Add files using upload-large-folder tool

case_1486/design_parameter_sample_1486.json

@@ -0,0 +1,117 @@
+{
+    "inputs": [
+        {
+            "description": "",
+            "name": "Dihedral angle",
+            "type": "real",
+            "units": "deg",
+            "value": 7.948959129103091
+        },
+        {
+            "description": "",
+            "name": "Max Wing Blend",
+            "type": "real",
+            "units": "mm",
+            "value": 80.01566526646454
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 1",
+            "type": "real",
+            "units": "deg",
+            "value": 23.532006858040535
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 2",
+            "type": "real",
+            "units": "deg",
+            "value": 7.8121126370452725
+        },
+        {
+            "description": "",
+            "name": "Wing Position",
+            "type": "real",
+            "value": 0.4902516235174541
+        },
+        {
+            "description": "",
+            "name": "Rear Point",
+            "type": "point",
+            "units": "mm",
+            "value": [
+                4500.509664510129,
+                0.0,
+                0.0
+            ]
+        },
+        {
+            "description": "",
+            "name": "Inlet Location",
+            "type": "real",
+            "value": 0.5332231118017884
+        },
+        {
+            "description": "",
+            "name": "NACA 4-digit code",
+            "type": "text",
+            "value": "1412"
+        },
+        {
+            "description": "",
+            "name": "Fore Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 7.3637482196971735
+        },
+        {
+            "description": "",
+            "name": "Aft Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 22.733649362411175
+        },
+        {
+            "description": "",
+            "name": "Top Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 179.31529089205156
+        },
+        {
+            "description": "",
+            "name": "Bottom Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 154.005908044646
+        },
+        {
+            "description": "",
+            "name": "Wing span",
+            "type": "real",
+            "units": "mm",
+            "value": 7480.59664249129
+        },
+        {
+            "description": "",
+            "name": "Rear tail offset",
+            "type": "real",
+            "units": "mm",
+            "value": 1767.1170180865397
+        },
+        {
+            "description": "",
+            "name": "Root Chord",
+            "type": "real",
+            "units": "mm",
+            "value": 1483.2491370594719
+        },
+        {
+            "description": "",
+            "name": "Tail Root chord",
+            "type": "real",
+            "units": "mm",
+            "value": 990.0279807525184
+        }
+    ]
+}

case_1486/param_3.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1486_3",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 157.67008120183448,
+  "alpha": 2.9326446205642824,
+  "beta": 0,
+  "altitude_m": 7124.121808966215,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      2.9326446205642824
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_1486/param_4.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1486_4",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 67.70168771576857,
+  "alpha": 3.1454310310578286,
+  "beta": 0,
+  "altitude_m": 1274.9480385677762,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      3.1454310310578286
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_1486/param_6.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1486_6",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 46.71941009287217,
+  "alpha": -0.1425923327306533,
+  "beta": 0,
+  "altitude_m": 9362.363237494323,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      -0.1425923327306533
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_1486/param_7.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1486_7",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 162.15785778815098,
+  "alpha": -0.808078902495386,
+  "beta": 0,
+  "altitude_m": 9472.039206734555,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      -0.808078902495386
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_1486/params.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1486_1",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 140.78203776478944,
+  "alpha": 4.775052984593849,
+  "beta": 0,
+  "altitude_m": 7311.930294335098,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      4.775052984593849
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_1486/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": 7.948959129103091
+        },
+        {
+            "description": "",
+            "name": "Max Wing Blend",
+            "type": "real",
+            "units": "mm",
+            "value": 80.01566526646454
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 1",
+            "type": "real",
+            "units": "deg",
+            "value": 23.532006858040535
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 2",
+            "type": "real",
+            "units": "deg",
+            "value": 7.8121126370452725
+        },
+        {
+            "description": "",
+            "name": "Wing Position",
+            "type": "real",
+            "value": 0.4902516235174541
+        },
+        {
+            "description": "",
+            "name": "Rear Point",
+            "type": "point",
+            "units": "mm",
+            "value": [
+                4500.509664510129,
+                0.0,
+                0.0
+            ]
+        },
+        {
+            "description": "",
+            "name": "Inlet Location",
+            "type": "real",
+            "value": 0.5332231118017884
+        },
+        {
+            "description": "",
+            "name": "NACA 4-digit code",
+            "type": "text",
+            "value": "1412"
+        },
+        {
+            "description": "",
+            "name": "Fore Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 7.3637482196971735
+        },
+        {
+            "description": "",
+            "name": "Aft Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 22.733649362411175
+        },
+        {
+            "description": "",
+            "name": "Top Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 179.31529089205156
+        },
+        {
+            "description": "",
+            "name": "Bottom Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 154.005908044646
+        },
+        {
+            "description": "",
+            "name": "Wing span",
+            "type": "real",
+            "units": "mm",
+            "value": 7480.59664249129
+        },
+        {
+            "description": "",
+            "name": "Rear tail offset",
+            "type": "real",
+            "units": "mm",
+            "value": 1767.1170180865397
+        },
+        {
+            "description": "",
+            "name": "Root Chord",
+            "type": "real",
+            "units": "mm",
+            "value": 1483.2491370594719
+        },
+        {
+            "description": "",
+            "name": "Tail Root chord",
+            "type": "real",
+            "units": "mm",
+            "value": 990.0279807525184
+        },
+        {
+            "description": "",
+            "name": "File Path_0",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/data_set_v1/case_1486/reference_area/../design_1486.stl"
+        },
+        {
+            "description": "",
+            "name": "File Surface Reference",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/data_set_v1/case_1486/reference_area/reference_area.txt"
+        }
+    ],
+    "title": "CCA_1_automated"
+}

case_1486/reference_area/mac.txt

@@ -0,0 +1 @@
+1.153638217713

case_1486/reference_area/reference_area.txt

@@ -0,0 +1 @@
+2953946.663883884

case_1486/reference_area/reference_area_m2.txt

@@ -0,0 +1 @@
+5.907893327768

case_1486/results/alpha_4.775052984593849/force_coefficents_corected.csv

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+,value
+CL,0.3921160272095672
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+CFy,-8.718442291037317e-05
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+CMxSkinFriction,-4.253801158633946e-06
+CMySkinFriction,0.0006007843253328239
+CMzSkinFriction,-4.912395674299438e-05

case_1486/results/alpha_4.775052984593849/force_coefficients.csv

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+,value
+CL,2.3165796608622973
+CD,0.5303131230818836
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+CMzSkinFriction,-0.00033480784097354575

case_1486/results/alpha_4.775052984593849/forces_actual.csv

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+,value_SI
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+MzPressure,-1.0301972959040613
+MzSkinFriction,-1.8890993515499812

case_1486/results/alpha_4.775052984593849/forces_summary.json

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+{
+  "case_id": "case-4626d0dc-e45e-4c60-8171-1e8714d4e194",
+  "case_name": "alpha_case",
+  "case_status": "Flow360Status.COMPLETED",
+  "reference": {
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+    "MzSkinFriction": -1.8890993515499812
+  }
+}

case_1486/results_10/alpha_-7.906952456915487/force_coefficents_corected.csv

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+,value
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+CMzSkinFriction,-2.951362074070019e-05

case_1486/results_10/alpha_-7.906952456915487/force_coefficients.csv

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+,value
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case_1486/results_10/alpha_-7.906952456915487/forces_actual.csv

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+,value_SI
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+MzSkinFriction,-1.35877000161115

case_1486/results_10/alpha_-7.906952456915487/forces_summary.json

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+{
+  "case_id": "case-8dd9ae1a-ac10-440d-8239-687c1bb446a5",
+  "case_name": "alpha_case",
+  "case_status": "Flow360Status.COMPLETED",
+  "reference": {
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+    "velocity_magnitude_m_s": 149.22579329690885,
+    "reference_area_m2": 1.0,
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+    "dynamic_pressure_Pa": 6754.935055500158
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+  "force_coefficients": {
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+}

case_1486/results_3/alpha_2.9326446205642824/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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case_1486/results_3/alpha_2.9326446205642824/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_1486/results_3/alpha_2.9326446205642824/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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case_1486/results_3/alpha_2.9326446205642824/forces_summary.json

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

case_1486/results_4/alpha_3.1454310310578286/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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case_1486/results_4/alpha_3.1454310310578286/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_1486/results_4/alpha_3.1454310310578286/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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case_1486/results_4/alpha_3.1454310310578286/forces_summary.json

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

case_1486/results_5/alpha_-5.251816699245783/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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case_1486/results_5/alpha_-5.251816699245783/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_1486/results_5/alpha_-5.251816699245783/forces_actual.csv

@@ -0,0 +1,25 @@
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case_1486/results_5/alpha_-5.251816699245783/forces_summary.json

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

case_1486/results_6/alpha_-0.1425923327306533/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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case_1486/results_6/alpha_-0.1425923327306533/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_1486/results_6/alpha_-0.1425923327306533/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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case_1486/results_6/alpha_-0.1425923327306533/forces_summary.json

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

case_1486/results_7/alpha_-0.808078902495386/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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case_1486/results_7/alpha_-0.808078902495386/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_1486/results_7/alpha_-0.808078902495386/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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case_1486/results_7/alpha_-0.808078902495386/forces_summary.json

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

case_1486/results_8/alpha_4.86743224631784/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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case_1486/results_8/alpha_4.86743224631784/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_1486/results_8/alpha_4.86743224631784/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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case_1486/results_8/alpha_4.86743224631784/forces_summary.json

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