Add files using upload-large-folder tool

case_1534/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": 12.722497666988454
+        },
+        {
+            "description": "",
+            "name": "Max Wing Blend",
+            "type": "real",
+            "units": "mm",
+            "value": 862.1954010102883
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 1",
+            "type": "real",
+            "units": "deg",
+            "value": 10.757638374881894
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 2",
+            "type": "real",
+            "units": "deg",
+            "value": 9.347591005569573
+        },
+        {
+            "description": "",
+            "name": "Wing Position",
+            "type": "real",
+            "value": 0.24724450846337587
+        },
+        {
+            "description": "",
+            "name": "Rear Point",
+            "type": "point",
+            "units": "mm",
+            "value": [
+                5643.510354154515,
+                0.0,
+                0.0
+            ]
+        },
+        {
+            "description": "",
+            "name": "Inlet Location",
+            "type": "real",
+            "value": 0.3911786088153273
+        },
+        {
+            "description": "",
+            "name": "NACA 4-digit code",
+            "type": "text",
+            "value": "4412"
+        },
+        {
+            "description": "",
+            "name": "Fore Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 4.797991287127235
+        },
+        {
+            "description": "",
+            "name": "Aft Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 12.057074938706966
+        },
+        {
+            "description": "",
+            "name": "Top Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 189.50036346060583
+        },
+        {
+            "description": "",
+            "name": "Bottom Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 107.93908589614136
+        },
+        {
+            "description": "",
+            "name": "Wing span",
+            "type": "real",
+            "units": "mm",
+            "value": 12383.868816429842
+        },
+        {
+            "description": "",
+            "name": "Rear tail offset",
+            "type": "real",
+            "units": "mm",
+            "value": 1310.0188178483372
+        },
+        {
+            "description": "",
+            "name": "Root Chord",
+            "type": "real",
+            "units": "mm",
+            "value": 1750.940359870258
+        },
+        {
+            "description": "",
+            "name": "Tail Root chord",
+            "type": "real",
+            "units": "mm",
+            "value": 897.9398988090519
+        },
+        {
+            "description": "",
+            "name": "File Path_0",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/CCA_Drone/cases/case_1534/reference_area/../design_1534.stl"
+        },
+        {
+            "description": "",
+            "name": "File Surface Reference",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/CCA_Drone/cases/case_1534/reference_area/reference_area.txt"
+        }
+    ],
+    "title": "CCA_1_automated"
+}

case_1534/reference_area/mac.txt

@@ -0,0 +1 @@
+1.361842502121

case_1534/reference_area/reference_area.txt

@@ -0,0 +1 @@
+5390656.8258094508

case_1534/results_6/alpha_6.803739414351503/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
+CL,10.938868257184783
+CD,0.6473737792177806
+CFx,-0.6530994822428581
+CFy,-0.004033931632872093
+CFz,10.938527900241317
+CMx,0.008407459664882723
+CMy,-25.487094330971715
+CMz,-0.018015590733050743
+CLPressure,10.946429402304958
+CDPressure,0.495951075738442
+CFxPressure,-0.8043515930735439
+CFyPressure,-0.004180715648956808
+CFzPressure,10.928096936058559
+CMxPressure,0.008350367671074894
+CMyPressure,-25.51525632589066
+CMzPressure,-0.01855219275061956
+CLSkinFriction,-0.0075611451201597485
+CDSkinFriction,0.15142270347933962
+CFxSkinFriction,0.15125211083068574
+CFySkinFriction,0.00014678401608325144
+CFzSkinFriction,0.010430964182762929
+CMxSkinFriction,5.7091993824876065e-05
+CMySkinFriction,0.02816199491893822
+CMzSkinFriction,0.00053660201756804

case_1534/results_6/alpha_6.803739414351503/forces_summary.json

@@ -0,0 +1,64 @@
+{
+  "case_id": "case-1cea1f0d-a7d8-4af9-aacd-9c4f30e240f2",
+  "case_name": "alpha_case",
+  "case_status": "Flow360Status.COMPLETED",
+  "reference": {
+    "density_kg_m3": 0.46519884007476386,
+    "velocity_magnitude_m_s": 100.3471885575714,
+    "reference_area_m2": 1.0,
+    "reference_length_m": 1.0,
+    "dynamic_pressure_Pa": 2342.173409310318
+  },
+  "force_coefficients": {
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+    "CD": 0.6473737792177806,
+    "CFx": -0.6530994822428581,
+    "CFy": -0.004033931632872093,
+    "CFz": 10.938527900241317,
+    "CMx": 0.008407459664882723,
+    "CMy": -25.487094330971715,
+    "CMz": -0.018015590733050743,
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+    "CFyPressure": -0.004180715648956808,
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+    "CMxPressure": 0.008350367671074894,
+    "CMyPressure": -25.51525632589066,
+    "CMzPressure": -0.01855219275061956,
+    "CLSkinFriction": -0.0075611451201597485,
+    "CDSkinFriction": 0.15142270347933962,
+    "CFxSkinFriction": 0.15125211083068574,
+    "CFySkinFriction": 0.00014678401608325144,
+    "CFzSkinFriction": 0.010430964182762929,
+    "CMxSkinFriction": 5.7091993824876065e-05,
+    "CMySkinFriction": 0.02816199491893822,
+    "CMzSkinFriction": 0.00053660201756804
+  },
+  "forces_N_and_moments_Nm": {
+    "L": 25620.726359926903,
+    "D": 1516.2616515686145,
+    "Fx": -1529.6722409435586,
+    "Fy": -9.44816740548877,
+    "Fz": 25619.92918494424,
+    "LPressure": 25638.435872971313,
+    "DPressure": 1161.6034219134265,
+    "FxPressure": -1883.930913033248,
+    "FyPressure": -9.791961024874167,
+    "FzPressure": 25595.49805800192,
+    "LSkinFriction": -17.709513044374635,
+    "DSkinFriction": 354.65822965519027,
+    "FxSkinFriction": 354.2586720896893,
+    "FySkinFriction": 0.3437936193819696,
+    "FzSkinFriction": 24.431126942335666,
+    "Mx": 19.691728466937352,
+    "MxPressure": 19.558009117156146,
+    "MxSkinFriction": 0.13371934982113362,
+    "My": -59695.1946225857,
+    "MyPressure": -59761.15489823799,
+    "MySkinFriction": 65.96027565226939,
+    "Mz": -42.19563756796883,
+    "MzPressure": -43.45245254490079,
+    "MzSkinFriction": 1.2568149769301316
+  }
+}

case_72/design_parameter_sample_72.json

@@ -0,0 +1,117 @@
+{
+    "inputs": [
+        {
+            "description": "",
+            "name": "Dihedral angle",
+            "type": "real",
+            "units": "deg",
+            "value": 13.007549325412901
+        },
+        {
+            "description": "",
+            "name": "Max Wing Blend",
+            "type": "real",
+            "units": "mm",
+            "value": 301.60338165354193
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 1",
+            "type": "real",
+            "units": "deg",
+            "value": 6.826141882507524
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 2",
+            "type": "real",
+            "units": "deg",
+            "value": 5.25052225704746
+        },
+        {
+            "description": "",
+            "name": "Wing Position",
+            "type": "real",
+            "value": 0.2619554402383594
+        },
+        {
+            "description": "",
+            "name": "Rear Point",
+            "type": "point",
+            "units": "mm",
+            "value": [
+                6082.255008474221,
+                0.0,
+                0.0
+            ]
+        },
+        {
+            "description": "",
+            "name": "Inlet Location",
+            "type": "real",
+            "value": 0.5972313777028584
+        },
+        {
+            "description": "",
+            "name": "NACA 4-digit code",
+            "type": "text",
+            "value": "0012"
+        },
+        {
+            "description": "",
+            "name": "Fore Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 2.407458033026791
+        },
+        {
+            "description": "",
+            "name": "Aft Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 28.478715847855227
+        },
+        {
+            "description": "",
+            "name": "Top Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 115.88933759873646
+        },
+        {
+            "description": "",
+            "name": "Bottom Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 192.8563871776849
+        },
+        {
+            "description": "",
+            "name": "Wing span",
+            "type": "real",
+            "units": "mm",
+            "value": 7581.5983136253835
+        },
+        {
+            "description": "",
+            "name": "Rear tail offset",
+            "type": "real",
+            "units": "mm",
+            "value": 1101.8823029780374
+        },
+        {
+            "description": "",
+            "name": "Root Chord",
+            "type": "real",
+            "units": "mm",
+            "value": 1628.4319470426958
+        },
+        {
+            "description": "",
+            "name": "Tail Root chord",
+            "type": "real",
+            "units": "mm",
+            "value": 1160.588538483454
+        }
+    ]
+}

case_72/param_10.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_72_10",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 45.749612310466084,
+  "alpha": 7.630885609676479,
+  "beta": 0,
+  "altitude_m": 3780.6372112094355,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      7.630885609676479
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_72/param_2.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_72_2",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 46.88063871658015,
+  "alpha": 9.641754843984277,
+  "beta": 0,
+  "altitude_m": 4871.868696675447,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      9.641754843984277
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_72/param_3.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_72_3",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 117.17496396933464,
+  "alpha": -3.352243547503936,
+  "beta": 0,
+  "altitude_m": 6834.291235758403,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      -3.352243547503936
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_72/param_4.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_72_4",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 45.16288508975461,
+  "alpha": 4.171621820632657,
+  "beta": 0,
+  "altitude_m": 8155.7671072309095,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      4.171621820632657
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_72/param_5.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_72_5",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 163.90643742486347,
+  "alpha": 2.5670516988548737,
+  "beta": 0,
+  "altitude_m": 3835.071926572173,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      2.5670516988548737
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_72/param_6.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_72_6",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 91.73447884463855,
+  "alpha": 2.021410910524681,
+  "beta": 0,
+  "altitude_m": 4128.836966028386,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      2.021410910524681
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_72/param_7.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_72_7",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 40.669741755915936,
+  "alpha": 6.170645963103421,
+  "beta": 0,
+  "altitude_m": 5921.532611005311,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      6.170645963103421
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_72/param_8.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_72_8",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 146.4630996927344,
+  "alpha": 1.9155415617772604,
+  "beta": 0,
+  "altitude_m": 8273.235590420016,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      1.9155415617772604
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_72/param_9.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_72_9",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 155.3378163936942,
+  "alpha": -7.084599345033562,
+  "beta": 0,
+  "altitude_m": 1024.4199648199462,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      -7.084599345033562
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_72/params.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_72_1",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 99.15455707868239,
+  "alpha": 8.3432574771781,
+  "beta": 0,
+  "altitude_m": 6816.908124829978,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      8.3432574771781
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_72/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": 13.007549325412901
+        },
+        {
+            "description": "",
+            "name": "Max Wing Blend",
+            "type": "real",
+            "units": "mm",
+            "value": 301.60338165354193
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 1",
+            "type": "real",
+            "units": "deg",
+            "value": 6.826141882507524
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 2",
+            "type": "real",
+            "units": "deg",
+            "value": 5.25052225704746
+        },
+        {
+            "description": "",
+            "name": "Wing Position",
+            "type": "real",
+            "value": 0.2619554402383594
+        },
+        {
+            "description": "",
+            "name": "Rear Point",
+            "type": "point",
+            "units": "mm",
+            "value": [
+                6082.255008474221,
+                0.0,
+                0.0
+            ]
+        },
+        {
+            "description": "",
+            "name": "Inlet Location",
+            "type": "real",
+            "value": 0.5972313777028584
+        },
+        {
+            "description": "",
+            "name": "NACA 4-digit code",
+            "type": "text",
+            "value": "0012"
+        },
+        {
+            "description": "",
+            "name": "Fore Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 2.407458033026791
+        },
+        {
+            "description": "",
+            "name": "Aft Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 28.478715847855227
+        },
+        {
+            "description": "",
+            "name": "Top Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 115.88933759873646
+        },
+        {
+            "description": "",
+            "name": "Bottom Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 192.8563871776849
+        },
+        {
+            "description": "",
+            "name": "Wing span",
+            "type": "real",
+            "units": "mm",
+            "value": 7581.5983136253835
+        },
+        {
+            "description": "",
+            "name": "Rear tail offset",
+            "type": "real",
+            "units": "mm",
+            "value": 1101.8823029780374
+        },
+        {
+            "description": "",
+            "name": "Root Chord",
+            "type": "real",
+            "units": "mm",
+            "value": 1628.4319470426958
+        },
+        {
+            "description": "",
+            "name": "Tail Root chord",
+            "type": "real",
+            "units": "mm",
+            "value": 1160.588538483454
+        },
+        {
+            "description": "",
+            "name": "File Path_0",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/CCA_Drone/cases/case_72/reference_area/../design_72.stl"
+        },
+        {
+            "description": "",
+            "name": "File Surface Reference",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/CCA_Drone/cases/case_72/reference_area/reference_area.txt"
+        }
+    ],
+    "title": "CCA_1_automated"
+}

case_72/reference_area/mac.txt

@@ -0,0 +1 @@
+1.266558181033

case_72/reference_area/reference_area.txt

@@ -0,0 +1 @@
+3238956.9920402002

case_72/reference_area/reference_area_m2.txt

@@ -0,0 +1 @@
+6.477913984080

case_72/results/alpha_8.3432574771781/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
+CL,0.8436509709527014
+CD,0.1034773475919096
+CFx,-0.02003428987109906
+CFy,0.0001090726198565105
+CFz,0.8497371061001476
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case_72/results/alpha_8.3432574771781/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_72/results/alpha_8.3432574771781/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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case_72/results/alpha_8.3432574771781/forces_summary.json

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

case_72/results_10/alpha_7.630885609676479/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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case_72/results_10/alpha_7.630885609676479/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_72/results_10/alpha_7.630885609676479/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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case_72/results_10/alpha_7.630885609676479/forces_summary.json

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

case_72/results_2/alpha_9.641754843984277/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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case_72/results_2/alpha_9.641754843984277/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_72/results_2/alpha_9.641754843984277/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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+MzSkinFriction,0.07561626977482098

case_72/results_2/alpha_9.641754843984277/forces_summary.json

@@ -0,0 +1,64 @@
+{
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+  "case_name": "alpha_case",
+  "case_status": "Flow360Status.COMPLETED",
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+    "MzSkinFriction": 0.07561626977482098
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+}

case_72/results_5/alpha_2.5670516988548737/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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case_72/results_5/alpha_2.5670516988548737/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_72/results_5/alpha_2.5670516988548737/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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case_72/results_5/alpha_2.5670516988548737/forces_summary.json

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

case_72/results_6/alpha_2.021410910524681/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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case_72/results_6/alpha_2.021410910524681/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_72/results_6/alpha_2.021410910524681/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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case_72/results_6/alpha_2.021410910524681/forces_summary.json

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

case_72/results_8/alpha_1.9155415617772604/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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case_72/results_8/alpha_1.9155415617772604/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_72/results_8/alpha_1.9155415617772604/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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case_72/results_8/alpha_1.9155415617772604/forces_summary.json

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