Add files using upload-large-folder tool

case_143/design_parameter_sample_143.json

@@ -0,0 +1,117 @@
+{
+    "inputs": [
+        {
+            "description": "",
+            "name": "Dihedral angle",
+            "type": "real",
+            "units": "deg",
+            "value": 14.19401455896697
+        },
+        {
+            "description": "",
+            "name": "Max Wing Blend",
+            "type": "real",
+            "units": "mm",
+            "value": 131.2443390116421
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 1",
+            "type": "real",
+            "units": "deg",
+            "value": 20.400085962312552
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 2",
+            "type": "real",
+            "units": "deg",
+            "value": 9.67743303093947
+        },
+        {
+            "description": "",
+            "name": "Wing Position",
+            "type": "real",
+            "value": 0.3115343171458187
+        },
+        {
+            "description": "",
+            "name": "Rear Point",
+            "type": "point",
+            "units": "mm",
+            "value": [
+                6525.343770351895,
+                0.0,
+                0.0
+            ]
+        },
+        {
+            "description": "",
+            "name": "Inlet Location",
+            "type": "real",
+            "value": 0.31732877607854293
+        },
+        {
+            "description": "",
+            "name": "NACA 4-digit code",
+            "type": "text",
+            "value": "0012"
+        },
+        {
+            "description": "",
+            "name": "Fore Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 7.200766043501854
+        },
+        {
+            "description": "",
+            "name": "Aft Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 12.45920531003533
+        },
+        {
+            "description": "",
+            "name": "Top Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 188.8670521711437
+        },
+        {
+            "description": "",
+            "name": "Bottom Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 99.43477791112473
+        },
+        {
+            "description": "",
+            "name": "Wing span",
+            "type": "real",
+            "units": "mm",
+            "value": 15531.059525239034
+        },
+        {
+            "description": "",
+            "name": "Rear tail offset",
+            "type": "real",
+            "units": "mm",
+            "value": 1245.8157770836308
+        },
+        {
+            "description": "",
+            "name": "Root Chord",
+            "type": "real",
+            "units": "mm",
+            "value": 2324.2008029083663
+        },
+        {
+            "description": "",
+            "name": "Tail Root chord",
+            "type": "real",
+            "units": "mm",
+            "value": 1065.8610056062896
+        }
+    ]
+}

case_143/params.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_143_1",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 105.55134040973013,
+  "alpha": -7.615566772581033,
+  "beta": 0,
+  "altitude_m": 7710.7596386696505,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      -7.615566772581033
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_143/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": 14.19401455896697
+        },
+        {
+            "description": "",
+            "name": "Max Wing Blend",
+            "type": "real",
+            "units": "mm",
+            "value": 131.2443390116421
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 1",
+            "type": "real",
+            "units": "deg",
+            "value": 20.400085962312552
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 2",
+            "type": "real",
+            "units": "deg",
+            "value": 9.67743303093947
+        },
+        {
+            "description": "",
+            "name": "Wing Position",
+            "type": "real",
+            "value": 0.3115343171458187
+        },
+        {
+            "description": "",
+            "name": "Rear Point",
+            "type": "point",
+            "units": "mm",
+            "value": [
+                6525.343770351895,
+                0.0,
+                0.0
+            ]
+        },
+        {
+            "description": "",
+            "name": "Inlet Location",
+            "type": "real",
+            "value": 0.31732877607854293
+        },
+        {
+            "description": "",
+            "name": "NACA 4-digit code",
+            "type": "text",
+            "value": "0012"
+        },
+        {
+            "description": "",
+            "name": "Fore Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 7.200766043501854
+        },
+        {
+            "description": "",
+            "name": "Aft Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 12.45920531003533
+        },
+        {
+            "description": "",
+            "name": "Top Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 188.8670521711437
+        },
+        {
+            "description": "",
+            "name": "Bottom Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 99.43477791112473
+        },
+        {
+            "description": "",
+            "name": "Wing span",
+            "type": "real",
+            "units": "mm",
+            "value": 15531.059525239034
+        },
+        {
+            "description": "",
+            "name": "Rear tail offset",
+            "type": "real",
+            "units": "mm",
+            "value": 1245.8157770836308
+        },
+        {
+            "description": "",
+            "name": "Root Chord",
+            "type": "real",
+            "units": "mm",
+            "value": 2324.2008029083663
+        },
+        {
+            "description": "",
+            "name": "Tail Root chord",
+            "type": "real",
+            "units": "mm",
+            "value": 1065.8610056062896
+        },
+        {
+            "description": "",
+            "name": "File Path_0",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/CCA_Drone/cases/case_143/reference_area/../design_143.stl"
+        },
+        {
+            "description": "",
+            "name": "File Surface Reference",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/CCA_Drone/cases/case_143/reference_area/reference_area.txt"
+        }
+    ],
+    "title": "CCA_1_automated"
+}

case_143/reference_area/mac.txt

@@ -0,0 +1 @@
+1.807711735595

case_143/reference_area/reference_area.txt

@@ -0,0 +1 @@
+9242129.007568907

case_143/reference_area/reference_area_m2.txt

@@ -0,0 +1 @@
+18.484258015138

case_143/results/alpha_-7.615566772581033/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
+CL,-0.749094409410923
+CD,0.04024440495475199
+CFx,-0.05938482156355624
+CFy,1.381918429038665e-05
+CFz,-0.7478204927044497
+CMx,-0.0008542833143646739
+CMy,1.283041277221041
+CMz,-8.178703163391362e-05
+CLPressure,-0.7497129105071585
+CDPressure,0.02917944411580905
+CFxPressure,-0.07043415198278409
+CFyPressure,1.51454996930855e-05
+CFzPressure,-0.7469671467839056
+CMxPressure,-0.0008541206068213834
+CMyPressure,1.278685587826367
+CMzPressure,-7.628570987433559e-05
+CLSkinFriction,0.0006185010962359673
+CDSkinFriction,0.01106496083894282
+CFxSkinFriction,0.01104933041922787
+CFySkinFriction,-1.326315402849072e-06
+CFzSkinFriction,-0.0008533459205440947
+CMxSkinFriction,-1.627075426161701e-07
+CMySkinFriction,0.004355689394673192
+CMzSkinFriction,-5.501321759836163e-06

case_143/results/alpha_-7.615566772581033/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
+CL,-13.846454341248918
+CD,0.743887964849334
+CFx,-1.0976843639637044
+CFy,0.0002554373679822486
+CFz,-13.822906936156674
+CMx,-0.028545202183338444
+CMy,42.87181085244652
+CMz,-0.0027328490615568346
+CLPressure,-13.857886875094383
+CDPressure,0.5393603737749147
+CFxPressure,-1.301923038327225
+CFyPressure,0.00027995332409518574
+CFzPressure,-13.807133469985171
+CMxPressure,-0.02853976543929594
+CMyPressure,42.72626893171821
+CMzPressure,-0.0025490267402470228
+CLSkinFriction,0.011432533845471316
+CDSkinFriction,0.20452759107441693
+CFxSkinFriction,0.20423867436352078
+CFySkinFriction,-2.4515956115713947e-05
+CFzSkinFriction,-0.015773466171502496
+CMxSkinFriction,-5.436744019970514e-06
+CMySkinFriction,0.14554192072829597
+CMzSkinFriction,-0.00018382232131843715

case_143/results/alpha_-7.615566772581033/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
+L,-41943.215801618324
+D,2253.3605118642968
+Fx,-3325.068716157631
+Fy,0.7737623210268338
+Fz,-41871.8867906664
+LPressure,-41977.84685029127
+DPressure,1633.8123821843526
+FxPressure,-3943.7416690121395
+FyPressure,0.8480252342958764
+FzPressure,-41824.10633516019
+LSkinFriction,34.63104867297439
+DSkinFriction,619.5481296799372
+FxSkinFriction,618.6729528545089
+FySkinFriction,-0.07426291327745398
+FzSkinFriction,-47.78045550621312
+Mx,-86.46817053445027
+MxPressure,-86.45170173146195
+MxSkinFriction,-0.016468802920070365
+My,129865.853746652
+MyPressure,129424.98303427733
+MySkinFriction,440.8707123746116
+Mz,-8.278254859849525
+MzPressure,-7.7214264399642065
+MzSkinFriction,-0.5568284199114472

case_143/results/alpha_-7.615566772581033/forces_summary.json

@@ -0,0 +1,64 @@
+{
+  "case_id": "case-6d3e140c-c5c6-4b5a-945f-66728bb19bf5",
+  "case_name": "alpha_case",
+  "case_status": "Flow360Status.COMPLETED",
+  "reference": {
+    "density_kg_m3": 0.5437830133046433,
+    "velocity_magnitude_m_s": 105.55134040973013,
+    "reference_area_m2": 1.0,
+    "reference_length_m": 1.0,
+    "dynamic_pressure_Pa": 3029.1665120845037
+  },
+  "force_coefficients": {
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+    "CD": 0.743887964849334,
+    "CFx": -1.0976843639637044,
+    "CFy": 0.0002554373679822486,
+    "CFz": -13.822906936156674,
+    "CMx": -0.028545202183338444,
+    "CMy": 42.87181085244652,
+    "CMz": -0.0027328490615568346,
+    "CLPressure": -13.857886875094383,
+    "CDPressure": 0.5393603737749147,
+    "CFxPressure": -1.301923038327225,
+    "CFyPressure": 0.00027995332409518574,
+    "CFzPressure": -13.807133469985171,
+    "CMxPressure": -0.02853976543929594,
+    "CMyPressure": 42.72626893171821,
+    "CMzPressure": -0.0025490267402470228,
+    "CLSkinFriction": 0.011432533845471316,
+    "CDSkinFriction": 0.20452759107441693,
+    "CFxSkinFriction": 0.20423867436352078,
+    "CFySkinFriction": -2.4515956115713947e-05,
+    "CFzSkinFriction": -0.015773466171502496,
+    "CMxSkinFriction": -5.436744019970514e-06,
+    "CMySkinFriction": 0.14554192072829597,
+    "CMzSkinFriction": -0.00018382232131843715
+  },
+  "forces_N_and_moments_Nm": {
+    "L": -41943.215801618324,
+    "D": 2253.3605118642968,
+    "Fx": -3325.068716157631,
+    "Fy": 0.7737623210268338,
+    "Fz": -41871.8867906664,
+    "LPressure": -41977.84685029127,
+    "DPressure": 1633.8123821843526,
+    "FxPressure": -3943.7416690121395,
+    "FyPressure": 0.8480252342958764,
+    "FzPressure": -41824.10633516019,
+    "LSkinFriction": 34.63104867297439,
+    "DSkinFriction": 619.5481296799372,
+    "FxSkinFriction": 618.6729528545089,
+    "FySkinFriction": -0.07426291327745398,
+    "FzSkinFriction": -47.78045550621312,
+    "Mx": -86.46817053445027,
+    "MxPressure": -86.45170173146195,
+    "MxSkinFriction": -0.016468802920070365,
+    "My": 129865.853746652,
+    "MyPressure": 129424.98303427733,
+    "MySkinFriction": 440.8707123746116,
+    "Mz": -8.278254859849525,
+    "MzPressure": -7.7214264399642065,
+    "MzSkinFriction": -0.5568284199114472
+  }
+}

case_70/design_parameter_sample_70.json

@@ -0,0 +1,117 @@
+{
+    "inputs": [
+        {
+            "description": "",
+            "name": "Dihedral angle",
+            "type": "real",
+            "units": "deg",
+            "value": 3.860466408302331
+        },
+        {
+            "description": "",
+            "name": "Max Wing Blend",
+            "type": "real",
+            "units": "mm",
+            "value": 179.33295708887607
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 1",
+            "type": "real",
+            "units": "deg",
+            "value": 34.73587271211598
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 2",
+            "type": "real",
+            "units": "deg",
+            "value": 9.896204485012555
+        },
+        {
+            "description": "",
+            "name": "Wing Position",
+            "type": "real",
+            "value": 0.3005925929925621
+        },
+        {
+            "description": "",
+            "name": "Rear Point",
+            "type": "point",
+            "units": "mm",
+            "value": [
+                5979.325263452651,
+                0.0,
+                0.0
+            ]
+        },
+        {
+            "description": "",
+            "name": "Inlet Location",
+            "type": "real",
+            "value": 0.22254528974530863
+        },
+        {
+            "description": "",
+            "name": "NACA 4-digit code",
+            "type": "text",
+            "value": "4412"
+        },
+        {
+            "description": "",
+            "name": "Fore Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 2.355991591973586
+        },
+        {
+            "description": "",
+            "name": "Aft Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 26.6606291265945
+        },
+        {
+            "description": "",
+            "name": "Top Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 85.02364801245707
+        },
+        {
+            "description": "",
+            "name": "Bottom Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 63.899334393452484
+        },
+        {
+            "description": "",
+            "name": "Wing span",
+            "type": "real",
+            "units": "mm",
+            "value": 15447.754727827009
+        },
+        {
+            "description": "",
+            "name": "Rear tail offset",
+            "type": "real",
+            "units": "mm",
+            "value": 1679.9451756025535
+        },
+        {
+            "description": "",
+            "name": "Root Chord",
+            "type": "real",
+            "units": "mm",
+            "value": 1685.8044227396254
+        },
+        {
+            "description": "",
+            "name": "Tail Root chord",
+            "type": "real",
+            "units": "mm",
+            "value": 952.490601178443
+        }
+    ]
+}

case_70/param_10.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_70_10",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 60.00198675236497,
+  "alpha": 7.384050571453876,
+  "beta": 0,
+  "altitude_m": 5758.830483935442,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      7.384050571453876
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_70/param_2.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_70_2",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 81.6445429157441,
+  "alpha": 3.8479900686780244,
+  "beta": 0,
+  "altitude_m": 8475.44853765,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      3.8479900686780244
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_70/param_3.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_70_3",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 83.8715168288636,
+  "alpha": 7.152098934744119,
+  "beta": 0,
+  "altitude_m": 2177.944706412504,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      7.152098934744119
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_70/param_4.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_70_4",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 159.57691101216318,
+  "alpha": 9.040768087718003,
+  "beta": 0,
+  "altitude_m": 6473.567388930765,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      9.040768087718003
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_70/param_5.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_70_5",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 68.59963927887576,
+  "alpha": 7.66424681373182,
+  "beta": 0,
+  "altitude_m": 6847.979863355818,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      7.66424681373182
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_70/param_6.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_70_6",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 99.07132195609807,
+  "alpha": 9.961154171458563,
+  "beta": 0,
+  "altitude_m": 9562.305554199103,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      9.961154171458563
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_70/param_7.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_70_7",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 70.02378769134467,
+  "alpha": -0.010610582362317267,
+  "beta": 0,
+  "altitude_m": 4304.6246603322215,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      -0.010610582362317267
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_70/param_8.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_70_8",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 116.30895767151952,
+  "alpha": 9.496069231749615,
+  "beta": 0,
+  "altitude_m": 4242.54893316918,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      9.496069231749615
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_70/param_9.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_70_9",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 124.43341946240875,
+  "alpha": 9.292131019047694,
+  "beta": 0,
+  "altitude_m": 8137.626250640648,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      9.292131019047694
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_70/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": 3.860466408302331
+        },
+        {
+            "description": "",
+            "name": "Max Wing Blend",
+            "type": "real",
+            "units": "mm",
+            "value": 179.33295708887607
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 1",
+            "type": "real",
+            "units": "deg",
+            "value": 34.73587271211598
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 2",
+            "type": "real",
+            "units": "deg",
+            "value": 9.896204485012555
+        },
+        {
+            "description": "",
+            "name": "Wing Position",
+            "type": "real",
+            "value": 0.3005925929925621
+        },
+        {
+            "description": "",
+            "name": "Rear Point",
+            "type": "point",
+            "units": "mm",
+            "value": [
+                5979.325263452651,
+                0.0,
+                0.0
+            ]
+        },
+        {
+            "description": "",
+            "name": "Inlet Location",
+            "type": "real",
+            "value": 0.22254528974530863
+        },
+        {
+            "description": "",
+            "name": "NACA 4-digit code",
+            "type": "text",
+            "value": "4412"
+        },
+        {
+            "description": "",
+            "name": "Fore Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 2.355991591973586
+        },
+        {
+            "description": "",
+            "name": "Aft Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 26.6606291265945
+        },
+        {
+            "description": "",
+            "name": "Top Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 85.02364801245707
+        },
+        {
+            "description": "",
+            "name": "Bottom Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 63.899334393452484
+        },
+        {
+            "description": "",
+            "name": "Wing span",
+            "type": "real",
+            "units": "mm",
+            "value": 15447.754727827009
+        },
+        {
+            "description": "",
+            "name": "Rear tail offset",
+            "type": "real",
+            "units": "mm",
+            "value": 1679.9451756025535
+        },
+        {
+            "description": "",
+            "name": "Root Chord",
+            "type": "real",
+            "units": "mm",
+            "value": 1685.8044227396254
+        },
+        {
+            "description": "",
+            "name": "Tail Root chord",
+            "type": "real",
+            "units": "mm",
+            "value": 952.490601178443
+        },
+        {
+            "description": "",
+            "name": "File Path_0",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/CCA_Drone/cases/case_70/reference_area/../design_70.stl"
+        },
+        {
+            "description": "",
+            "name": "File Surface Reference",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/CCA_Drone/cases/case_70/reference_area/reference_area.txt"
+        }
+    ],
+    "title": "CCA_1_automated"
+}

case_70/reference_area/mac.txt

@@ -0,0 +1 @@
+1.311181217686

case_70/reference_area/reference_area.txt

@@ -0,0 +1 @@
+6646051.2589603998

case_70/reference_area/reference_area_m2.txt

@@ -0,0 +1 @@
+13.292102517921

case_70/results_10/alpha_7.384050571453876/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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+CMzSkinFriction,7.1809618747001e-05

case_70/results_10/alpha_7.384050571453876/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_70/results_10/alpha_7.384050571453876/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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+MzSkinFriction,1.527309560771907

case_70/results_10/alpha_7.384050571453876/forces_summary.json

@@ -0,0 +1,64 @@
+{
+  "case_id": "case-1c3f9776-160f-405e-b234-3a0068955188",
+  "case_name": "alpha_case",
+  "case_status": "Flow360Status.COMPLETED",
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+}

case_70/results_2/alpha_3.8479900686780244/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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case_70/results_2/alpha_3.8479900686780244/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_70/results_2/alpha_3.8479900686780244/forces_actual.csv

@@ -0,0 +1,25 @@
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case_70/results_2/alpha_3.8479900686780244/forces_summary.json

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

case_70/results_3/alpha_7.152098934744119/force_coefficents_corected.csv

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case_70/results_3/alpha_7.152098934744119/force_coefficients.csv

@@ -0,0 +1,25 @@
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case_70/results_3/alpha_7.152098934744119/forces_actual.csv

@@ -0,0 +1,25 @@
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+MzSkinFriction,3.674080772835369

case_70/results_3/alpha_7.152098934744119/forces_summary.json

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

case_70/results_4/alpha_9.040768087718003/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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case_70/results_4/alpha_9.040768087718003/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_70/results_4/alpha_9.040768087718003/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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+MzSkinFriction,-2.2488296649929675

case_70/results_4/alpha_9.040768087718003/forces_summary.json

@@ -0,0 +1,64 @@
+{
+  "case_id": "case-7d08724f-5da2-4871-8a04-cb22eb25bacf",
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+}

case_70/results_5/alpha_7.66424681373182/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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case_70/results_5/alpha_7.66424681373182/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_70/results_5/alpha_7.66424681373182/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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case_70/results_5/alpha_7.66424681373182/forces_summary.json

@@ -0,0 +1,64 @@
+{
+  "case_id": "case-61128a20-d861-4263-b7e7-2af85cf43de3",
+  "case_name": "alpha_case",
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+}

case_70/results_6/alpha_9.961154171458563/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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case_70/results_6/alpha_9.961154171458563/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_70/results_6/alpha_9.961154171458563/forces_actual.csv

@@ -0,0 +1,25 @@
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+MzSkinFriction,6.122379800070296

case_70/results_6/alpha_9.961154171458563/forces_summary.json

@@ -0,0 +1,64 @@
+{
+  "case_id": "case-9a29a22f-8d52-40ff-a590-0785bbe891ee",
+  "case_name": "alpha_case",
+  "case_status": "Flow360Status.COMPLETED",
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+    "CLSkinFriction": -0.0156749003897104,
+    "CDSkinFriction": 0.1710536873717649,
+    "CFxSkinFriction": 0.17118654849071535,
+    "CFySkinFriction": 1.5719450834489423e-05,
+    "CFzSkinFriction": 0.014150338566294602,
+    "CMxSkinFriction": -0.0017895159580429627,
+    "CMySkinFriction": -0.005227619238948846,
+    "CMzSkinFriction": 0.002859132238553909
+  },
+  "forces_N_and_moments_Nm": {
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+    "D": 2416.9895627981805,
+    "Fx": -4153.083963869006,
+    "Fy": -0.6391373276030473,
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+    "FxPressure": -4519.6529012516985,
+    "FyPressure": -0.6727980470887919,
+    "FzPressure": 37589.36580925703,
+    "LSkinFriction": -33.565321750425746,
+    "DSkinFriction": 366.2844362952983,
+    "FxSkinFriction": 366.56893738269406,
+    "FySkinFriction": 0.03366071948667637,
+    "FzSkinFriction": 30.300713564146065,
+    "Mx": -3732.796891806283,
+    "MxPressure": -3728.9649262168987,
+    "MxSkinFriction": -3.8319655893100797,
+    "My": -103977.76471807716,
+    "MyPressure": -103966.57059770756,
+    "MySkinFriction": -11.194120369608012,
+    "Mz": -1335.426016380576,
+    "MzPressure": -1341.5483961806513,
+    "MzSkinFriction": 6.122379800070296
+  }
+}

case_70/results_7/alpha_-0.010610582362317267/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
+CL,0.3494917909310937
+CD,0.02631949855911172
+CFx,0.02638422035161442
+CFy,-4.400725211380433e-05
+CFz,0.3494869108408267
+CMx,-0.00169773112066354
+CMy,-0.7607872743111964
+CMz,-0.0003851330574265147
+CLPressure,0.3495917796699319
+CDPressure,0.01327285538192216
+CFxPressure,0.01333759591501762
+CFyPressure,-4.598766526975791e-05
+CFzPressure,0.3495893156805388
+CMxPressure,-0.00169877041040891
+CMyPressure,-0.7628897751432685
+CMzPressure,-0.0004000694146730699
+CLSkinFriction,-9.998873883836826e-05
+CDSkinFriction,0.01304664317718957
+CFxSkinFriction,0.01304662443659682
+CFySkinFriction,1.980413155928643e-06
+CFzSkinFriction,-0.000102404839712308
+CMxSkinFriction,1.039289745238768e-06
+CMySkinFriction,0.002102500832071933
+CMzSkinFriction,1.493635724661021e-05

case_70/results_7/alpha_-0.010610582362317267/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
+CL,4.645480714227911
+CD,0.3498414730679871
+CFx,0.3507017617690766
+CFy,-0.0005849489066286829
+CFz,4.645415847567785
+CMx,-0.029588660945690678
+CMy,-13.259270821749505
+CMz,-0.006712235710632746
+CLPressure,4.6468097747951855
+CDPressure,0.1764241544420489
+CFxPressure,0.17728469224501855
+CFyPressure,-0.0006112727613254573
+CFzPressure,4.646777023195569
+CMxPressure,-0.029606774056492396
+CMyPressure,-13.295913952985682
+CMzPressure,-0.006972551849597849
+CLSkinFriction,-0.00132906056727722
+CDSkinFriction,0.17341731862593837
+CFxSkinFriction,0.1734170695240583
+CFySkinFriction,2.6323854696442993e-05
+CFzSkinFriction,-0.0013611756277872656
+CMxSkinFriction,1.8113110799420573e-05
+CMySkinFriction,0.036643131236172896
+CMzSkinFriction,0.00026031613896606285