Add files using upload-large-folder tool

case_1478/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": 1.4548472276816835
+        },
+        {
+            "description": "",
+            "name": "Max Wing Blend",
+            "type": "real",
+            "units": "mm",
+            "value": 949.4259955228018
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 1",
+            "type": "real",
+            "units": "deg",
+            "value": 44.116402971359044
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 2",
+            "type": "real",
+            "units": "deg",
+            "value": 9.17990715950613
+        },
+        {
+            "description": "",
+            "name": "Wing Position",
+            "type": "real",
+            "value": 0.2696834599576547
+        },
+        {
+            "description": "",
+            "name": "Rear Point",
+            "type": "point",
+            "units": "mm",
+            "value": [
+                6960.925426022296,
+                0.0,
+                0.0
+            ]
+        },
+        {
+            "description": "",
+            "name": "Inlet Location",
+            "type": "real",
+            "value": 0.2400260809330755
+        },
+        {
+            "description": "",
+            "name": "NACA 4-digit code",
+            "type": "text",
+            "value": "1412"
+        },
+        {
+            "description": "",
+            "name": "Fore Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 3.2562068117401184
+        },
+        {
+            "description": "",
+            "name": "Aft Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 12.948626669087128
+        },
+        {
+            "description": "",
+            "name": "Top Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 76.6894288060115
+        },
+        {
+            "description": "",
+            "name": "Bottom Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 102.60241140114942
+        },
+        {
+            "description": "",
+            "name": "Wing span",
+            "type": "real",
+            "units": "mm",
+            "value": 14534.447993808139
+        },
+        {
+            "description": "",
+            "name": "Rear tail offset",
+            "type": "real",
+            "units": "mm",
+            "value": 1427.4900134889745
+        },
+        {
+            "description": "",
+            "name": "Root Chord",
+            "type": "real",
+            "units": "mm",
+            "value": 1990.9725884065438
+        },
+        {
+            "description": "",
+            "name": "Tail Root chord",
+            "type": "real",
+            "units": "mm",
+            "value": 902.8114434595802
+        },
+        {
+            "description": "",
+            "name": "File Path_0",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/data_set_v1/case_1478/reference_area/../design_1478.stl"
+        },
+        {
+            "description": "",
+            "name": "File Surface Reference",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/data_set_v1/case_1478/reference_area/reference_area.txt"
+        }
+    ],
+    "title": "CCA_1_automated"
+}

case_1478/reference_area/mac.txt

@@ -0,0 +1 @@
+1.548534235427

case_1478/reference_area/reference_area.txt

@@ -0,0 +1 @@
+8817899.084851956

case_1478/reference_area/reference_area_m2.txt

@@ -0,0 +1 @@
+17.635798169704

case_1478/results_3/alpha_9.819255011843634/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
+CL,0.893270553696732
+CD,0.06908216088091751
+CFx,-0.08426878843687516
+CFy,-4.474786909157315e-05
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+CFxPressure,-0.09424830572093203
+CFyPressure,-4.567038176118302e-05
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+CMyPressure,-1.643608798873774
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+CDSkinFriction,0.009968510317925486
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+CFySkinFriction,9.225126697135783e-07
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+CMxSkinFriction,1.808407491302244e-07
+CMySkinFriction,-0.001115636289725879
+CMzSkinFriction,4.187598814945094e-06

case_1478/results_3/alpha_9.819255011843634/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
+CL,15.753539195935305
+CD,1.2183190464228821
+CFx,-1.4861473448782165
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+CLSkinFriction,-0.01623960305257423
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+CFySkinFriction,1.6269247252063475e-05
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+CMySkinFriction,-0.030467622358467245
+CMzSkinFriction,0.00011436180452131143

case_1478/results_3/alpha_9.819255011843634/forces_actual.csv

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+,value_SI
+L,96282.62508937911
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+Fx,-9083.048948861304
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+MySkinFriction,-186.212293277055
+Mz,-26.178046580969124
+MzPressure,-26.877004104903598
+MzSkinFriction,0.6989575239138224

case_1478/results_3/alpha_9.819255011843634/forces_summary.json

@@ -0,0 +1,64 @@
+{
+  "case_id": "case-d91b0188-fe25-42c6-8863-5a091970f23c",
+  "case_name": "alpha_case",
+  "case_status": "Flow360Status.COMPLETED",
+  "reference": {
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+    "velocity_magnitude_m_s": 100.41983317731271,
+    "reference_area_m2": 1.0,
+    "reference_length_m": 1.0,
+    "dynamic_pressure_Pa": 6111.809155508481
+  },
+  "force_coefficients": {
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+    "CMySkinFriction": -0.030467622358467245,
+    "CMzSkinFriction": 0.00011436180452131143
+  },
+  "forces_N_and_moments_Nm": {
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+    "D": 7446.133502257733,
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+    "MzPressure": -26.877004104903598,
+    "MzSkinFriction": 0.6989575239138224
+  }
+}

case_1478/results_4/alpha_-3.2076297136759306/force_coefficents_corected.csv

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+,value
+CL,-0.2210913959136621
+CD,0.03808293518178708
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+CFySkinFriction,-4.532059305550923e-06
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+CMxSkinFriction,2.791611252479824e-06
+CMySkinFriction,0.001359452198720799
+CMzSkinFriction,-3.042200366354392e-06

case_1478/results_4/alpha_-3.2076297136759306/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
+CL,-3.8991232353914653
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+CMySkinFriction,0.03712614638520799
+CMzSkinFriction,-8.308138840091936e-05

case_1478/results_4/alpha_-3.2076297136759306/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
+L,-787.27362377509
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+MzSkinFriction,-0.016774998317818157

case_1478/results_4/alpha_-3.2076297136759306/forces_summary.json

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+{
+  "case_id": "case-43b5e7a3-08a2-4992-a822-fce8e942a6d1",
+  "case_name": "alpha_case",
+  "case_status": "Flow360Status.COMPLETED",
+  "reference": {
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+  },
+  "force_coefficients": {
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+    "CMzSkinFriction": -8.308138840091936e-05
+  },
+  "forces_N_and_moments_Nm": {
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+    "MzSkinFriction": -0.016774998317818157
+  }
+}

case_1478/results_5/alpha_8.003202028699743/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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+CMySkinFriction,-0.0008743541398973474
+CMzSkinFriction,4.104516846867801e-05

case_1478/results_5/alpha_8.003202028699743/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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+CMzSkinFriction,0.0011209286611236172

case_1478/results_5/alpha_8.003202028699743/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
+L,23804.640995053058
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+FzSkinFriction,24.481314521352285
+Mx,14.603046547236355
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+Mz,4.927512560323701
+MzPressure,2.9038252103263256
+MzSkinFriction,2.0236873499950288

case_1478/results_5/alpha_8.003202028699743/forces_summary.json

@@ -0,0 +1,64 @@
+{
+  "case_id": "case-e62fbd94-c805-41ea-820c-c40cf2f72ac2",
+  "case_name": "alpha_case",
+  "case_status": "Flow360Status.COMPLETED",
+  "reference": {
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+    "velocity_magnitude_m_s": 86.42700700709071,
+    "reference_area_m2": 1.0,
+    "reference_length_m": 1.0,
+    "dynamic_pressure_Pa": 1805.3667643456342
+  },
+  "force_coefficients": {
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+}

case_1478/results_6/alpha_-3.534778226944713/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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case_1478/results_6/alpha_-3.534778226944713/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_1478/results_6/alpha_-3.534778226944713/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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case_1478/results_6/alpha_-3.534778226944713/forces_summary.json

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

case_1478/results_8/alpha_9.006534071548984/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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case_1478/results_8/alpha_9.006534071548984/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_1478/results_8/alpha_9.006534071548984/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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case_1478/results_8/alpha_9.006534071548984/forces_summary.json

@@ -0,0 +1,64 @@
+{
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+  "case_name": "alpha_case",
+  "case_status": "Flow360Status.COMPLETED",
+  "reference": {
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+}

case_1478/results_9/alpha_1.1816362461447678/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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case_1496/design_parameter_sample_1496.json

@@ -0,0 +1,117 @@
+{
+    "inputs": [
+        {
+            "description": "",
+            "name": "Dihedral angle",
+            "type": "real",
+            "units": "deg",
+            "value": 14.832623545629339
+        },
+        {
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+            "name": "Max Wing Blend",
+            "type": "real",
+            "units": "mm",
+            "value": 55.26380889132307
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+        {
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+            "name": "Inlet Angle 1",
+            "type": "real",
+            "units": "deg",
+            "value": 29.945250628646658
+        },
+        {
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+            "name": "Inlet Angle 2",
+            "type": "real",
+            "units": "deg",
+            "value": 6.100521109179242
+        },
+        {
+            "description": "",
+            "name": "Wing Position",
+            "type": "real",
+            "value": 0.5084103730561276
+        },
+        {
+            "description": "",
+            "name": "Rear Point",
+            "type": "point",
+            "units": "mm",
+            "value": [
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+                0.0
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+        {
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+            "name": "Inlet Location",
+            "type": "real",
+            "value": 0.38676129615614196
+        },
+        {
+            "description": "",
+            "name": "NACA 4-digit code",
+            "type": "text",
+            "value": "2408"
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+        {
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+            "name": "Fore Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 1.4671508895979195
+        },
+        {
+            "description": "",
+            "name": "Aft Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 20.588667062924976
+        },
+        {
+            "description": "",
+            "name": "Top Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 192.05050636216978
+        },
+        {
+            "description": "",
+            "name": "Bottom Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 40.197210886254354
+        },
+        {
+            "description": "",
+            "name": "Wing span",
+            "type": "real",
+            "units": "mm",
+            "value": 12393.410735539259
+        },
+        {
+            "description": "",
+            "name": "Rear tail offset",
+            "type": "real",
+            "units": "mm",
+            "value": 1182.8685432087295
+        },
+        {
+            "description": "",
+            "name": "Root Chord",
+            "type": "real",
+            "units": "mm",
+            "value": 2022.5743454505732
+        },
+        {
+            "description": "",
+            "name": "Tail Root chord",
+            "type": "real",
+            "units": "mm",
+            "value": 847.3162196243813
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+    ]
+}

case_1496/param_10.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1496_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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+  "velocity_magnitude": 30.69425582018047,
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+    "values": [
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+    "unit": "fl.u.deg"
+  }
+}

case_1496/param_2.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1496_2",
+  "max_steps": 3500,
+  "volume_mesh_params": {
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+    "boundary_layer_first_layer_thickness": 1.78684e-05
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+    "variable": "alpha",
+    "values": [
+      -4.404911549155454
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_1496/param_3.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1496_3",
+  "max_steps": 3500,
+  "volume_mesh_params": {
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+    "unit": "fl.u.deg"
+  }
+}

case_1496/param_4.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1496_4",
+  "max_steps": 3500,
+  "volume_mesh_params": {
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+    "unit": "fl.u.deg"
+  }
+}

case_1496/param_5.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1496_5",
+  "max_steps": 3500,
+  "volume_mesh_params": {
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+    "boundary_layer_first_layer_thickness": 1.78684e-05
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+      -1.1653652804427477
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+    "unit": "fl.u.deg"
+  }
+}

case_1496/param_6.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1496_6",
+  "max_steps": 3500,
+  "volume_mesh_params": {
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+    "boundary_layer_first_layer_thickness": 1.78684e-05
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+    "unit": "fl.u.deg"
+  }
+}

case_1496/param_7.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1496_7",
+  "max_steps": 3500,
+  "volume_mesh_params": {
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+    "boundary_layer_first_layer_thickness": 1.78684e-05
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+    "unit": "fl.u.deg"
+  }
+}

case_1496/param_8.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1496_8",
+  "max_steps": 3500,
+  "volume_mesh_params": {
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+    "unit": "fl.u.deg"
+  }
+}

case_1496/param_9.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1496_9",
+  "max_steps": 3500,
+  "volume_mesh_params": {
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+    "unit": "fl.u.deg"
+  }
+}

case_1496/params.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1496_1",
+  "max_steps": 3500,
+  "volume_mesh_params": {
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+    "unit": "fl.u.deg"
+  }
+}

case_1496/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": 14.832623545629339
+        },
+        {
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+            "name": "Max Wing Blend",
+            "type": "real",
+            "units": "mm",
+            "value": 55.26380889132307
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+            "name": "Inlet Angle 1",
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+            "name": "Inlet Angle 2",
+            "type": "real",
+            "units": "deg",
+            "value": 6.100521109179242
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+        {
+            "description": "",
+            "name": "Wing Position",
+            "type": "real",
+            "value": 0.5084103730561276
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+        {
+            "description": "",
+            "name": "Rear Point",
+            "type": "point",
+            "units": "mm",
+            "value": [
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+                0.0,
+                0.0
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+        },
+        {
+            "description": "",
+            "name": "Inlet Location",
+            "type": "real",
+            "value": 0.38676129615614196
+        },
+        {
+            "description": "",
+            "name": "NACA 4-digit code",
+            "type": "text",
+            "value": "2408"
+        },
+        {
+            "description": "",
+            "name": "Fore Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 1.4671508895979195
+        },
+        {
+            "description": "",
+            "name": "Aft Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 20.588667062924976
+        },
+        {
+            "description": "",
+            "name": "Top Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 192.05050636216978
+        },
+        {
+            "description": "",
+            "name": "Bottom Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 40.197210886254354
+        },
+        {
+            "description": "",
+            "name": "Wing span",
+            "type": "real",
+            "units": "mm",
+            "value": 12393.410735539259
+        },
+        {
+            "description": "",
+            "name": "Rear tail offset",
+            "type": "real",
+            "units": "mm",
+            "value": 1182.8685432087295
+        },
+        {
+            "description": "",
+            "name": "Root Chord",
+            "type": "real",
+            "units": "mm",
+            "value": 2022.5743454505732
+        },
+        {
+            "description": "",
+            "name": "Tail Root chord",
+            "type": "real",
+            "units": "mm",
+            "value": 847.3162196243813
+        },
+        {
+            "description": "",
+            "name": "File Path_0",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/data_set_v1/case_1496/reference_area/../design_1496.stl"
+        },
+        {
+            "description": "",
+            "name": "File Surface Reference",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/data_set_v1/case_1496/reference_area/reference_area.txt"
+        }
+    ],
+    "title": "CCA_1_automated"
+}

case_1496/reference_area/mac.txt

@@ -0,0 +1 @@
+1.573113379795

case_1496/reference_area/reference_area.txt

@@ -0,0 +1 @@
+6229238.7719056318

case_1496/reference_area/reference_area_m2.txt

@@ -0,0 +1 @@
+12.458477543811

case_1496/results/alpha_6.822798280396361/force_coefficents_corected.csv

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case_1496/results/alpha_6.822798280396361/force_coefficients.csv

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case_1496/results/alpha_6.822798280396361/forces_actual.csv

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case_1496/results/alpha_6.822798280396361/forces_summary.json

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

case_1496/results_10/alpha_8.061578267132816/force_coefficents_corected.csv

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case_1496/results_10/alpha_8.061578267132816/force_coefficients.csv

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case_1496/results_10/alpha_8.061578267132816/forces_actual.csv

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case_1496/results_10/alpha_8.061578267132816/forces_summary.json

@@ -0,0 +1,64 @@
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+    "FzPressure": 5292.369961722699,
+    "LSkinFriction": -8.53686018805938,
+    "DSkinFriction": 92.9249859183965,
+    "FxSkinFriction": 93.20388017204871,
+    "FySkinFriction": -0.033585939149087925,
+    "FzSkinFriction": 4.579051285915272,
+    "Mx": 2.7029554053630673,
+    "MxPressure": 2.6794564263594847,
+    "MxSkinFriction": 0.023498979008303156,
+    "My": -24420.732890752413,
+    "MyPressure": -24429.665595722305,
+    "MySkinFriction": 8.932704969872486,
+    "Mz": -0.3499145417508246,
+    "MzPressure": -0.21297600049938303,
+    "MzSkinFriction": -0.1369385412500768
+  }
+}

case_1496/results_2/alpha_-4.404911549155454/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
+CL,-0.2625888995430379
+CD,0.03517493490525809
+CFx,0.01490302561338894
+CFy,0.0001159948352339853
+CFz,-0.2645148503135116
+CMx,-0.0009955532078504729
+CMy,0.6578450263742086
+CMz,0.0003978996370588309
+CLPressure,-0.263037634920827
+CDPressure,0.01851373825182979
+CFxPressure,-0.00174342162625026
+CFyPressure,0.000120722013390976
+CFzPressure,-0.2636826053607493
+CMxPressure,-0.0009967919888751496
+CMyPressure,0.6523090238990238
+CMzPressure,0.0004175510521425929
+CLSkinFriction,0.00044873537778931
+CDSkinFriction,0.01666119665342828
+CFxSkinFriction,0.0166464472396392
+CFySkinFriction,-4.727178157173608e-06
+CFzSkinFriction,-0.0008322449527621218
+CMxSkinFriction,1.238781024942621e-06
+CMySkinFriction,0.005536002475185446
+CMzSkinFriction,-1.965141508362933e-05

case_1496/results_2/alpha_-4.404911549155454/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
+CL,-3.2714579082109805
+CD,0.4382261366221716
+CFx,0.18566900993924626
+CFy,0.0014451190499606631
+CFz,-3.295452322635412
+CMx,-0.019511446825579187
+CMy,12.892840031408886
+CMz,0.0077982749180761915
+CLPressure,-3.2770484678382794
+CDPressure,0.23065299226241617
+CFxPressure,-0.021720379180033316
+CFyPressure,0.0015040124928751258
+CFzPressure,-3.2850838175804733
+CMxPressure,-0.019535725196540097
+CMyPressure,12.784342145942713
+CMzPressure,0.008183415096853854
+CLSkinFriction,0.005590559627301664
+CDSkinFriction,0.2075731443597552
+CFxSkinFriction,0.2073893891192796
+CFySkinFriction,-5.889344291674127e-05
+CFzSkinFriction,-0.01036850505493694
+CMxSkinFriction,2.4278370966119877e-05
+CMySkinFriction,0.10849788546618692
+CMzSkinFriction,-0.0003851401787750629