Add files using upload-large-folder tool

case_1527/design_parameter_sample_1527.json

@@ -0,0 +1,117 @@
+{
+    "inputs": [
+        {
+            "description": "",
+            "name": "Dihedral angle",
+            "type": "real",
+            "units": "deg",
+            "value": 11.245866434803952
+        },
+        {
+            "description": "",
+            "name": "Max Wing Blend",
+            "type": "real",
+            "units": "mm",
+            "value": 549.0355386018781
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 1",
+            "type": "real",
+            "units": "deg",
+            "value": 16.08905422690775
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 2",
+            "type": "real",
+            "units": "deg",
+            "value": 0.6523385631645222
+        },
+        {
+            "description": "",
+            "name": "Wing Position",
+            "type": "real",
+            "value": 0.42914969693403937
+        },
+        {
+            "description": "",
+            "name": "Rear Point",
+            "type": "point",
+            "units": "mm",
+            "value": [
+                6620.46517680258,
+                0.0,
+                0.0
+            ]
+        },
+        {
+            "description": "",
+            "name": "Inlet Location",
+            "type": "real",
+            "value": 0.2962188563652569
+        },
+        {
+            "description": "",
+            "name": "NACA 4-digit code",
+            "type": "text",
+            "value": "1412"
+        },
+        {
+            "description": "",
+            "name": "Fore Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 4.199544613585401
+        },
+        {
+            "description": "",
+            "name": "Aft Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 26.904089805895353
+        },
+        {
+            "description": "",
+            "name": "Top Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 95.50974575049717
+        },
+        {
+            "description": "",
+            "name": "Bottom Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 141.86624470790696
+        },
+        {
+            "description": "",
+            "name": "Wing span",
+            "type": "real",
+            "units": "mm",
+            "value": 8327.424350224373
+        },
+        {
+            "description": "",
+            "name": "Rear tail offset",
+            "type": "real",
+            "units": "mm",
+            "value": 1119.5477926940553
+        },
+        {
+            "description": "",
+            "name": "Root Chord",
+            "type": "real",
+            "units": "mm",
+            "value": 2227.044660132383
+        },
+        {
+            "description": "",
+            "name": "Tail Root chord",
+            "type": "real",
+            "units": "mm",
+            "value": 961.9769044136352
+        }
+    ]
+}

case_1527/param_10.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1527_10",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 53.853791953509834,
+  "alpha": 7.3947363061559646,
+  "beta": 0,
+  "altitude_m": 9259.702974485444,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      7.3947363061559646
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_1527/param_2.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1527_2",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 155.1817529852553,
+  "alpha": -4.3620408230016,
+  "beta": 0,
+  "altitude_m": 6440.529272467892,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      -4.3620408230016
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_1527/param_3.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1527_3",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 128.21718501005262,
+  "alpha": 0.3296729145917805,
+  "beta": 0,
+  "altitude_m": 3054.1629179239667,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      0.3296729145917805
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_1527/param_4.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1527_4",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 64.46772917134867,
+  "alpha": -2.8302085894029974,
+  "beta": 0,
+  "altitude_m": 272.3887633332084,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      -2.8302085894029974
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_1527/param_5.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1527_5",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 70.87831131628633,
+  "alpha": -1.5782139694629675,
+  "beta": 0,
+  "altitude_m": 1293.4789077352373,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      -1.5782139694629675
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_1527/param_6.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1527_6",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 103.27143896977287,
+  "alpha": -3.5893417819142437,
+  "beta": 0,
+  "altitude_m": 4720.485884504813,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      -3.5893417819142437
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_1527/param_7.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1527_7",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 44.91204961836202,
+  "alpha": 4.3934172895299355,
+  "beta": 0,
+  "altitude_m": 7191.647430428912,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      4.3934172895299355
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_1527/param_8.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1527_8",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 44.67753447761048,
+  "alpha": 4.606313622412102,
+  "beta": 0,
+  "altitude_m": 4474.443140953797,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      4.606313622412102
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_1527/param_9.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1527_9",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 22.274552531788583,
+  "alpha": 3.0514358193147206,
+  "beta": 0,
+  "altitude_m": 6216.017840690355,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      3.0514358193147206
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_1527/params.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1527_1",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 71.54342355338808,
+  "alpha": -1.8970991512894813,
+  "beta": 0,
+  "altitude_m": 4023.39579249752,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      -1.8970991512894813
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_1527/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": 11.245866434803952
+        },
+        {
+            "description": "",
+            "name": "Max Wing Blend",
+            "type": "real",
+            "units": "mm",
+            "value": 549.0355386018781
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 1",
+            "type": "real",
+            "units": "deg",
+            "value": 16.08905422690775
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 2",
+            "type": "real",
+            "units": "deg",
+            "value": 0.6523385631645222
+        },
+        {
+            "description": "",
+            "name": "Wing Position",
+            "type": "real",
+            "value": 0.42914969693403937
+        },
+        {
+            "description": "",
+            "name": "Rear Point",
+            "type": "point",
+            "units": "mm",
+            "value": [
+                6620.46517680258,
+                0.0,
+                0.0
+            ]
+        },
+        {
+            "description": "",
+            "name": "Inlet Location",
+            "type": "real",
+            "value": 0.2962188563652569
+        },
+        {
+            "description": "",
+            "name": "NACA 4-digit code",
+            "type": "text",
+            "value": "1412"
+        },
+        {
+            "description": "",
+            "name": "Fore Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 4.199544613585401
+        },
+        {
+            "description": "",
+            "name": "Aft Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 26.904089805895353
+        },
+        {
+            "description": "",
+            "name": "Top Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 95.50974575049717
+        },
+        {
+            "description": "",
+            "name": "Bottom Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 141.86624470790696
+        },
+        {
+            "description": "",
+            "name": "Wing span",
+            "type": "real",
+            "units": "mm",
+            "value": 8327.424350224373
+        },
+        {
+            "description": "",
+            "name": "Rear tail offset",
+            "type": "real",
+            "units": "mm",
+            "value": 1119.5477926940553
+        },
+        {
+            "description": "",
+            "name": "Root Chord",
+            "type": "real",
+            "units": "mm",
+            "value": 2227.044660132383
+        },
+        {
+            "description": "",
+            "name": "Tail Root chord",
+            "type": "real",
+            "units": "mm",
+            "value": 961.9769044136352
+        },
+        {
+            "description": "",
+            "name": "File Path_0",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/CCA_Drone/cases/case_1527/reference_area/../design_1527.stl"
+        },
+        {
+            "description": "",
+            "name": "File Surface Reference",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/CCA_Drone/cases/case_1527/reference_area/reference_area.txt"
+        }
+    ],
+    "title": "CCA_1_automated"
+}

case_1527/reference_area/mac.txt

@@ -0,0 +1 @@
+1.732145846770

case_1527/reference_area/reference_area.txt

@@ -0,0 +1 @@
+4922101.4624888208

case_1527/reference_area/reference_area_m2.txt

@@ -0,0 +1 @@
+9.844202924978

case_1527/results_10/alpha_7.3947363061559646/force_coefficents_corected.csv

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+,value
+CL,0.73316350651528
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+CMxSkinFriction,-3.161870565761558e-07
+CMySkinFriction,0.0004753779185884288
+CMzSkinFriction,-1.943841490212054e-05

case_1527/results_10/alpha_7.3947363061559646/force_coefficients.csv

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+,value
+CL,7.217410335324845
+CD,0.6124312509666039
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+CMyPressure,-26.759626540512453
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+CLSkinFriction,-0.013083897447596615
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+CFySkinFriction,-2.8233750505732897e-05
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+CMxSkinFriction,-5.391493699776919e-06
+CMySkinFriction,0.00810595184014202
+CMzSkinFriction,-0.00033145598245951715

case_1527/results_10/alpha_7.3947363061559646/forces_actual.csv

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+,value_SI
+L,4737.696744066629
+D,402.01587672907874
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+FzSkinFriction,5.062785854582333
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+MySkinFriction,5.320958606529507
+Mz,-4.429728853374924
+MzPressure,-4.212152485129359
+MzSkinFriction,-0.21757636824582477

case_1527/results_10/alpha_7.3947363061559646/forces_summary.json

@@ -0,0 +1,64 @@
+{
+  "case_id": "case-520d2356-30c1-462b-a541-6cbc8784c40c",
+  "case_name": "alpha_case",
+  "case_status": "Flow360Status.COMPLETED",
+  "reference": {
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+    "velocity_magnitude_m_s": 53.853791953509834,
+    "reference_area_m2": 1.0,
+    "reference_length_m": 1.0,
+    "dynamic_pressure_Pa": 656.4261312507725
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+    "CMySkinFriction": 0.00810595184014202,
+    "CMzSkinFriction": -0.00033145598245951715
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+  "forces_N_and_moments_Nm": {
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+    "FxSkinFriction": 105.74060427337452,
+    "FySkinFriction": -0.018533371615177787,
+    "FzSkinFriction": 5.062785854582333,
+    "Mx": 4.309620986429526,
+    "MxPressure": 4.313160103778323,
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+    "My": -17560.397165097544,
+    "MyPressure": -17565.718123704082,
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+    "Mz": -4.429728853374924,
+    "MzPressure": -4.212152485129359,
+    "MzSkinFriction": -0.21757636824582477
+  }
+}

case_1527/results_6/alpha_-3.5893417819142437/force_coefficents_corected.csv

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+,value
+CL,-0.2237554131988613
+CD,0.02599729602372449
+CFx,0.01193812217924786
+CFy,-6.271140518162597e-05
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+CMx,0.0002518296397103598
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+CFzPressure,-0.2242173501919338
+CMxPressure,0.0002511079724144618
+CMyPressure,0.4105413336028055
+CMzPressure,-0.0001694362264841778
+CLSkinFriction,0.0001677252754195973
+CDSkinFriction,0.01428157310633479
+CFxSkinFriction,0.01426405866950162
+CFySkinFriction,-1.789159701650266e-06
+CFzSkinFriction,-0.0007266996853003456
+CMxSkinFriction,7.216672959798783e-07
+CMySkinFriction,0.003063208789522465
+CMzSkinFriction,9.279938507879059e-07

case_1527/results_6/alpha_-3.5893417819142437/force_coefficients.csv

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+,value
+CL,-2.202693693091891
+CD,0.25592265755826754
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case_1527/results_6/alpha_-3.5893417819142437/forces_actual.csv

@@ -0,0 +1,25 @@
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case_1527/results_6/alpha_-3.5893417819142437/forces_summary.json

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

case_1527/results_8/alpha_4.606313622412102/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_1527/results_8/alpha_4.606313622412102/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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+MzSkinFriction,-0.1407133493534473

case_1527/results_8/alpha_4.606313622412102/forces_summary.json

@@ -0,0 +1,64 @@
+{
+  "case_id": "case-a978dbdc-904b-456e-a26f-4b437bb0d0ab",
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+}

case_1550/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": 5.61253469906857
+        },
+        {
+            "description": "",
+            "name": "Max Wing Blend",
+            "type": "real",
+            "units": "mm",
+            "value": 262.58656965874985
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+        {
+            "description": "",
+            "name": "Inlet Angle 1",
+            "type": "real",
+            "units": "deg",
+            "value": 30.509640792954514
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 2",
+            "type": "real",
+            "units": "deg",
+            "value": 5.504602708175492
+        },
+        {
+            "description": "",
+            "name": "Wing Position",
+            "type": "real",
+            "value": 0.4719991501805698
+        },
+        {
+            "description": "",
+            "name": "Rear Point",
+            "type": "point",
+            "units": "mm",
+            "value": [
+                6817.281266826672,
+                0.0,
+                0.0
+            ]
+        },
+        {
+            "description": "",
+            "name": "Inlet Location",
+            "type": "real",
+            "value": 0.3631515082261768
+        },
+        {
+            "description": "",
+            "name": "NACA 4-digit code",
+            "type": "text",
+            "value": "0012"
+        },
+        {
+            "description": "",
+            "name": "Fore Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 7.910431198021906
+        },
+        {
+            "description": "",
+            "name": "Aft Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 27.40320319950881
+        },
+        {
+            "description": "",
+            "name": "Top Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 71.42809048775842
+        },
+        {
+            "description": "",
+            "name": "Bottom Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 175.7107676993055
+        },
+        {
+            "description": "",
+            "name": "Wing span",
+            "type": "real",
+            "units": "mm",
+            "value": 8872.934884052782
+        },
+        {
+            "description": "",
+            "name": "Rear tail offset",
+            "type": "real",
+            "units": "mm",
+            "value": 1631.1460436431692
+        },
+        {
+            "description": "",
+            "name": "Root Chord",
+            "type": "real",
+            "units": "mm",
+            "value": 1738.7988109842074
+        },
+        {
+            "description": "",
+            "name": "Tail Root chord",
+            "type": "real",
+            "units": "mm",
+            "value": 978.6386260091374
+        },
+        {
+            "description": "",
+            "name": "File Path_0",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/CCA_Drone/cases/case_1550/reference_area/../design_1550.stl"
+        },
+        {
+            "description": "",
+            "name": "File Surface Reference",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/CCA_Drone/cases/case_1550/reference_area/reference_area.txt"
+        }
+    ],
+    "title": "CCA_1_automated"
+}

case_1550/reference_area/mac.txt

@@ -0,0 +1 @@
+1.352399075210

case_1550/reference_area/reference_area.txt

@@ -0,0 +1 @@
+4286262.7415522877

case_1550/reference_area/reference_area_m2.txt

@@ -0,0 +1 @@
+8.572525483105

case_1550/results_3/alpha_-6.672352901855423/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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+CMzSkinFriction,-6.935474429015637e-06

case_1550/results_3/alpha_-6.672352901855423/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_1550/results_3/alpha_-6.672352901855423/forces_actual.csv

@@ -0,0 +1,25 @@
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case_1550/results_3/alpha_-6.672352901855423/forces_summary.json

@@ -0,0 +1,64 @@
+{
+  "case_id": "case-21837858-f615-4b2b-b373-99b3b68f0807",
+  "case_name": "alpha_case",
+  "case_status": "Flow360Status.COMPLETED",
+  "reference": {
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+    "MzSkinFriction": -0.2815275972817824
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+}

case_1550/results_4/alpha_5.057017570288302/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
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case_1550/results_4/alpha_5.057017570288302/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_1550/results_4/alpha_5.057017570288302/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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case_1550/results_4/alpha_5.057017570288302/forces_summary.json

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

case_1550/results_7/alpha_4.145130450521149/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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case_1550/results_7/alpha_4.145130450521149/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_1550/results_7/alpha_4.145130450521149/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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case_1550/results_7/alpha_4.145130450521149/forces_summary.json

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

case_1550/results_9/alpha_6.636892809475377/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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case_1550/results_9/alpha_6.636892809475377/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_1550/results_9/alpha_6.636892809475377/forces_actual.csv

@@ -0,0 +1,25 @@
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case_1550/results_9/alpha_6.636892809475377/forces_summary.json

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