",
+            "name": "Tail Root chord",
+            "type": "real",
+            "units": "mm",
+            "value": 845.7917321100383
+        },
+        {
+            "description": "",
+            "name": "File Path_0",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/CCA_Drone/cases/case_150/reference_area/../design_150.stl"
+        },
+        {
+            "description": "",
+            "name": "File Surface Reference",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/CCA_Drone/cases/case_150/reference_area/reference_area.txt"
+        }
+    ],
+    "title": "CCA_1_automated"
+}

case_150/reference_area/mac.txt

@@ -0,0 +1 @@
+1.760441473586

case_150/reference_area/reference_area.txt

@@ -0,0 +1 @@
+7342563.622057151

case_150/reference_area/reference_area_m2.txt

@@ -0,0 +1 @@
+14.685127244114

case_150/results/alpha_-7.0633048742682005/force_coefficents_corected.csv

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+,value
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+CMzSkinFriction,-8.194144946885903e-06

case_150/results/alpha_-7.0633048742682005/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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+CMzSkinFriction,-0.00021183755114161998

case_150/results/alpha_-7.0633048742682005/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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+D,1282.510467692769
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+Mz,-3.2218370124892832
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+MzSkinFriction,-0.4650537565004166

case_150/results/alpha_-7.0633048742682005/forces_summary.json

@@ -0,0 +1,64 @@
+{
+  "case_id": "case-1ef85a76-d8f9-42e1-82f7-23305ab04b0e",
+  "case_name": "alpha_case",
+  "case_status": "Flow360Status.COMPLETED",
+  "reference": {
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+  "forces_N_and_moments_Nm": {
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+    "MzPressure": -2.7567832559743026,
+    "MzSkinFriction": -0.4650537565004166
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+}

case_150/results_10/alpha_3.5429317345672118/force_coefficents_corected.csv

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+,value
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+CMyPressure,-1.424622536808449
+CMzPressure,-0.0001506256010973214
+CLSkinFriction,-0.0004469705858916207
+CDSkinFriction,0.01212918545644521
+CFxSkinFriction,0.01213362503269108
+CFySkinFriction,-3.835886841171763e-06
+CFzSkinFriction,0.0003034239732567485
+CMxSkinFriction,1.331420134680231e-06
+CMySkinFriction,0.002220864230209453
+CMzSkinFriction,-6.048214207995211e-06