Add files using upload-large-folder tool

case_2264/design_parameter_sample_2264.json

@@ -0,0 +1,117 @@
+{
+    "inputs": [
+        {
+            "description": "",
+            "name": "Dihedral angle",
+            "type": "real",
+            "units": "deg",
+            "value": 12.458040502349386
+        },
+        {
+            "description": "",
+            "name": "Max Wing Blend",
+            "type": "real",
+            "units": "mm",
+            "value": 691.4938617510135
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 1",
+            "type": "real",
+            "units": "deg",
+            "value": 23.138808685785214
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 2",
+            "type": "real",
+            "units": "deg",
+            "value": 4.754253606102203
+        },
+        {
+            "description": "",
+            "name": "Wing Position",
+            "type": "real",
+            "value": 0.4766963951982873
+        },
+        {
+            "description": "",
+            "name": "Rear Point",
+            "type": "point",
+            "units": "mm",
+            "value": [
+                6305.14746106265,
+                0.0,
+                0.0
+            ]
+        },
+        {
+            "description": "",
+            "name": "Inlet Location",
+            "type": "real",
+            "value": 0.24386208663247208
+        },
+        {
+            "description": "",
+            "name": "NACA 4-digit code",
+            "type": "text",
+            "value": "1412"
+        },
+        {
+            "description": "",
+            "name": "Fore Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 4.3589237027104115
+        },
+        {
+            "description": "",
+            "name": "Aft Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 27.664749804452047
+        },
+        {
+            "description": "",
+            "name": "Top Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 170.27959629885632
+        },
+        {
+            "description": "",
+            "name": "Bottom Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 173.0648634763705
+        },
+        {
+            "description": "",
+            "name": "Wing span",
+            "type": "real",
+            "units": "mm",
+            "value": 8118.205163517529
+        },
+        {
+            "description": "",
+            "name": "Rear tail offset",
+            "type": "real",
+            "units": "mm",
+            "value": 1020.2487764958272
+        },
+        {
+            "description": "",
+            "name": "Root Chord",
+            "type": "real",
+            "units": "mm",
+            "value": 2308.430489452396
+        },
+        {
+            "description": "",
+            "name": "Tail Root chord",
+            "type": "real",
+            "units": "mm",
+            "value": 859.8795031668901
+        }
+    ]
+}

case_2264/param_4.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_2264_4",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 117.27438558059268,
+  "alpha": -6.4054749784721565,
+  "beta": 0,
+  "altitude_m": 7083.666176951026,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      -6.4054749784721565
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_2264/param_5.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_2264_5",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 41.87229837746305,
+  "alpha": 4.887826802854352,
+  "beta": 0,
+  "altitude_m": 3513.276133408208,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      4.887826802854352
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_2264/param_8.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_2264_8",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 109.36575853412131,
+  "alpha": 9.72029431911535,
+  "beta": 0,
+  "altitude_m": 2563.072390991586,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      9.72029431911535
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_2264/param_9.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_2264_9",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 135.36507444914778,
+  "alpha": 0.43597411152727794,
+  "beta": 0,
+  "altitude_m": 3125.298064163013,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      0.43597411152727794
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_2264/params.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_2264_1",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 170.0226470988781,
+  "alpha": 8.538509170845156,
+  "beta": 0,
+  "altitude_m": 4784.560661512161,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      8.538509170845156
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_2264/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": 12.458040502349386
+        },
+        {
+            "description": "",
+            "name": "Max Wing Blend",
+            "type": "real",
+            "units": "mm",
+            "value": 691.4938617510135
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 1",
+            "type": "real",
+            "units": "deg",
+            "value": 23.138808685785214
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 2",
+            "type": "real",
+            "units": "deg",
+            "value": 4.754253606102203
+        },
+        {
+            "description": "",
+            "name": "Wing Position",
+            "type": "real",
+            "value": 0.4766963951982873
+        },
+        {
+            "description": "",
+            "name": "Rear Point",
+            "type": "point",
+            "units": "mm",
+            "value": [
+                6305.14746106265,
+                0.0,
+                0.0
+            ]
+        },
+        {
+            "description": "",
+            "name": "Inlet Location",
+            "type": "real",
+            "value": 0.24386208663247208
+        },
+        {
+            "description": "",
+            "name": "NACA 4-digit code",
+            "type": "text",
+            "value": "1412"
+        },
+        {
+            "description": "",
+            "name": "Fore Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 4.3589237027104115
+        },
+        {
+            "description": "",
+            "name": "Aft Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 27.664749804452047
+        },
+        {
+            "description": "",
+            "name": "Top Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 170.27959629885632
+        },
+        {
+            "description": "",
+            "name": "Bottom Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 173.0648634763705
+        },
+        {
+            "description": "",
+            "name": "Wing span",
+            "type": "real",
+            "units": "mm",
+            "value": 8118.205163517529
+        },
+        {
+            "description": "",
+            "name": "Rear tail offset",
+            "type": "real",
+            "units": "mm",
+            "value": 1020.2487764958272
+        },
+        {
+            "description": "",
+            "name": "Root Chord",
+            "type": "real",
+            "units": "mm",
+            "value": 2308.430489452396
+        },
+        {
+            "description": "",
+            "name": "Tail Root chord",
+            "type": "real",
+            "units": "mm",
+            "value": 859.8795031668901
+        },
+        {
+            "description": "",
+            "name": "File Path_0",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/CCA_Drone/cases/case_2264/reference_area/../design_2264.stl"
+        },
+        {
+            "description": "",
+            "name": "File Surface Reference",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/CCA_Drone/cases/case_2264/reference_area/reference_area.txt"
+        }
+    ],
+    "title": "CCA_1_automated"
+}

case_2264/reference_area/mac.txt

@@ -0,0 +1 @@
+1.795445936241

case_2264/reference_area/reference_area.txt

@@ -0,0 +1 @@
+4961921.7836880982

case_2264/reference_area/reference_area_m2.txt

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+9.923843567376

case_2264/results/alpha_8.538509170845156/force_coefficents_corected.csv

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+,value
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+CMySkinFriction,0.0003567898167633862
+CMzSkinFriction,-5.174427155823849e-05

case_2264/results/alpha_8.538509170845156/force_coefficients.csv

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+,value
+CL,8.575444918472451
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case_2264/results/alpha_8.538509170845156/forces_actual.csv

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+,value_SI
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+MzSkinFriction,-10.044048893737584

case_2264/results/alpha_8.538509170845156/forces_summary.json

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

case_2264/results_10/alpha_-6.3387221714750375/force_coefficents_corected.csv

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+,value
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case_2264/results_10/alpha_-6.3387221714750375/force_coefficients.csv

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+,value
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case_2264/results_10/alpha_-6.3387221714750375/forces_actual.csv

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+,value_SI
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case_2264/results_10/alpha_-6.3387221714750375/forces_summary.json

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+{
+  "case_id": "case-583f2e6c-84f1-4261-830e-c2c7f66aa7b8",
+  "case_name": "alpha_case",
+  "case_status": "Flow360Status.COMPLETED",
+  "reference": {
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+}

case_2264/results_2/alpha_-4.1525302319662/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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case_2264/results_2/alpha_-4.1525302319662/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_2264/results_2/alpha_-4.1525302319662/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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case_2264/results_2/alpha_-4.1525302319662/forces_summary.json

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

case_2264/results_3/alpha_9.664707990548994/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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case_2264/results_3/alpha_9.664707990548994/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_2264/results_3/alpha_9.664707990548994/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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case_2264/results_3/alpha_9.664707990548994/forces_summary.json

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

case_2264/results_5/alpha_4.887826802854352/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
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case_2264/results_5/alpha_4.887826802854352/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_2264/results_5/alpha_4.887826802854352/forces_actual.csv

@@ -0,0 +1,25 @@
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case_2264/results_5/alpha_4.887826802854352/forces_summary.json

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

case_2264/results_6/alpha_-2.434073149661768/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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case_2264/results_6/alpha_-2.434073149661768/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_2264/results_6/alpha_-2.434073149661768/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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+MzSkinFriction,0.44424758489098964

case_2264/results_6/alpha_-2.434073149661768/forces_summary.json

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

case_2264/results_7/alpha_8.767496619667995/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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case_2264/results_7/alpha_8.767496619667995/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_2264/results_7/alpha_8.767496619667995/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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case_2264/results_7/alpha_8.767496619667995/forces_summary.json

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

case_2264/results_8/alpha_9.72029431911535/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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case_2264/results_8/alpha_9.72029431911535/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_2264/results_8/alpha_9.72029431911535/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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case_2264/results_8/alpha_9.72029431911535/forces_summary.json

@@ -0,0 +1,64 @@
+{
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+  "case_name": "alpha_case",
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+}

case_2264/results_9/alpha_0.43597411152727794/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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+CMzPressure,-0.010038894732384642
+CLSkinFriction,-0.0028908787565709716
+CDSkinFriction,0.1303216393791975
+CFxSkinFriction,0.13033986362225644
+CFySkinFriction,1.6206389475645132e-05
+CFzSkinFriction,-0.0018991633416892116
+CMxSkinFriction,-1.1067546149945719e-05
+CMySkinFriction,0.03603529342021097
+CMzSkinFriction,7.238637290047883e-05