Add files using upload-large-folder tool

case_1611/design_parameter_sample_1611.json

@@ -0,0 +1,117 @@
+{
+    "inputs": [
+        {
+            "description": "",
+            "name": "Dihedral angle",
+            "type": "real",
+            "units": "deg",
+            "value": 1.5226506656051386
+        },
+        {
+            "description": "",
+            "name": "Max Wing Blend",
+            "type": "real",
+            "units": "mm",
+            "value": 790.0652480918534
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 1",
+            "type": "real",
+            "units": "deg",
+            "value": 44.52416376399969
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 2",
+            "type": "real",
+            "units": "deg",
+            "value": 1.5226536637091015
+        },
+        {
+            "description": "",
+            "name": "Wing Position",
+            "type": "real",
+            "value": 0.4545587070549959
+        },
+        {
+            "description": "",
+            "name": "Rear Point",
+            "type": "point",
+            "units": "mm",
+            "value": [
+                6961.608559115917,
+                0.0,
+                0.0
+            ]
+        },
+        {
+            "description": "",
+            "name": "Inlet Location",
+            "type": "real",
+            "value": 0.34114901957905486
+        },
+        {
+            "description": "",
+            "name": "NACA 4-digit code",
+            "type": "text",
+            "value": "1412"
+        },
+        {
+            "description": "",
+            "name": "Fore Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 3.618133372667713
+        },
+        {
+            "description": "",
+            "name": "Aft Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 20.944094303830248
+        },
+        {
+            "description": "",
+            "name": "Top Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 159.3281274309478
+        },
+        {
+            "description": "",
+            "name": "Bottom Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 83.09818478273556
+        },
+        {
+            "description": "",
+            "name": "Wing span",
+            "type": "real",
+            "units": "mm",
+            "value": 13213.217093625393
+        },
+        {
+            "description": "",
+            "name": "Rear tail offset",
+            "type": "real",
+            "units": "mm",
+            "value": 1232.750746941807
+        },
+        {
+            "description": "",
+            "name": "Root Chord",
+            "type": "real",
+            "units": "mm",
+            "value": 2363.2936222524786
+        },
+        {
+            "description": "",
+            "name": "Tail Root chord",
+            "type": "real",
+            "units": "mm",
+            "value": 840.5798525179611
+        }
+    ]
+}

case_1611/param_10.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1611_10",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 140.4978215961065,
+  "alpha": -6.301771826101367,
+  "beta": 0,
+  "altitude_m": 199.99189842836597,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      -6.301771826101367
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_1611/param_2.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1611_2",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 124.95098239981454,
+  "alpha": -3.4518518905236917,
+  "beta": 0,
+  "altitude_m": 536.6556061668687,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      -3.4518518905236917
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_1611/param_6.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1611_6",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 134.75976612517184,
+  "alpha": -2.927965714762724,
+  "beta": 0,
+  "altitude_m": 2731.61179651077,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      -2.927965714762724
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_2307/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": 8.209085687367786
+        },
+        {
+            "description": "",
+            "name": "Max Wing Blend",
+            "type": "real",
+            "units": "mm",
+            "value": 466.88016612621
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 1",
+            "type": "real",
+            "units": "deg",
+            "value": 18.327042698918817
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 2",
+            "type": "real",
+            "units": "deg",
+            "value": 5.813040666071458
+        },
+        {
+            "description": "",
+            "name": "Wing Position",
+            "type": "real",
+            "value": 0.22172679356943104
+        },
+        {
+            "description": "",
+            "name": "Rear Point",
+            "type": "point",
+            "units": "mm",
+            "value": [
+                6074.210331976352,
+                0.0,
+                0.0
+            ]
+        },
+        {
+            "description": "",
+            "name": "Inlet Location",
+            "type": "real",
+            "value": 0.521397323260415
+        },
+        {
+            "description": "",
+            "name": "NACA 4-digit code",
+            "type": "text",
+            "value": "1412"
+        },
+        {
+            "description": "",
+            "name": "Fore Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 4.45751372967794
+        },
+        {
+            "description": "",
+            "name": "Aft Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 17.80029255401351
+        },
+        {
+            "description": "",
+            "name": "Top Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 184.5306160754349
+        },
+        {
+            "description": "",
+            "name": "Bottom Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 189.98100269120414
+        },
+        {
+            "description": "",
+            "name": "Wing span",
+            "type": "real",
+            "units": "mm",
+            "value": 17218.6144931914
+        },
+        {
+            "description": "",
+            "name": "Rear tail offset",
+            "type": "real",
+            "units": "mm",
+            "value": 1148.5235714804614
+        },
+        {
+            "description": "",
+            "name": "Root Chord",
+            "type": "real",
+            "units": "mm",
+            "value": 2409.2738890282853
+        },
+        {
+            "description": "",
+            "name": "Tail Root chord",
+            "type": "real",
+            "units": "mm",
+            "value": 908.5323554038722
+        },
+        {
+            "description": "",
+            "name": "File Path_0",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/CCA_Drone/cases/case_2307/reference_area/../design_2307.stl"
+        },
+        {
+            "description": "",
+            "name": "File Surface Reference",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/CCA_Drone/cases/case_2307/reference_area/reference_area.txt"
+        }
+    ],
+    "title": "CCA_1_automated"
+}

case_2307/reference_area/mac.txt

@@ -0,0 +1 @@
+1.873879691466

case_2307/reference_area/reference_area.txt

@@ -0,0 +1 @@
+10766087.721941559

case_2307/reference_area/reference_area_m2.txt

@@ -0,0 +1 @@
+21.532175443883

case_2307/results/alpha_2.2034792529820653/force_coefficients.csv

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+,value
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case_2307/results/alpha_2.2034792529820653/forces_summary.json

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

case_2307/results_3/alpha_-0.036278702930132134/force_coefficents_corected.csv

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+,value
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case_2307/results_3/alpha_-0.036278702930132134/force_coefficients.csv

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+,value
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case_2307/results_3/alpha_-0.036278702930132134/forces_actual.csv

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+,value_SI
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case_2307/results_3/alpha_-0.036278702930132134/forces_summary.json

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+{
+  "case_id": "case-bad94b08-4fd3-4567-a49c-8d0fb758fdc7",
+  "case_name": "alpha_case",
+  "case_status": "Flow360Status.COMPLETED",
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+}

case_2307/results_4/alpha_-2.961940694322619/force_coefficents_corected.csv

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+,value
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+CMzSkinFriction,-1.417964183607845e-05

case_2307/results_4/alpha_-2.961940694322619/force_coefficients.csv

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+,value
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case_2307/results_4/alpha_-2.961940694322619/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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case_2307/results_4/alpha_-2.961940694322619/forces_summary.json

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

case_2307/results_6/alpha_-0.4286476882981747/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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case_2307/results_6/alpha_-0.4286476882981747/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_2307/results_6/alpha_-0.4286476882981747/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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case_2307/results_6/alpha_-0.4286476882981747/forces_summary.json

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

case_2307/results_7/alpha_4.559312018820693/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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case_2307/results_7/alpha_4.559312018820693/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_2307/results_7/alpha_4.559312018820693/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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case_2307/results_7/alpha_4.559312018820693/forces_summary.json

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

case_2307/results_9/alpha_-1.3709663968478862/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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case_2307/results_9/alpha_-1.3709663968478862/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_2307/results_9/alpha_-1.3709663968478862/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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+LSkinFriction,11.25808153711025
+DSkinFriction,1511.7806448435942
+FxSkinFriction,1511.6172418256556
+FySkinFriction,0.0077139368303993025
+FzSkinFriction,-24.915391608554135
+Mx,295.84542446726556
+MxPressure,295.8620093623507
+MxSkinFriction,-0.01658489507824216
+My,15485.354253649657
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+MySkinFriction,642.1569615710572
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+MzPressure,15.98995521024484
+MzSkinFriction,-2.8410943229165753

case_2307/results_9/alpha_-1.3709663968478862/forces_summary.json

@@ -0,0 +1,64 @@
+{
+  "case_id": "case-06a37c5e-df43-4d34-b7d8-944f0591e2ed",
+  "case_name": "alpha_case",
+  "case_status": "Flow360Status.COMPLETED",
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+    "MzSkinFriction": -2.8410943229165753
+  }
+}

case_759/design_parameter_sample_759.json

@@ -0,0 +1,117 @@
+{
+    "inputs": [
+        {
+            "description": "",
+            "name": "Dihedral angle",
+            "type": "real",
+            "units": "deg",
+            "value": 2.672679138661261
+        },
+        {
+            "description": "",
+            "name": "Max Wing Blend",
+            "type": "real",
+            "units": "mm",
+            "value": 823.479432833007
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+        {
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+            "name": "Inlet Angle 1",
+            "type": "real",
+            "units": "deg",
+            "value": 42.96440783495538
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 2",
+            "type": "real",
+            "units": "deg",
+            "value": 3.1394390576133517
+        },
+        {
+            "description": "",
+            "name": "Wing Position",
+            "type": "real",
+            "value": 0.3848850944488518
+        },
+        {
+            "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": 0.4770060844270694
+        },
+        {
+            "description": "",
+            "name": "NACA 4-digit code",
+            "type": "text",
+            "value": "2408"
+        },
+        {
+            "description": "",
+            "name": "Fore Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 0.4909914376681665
+        },
+        {
+            "description": "",
+            "name": "Aft Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 17.600409041579866
+        },
+        {
+            "description": "",
+            "name": "Top Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 85.19723959121862
+        },
+        {
+            "description": "",
+            "name": "Bottom Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 137.75147881335818
+        },
+        {
+            "description": "",
+            "name": "Wing span",
+            "type": "real",
+            "units": "mm",
+            "value": 16220.726809777412
+        },
+        {
+            "description": "",
+            "name": "Rear tail offset",
+            "type": "real",
+            "units": "mm",
+            "value": 1137.818892206028
+        },
+        {
+            "description": "",
+            "name": "Root Chord",
+            "type": "real",
+            "units": "mm",
+            "value": 2348.847128748669
+        },
+        {
+            "description": "",
+            "name": "Tail Root chord",
+            "type": "real",
+            "units": "mm",
+            "value": 832.1362763597515
+        }
+    ]
+}

case_759/param_10.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_759_10",
+  "max_steps": 3500,
+  "volume_mesh_params": {
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+    "boundary_layer_first_layer_thickness": 1.78684e-05
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+  "altitude_m": 7117.747117092589,
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+    "values": [
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+    "unit": "fl.u.deg"
+  }
+}

case_759/param_2.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_759_2",
+  "max_steps": 3500,
+  "volume_mesh_params": {
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+    "boundary_layer_first_layer_thickness": 1.78684e-05
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+  "velocity_magnitude": 47.39879841443009,
+  "alpha": 2.330649366950251,
+  "beta": 0,
+  "altitude_m": 6025.554776908606,
+  "sweep_schema": {
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+    "values": [
+      2.330649366950251
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_759/param_3.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_759_3",
+  "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": 98.67308184182596,
+  "alpha": -5.922617887578474,
+  "beta": 0,
+  "altitude_m": 5184.556403074827,
+  "sweep_schema": {
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+    "values": [
+      -5.922617887578474
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_759/param_6.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_759_6",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 139.04632924186097,
+  "alpha": -4.661270639884415,
+  "beta": 0,
+  "altitude_m": 6908.185093269644,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      -4.661270639884415
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_759/param_7.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_759_7",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 50.38988160272759,
+  "alpha": 5.847802690291434,
+  "beta": 0,
+  "altitude_m": 8137.301726945328,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      5.847802690291434
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_759/param_8.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_759_8",
+  "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": 43.06688900221681,
+  "alpha": 0.19513127946244602,
+  "beta": 0,
+  "altitude_m": 2630.739365103935,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      0.19513127946244602
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_759/param_9.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_759_9",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 169.69433159052593,
+  "alpha": 8.990854517337315,
+  "beta": 0,
+  "altitude_m": 3067.5970002889567,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      8.990854517337315
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_759/params.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_759_1",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 98.37842294401091,
+  "alpha": -4.033162075344691,
+  "beta": 0,
+  "altitude_m": 7737.838674382656,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      -4.033162075344691
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_759/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": 2.672679138661261
+        },
+        {
+            "description": "",
+            "name": "Max Wing Blend",
+            "type": "real",
+            "units": "mm",
+            "value": 823.479432833007
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 1",
+            "type": "real",
+            "units": "deg",
+            "value": 42.96440783495538
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 2",
+            "type": "real",
+            "units": "deg",
+            "value": 3.1394390576133517
+        },
+        {
+            "description": "",
+            "name": "Wing Position",
+            "type": "real",
+            "value": 0.3848850944488518
+        },
+        {
+            "description": "",
+            "name": "Rear Point",
+            "type": "point",
+            "units": "mm",
+            "value": [
+                4709.663091235383,
+                0.0,
+                0.0
+            ]
+        },
+        {
+            "description": "",
+            "name": "Inlet Location",
+            "type": "real",
+            "value": 0.4770060844270694
+        },
+        {
+            "description": "",
+            "name": "NACA 4-digit code",
+            "type": "text",
+            "value": "2408"
+        },
+        {
+            "description": "",
+            "name": "Fore Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 0.4909914376681665
+        },
+        {
+            "description": "",
+            "name": "Aft Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 17.600409041579866
+        },
+        {
+            "description": "",
+            "name": "Top Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 85.19723959121862
+        },
+        {
+            "description": "",
+            "name": "Bottom Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 137.75147881335818
+        },
+        {
+            "description": "",
+            "name": "Wing span",
+            "type": "real",
+            "units": "mm",
+            "value": 16220.726809777412
+        },
+        {
+            "description": "",
+            "name": "Rear tail offset",
+            "type": "real",
+            "units": "mm",
+            "value": 1137.818892206028
+        },
+        {
+            "description": "",
+            "name": "Root Chord",
+            "type": "real",
+            "units": "mm",
+            "value": 2348.847128748669
+        },
+        {
+            "description": "",
+            "name": "Tail Root chord",
+            "type": "real",
+            "units": "mm",
+            "value": 832.1362763597515
+        },
+        {
+            "description": "",
+            "name": "File Path_0",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/CCA_Drone/cases/case_759/reference_area/../design_759.stl"
+        },
+        {
+            "description": "",
+            "name": "File Surface Reference",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/CCA_Drone/cases/case_759/reference_area/reference_area.txt"
+        }
+    ],
+    "title": "CCA_1_automated"
+}

case_759/reference_area/mac.txt

@@ -0,0 +1 @@
+1.826881100138

case_759/reference_area/reference_area.txt

@@ -0,0 +1 @@
+10052691.092438919

case_759/reference_area/reference_area_m2.txt

@@ -0,0 +1 @@
+20.105382184878

case_759/results/alpha_-4.033162075344691/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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+CD,0.02073244639764586
+CFx,0.001615053080039563
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+CLPressure,-0.271220347411259
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+CFxPressure,-0.007307762953503682
+CFyPressure,-0.0001428055105737852
+CFzPressure,-0.2713784306241628
+CMxPressure,0.0002297579767166827
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+CMzPressure,-0.0003894385618330249
+CLSkinFriction,0.0001410244630900964
+CDSkinFriction,0.008935024749923975
+CFxSkinFriction,0.00892281603354325
+CFySkinFriction,-1.315778328972951e-07
+CFzSkinFriction,-0.0004877593797020469
+CMxSkinFriction,1.401498337423493e-07
+CMySkinFriction,0.001511926512390108
+CMzSkinFriction,1.533290356780519e-06

case_759/results/alpha_-4.033162075344691/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
+CL,-5.450153390290899
+CD,0.416833758452167
+CFx,0.03247125942305977
+CFy,-0.002873804790810271
+CFz,-5.465973653174358
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+CDPressure,0.23719167102360197
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+CFyPressure,-0.0028711593681925883
+CFzPressure,-5.456167064431193
+CMxPressure,0.008439043276920197
+CMyPressure,14.345627482188492
+CMzPressure,-0.01430413395859186
+CLSkinFriction,0.0028353507278436087
+CDSkinFriction,0.1796420874285655
+CFxSkinFriction,0.17939662651974422
+CFySkinFriction,-2.6454226174581312e-06
+CFzSkinFriction,-0.009806588743168677
+CMxSkinFriction,5.1477233961861325e-06
+CMySkinFriction,0.05553327658920275
+CMzSkinFriction,5.631797364280879e-05

case_759/results/alpha_-4.033162075344691/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
+L,-14296.854354768911
+D,1093.4392315192206
+Fx,85.1786791018417
+Fy,-7.538571044889182
+Fz,-14338.354103143312
+LPressure,-14304.292053031304
+DPressure,622.2017128599936
+FxPressure,-385.4149459617568
+FyPressure,-7.531631566462905
+FzPressure,-14312.629437993903
+LSkinFriction,7.437698262379451
+DSkinFriction,471.2375186592283
+FxSkinFriction,470.5936250635987
+FySkinFriction,-0.006939478425687348
+FzSkinFriction,-25.72466514941804
+Mx,22.150820395317965
+MxPressure,22.13731687600816
+MxSkinFriction,0.013503519329385582
+My,37777.156561252064
+MyPressure,37631.481548021555
+MySkinFriction,145.6750132305089
+Mz,-37.37490221343375
+MzPressure,-37.522635645705485
+MzSkinFriction,0.14773343226656893

case_759/results/alpha_-4.033162075344691/forces_summary.json

@@ -0,0 +1,64 @@
+{
+  "case_id": "case-0988c280-3386-4d14-b871-7917a6297114",
+  "case_name": "alpha_case",
+  "case_status": "Flow360Status.COMPLETED",
+  "reference": {
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+    "velocity_magnitude_m_s": 98.37842294401091,
+    "reference_area_m2": 1.0,
+    "reference_length_m": 1.0,
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+    "CMySkinFriction": 0.05553327658920275,
+    "CMzSkinFriction": 5.631797364280879e-05
+  },
+  "forces_N_and_moments_Nm": {
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+    "Fz": -14338.354103143312,
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+    "DPressure": 622.2017128599936,
+    "FxPressure": -385.4149459617568,
+    "FyPressure": -7.531631566462905,
+    "FzPressure": -14312.629437993903,
+    "LSkinFriction": 7.437698262379451,
+    "DSkinFriction": 471.2375186592283,
+    "FxSkinFriction": 470.5936250635987,
+    "FySkinFriction": -0.006939478425687348,
+    "FzSkinFriction": -25.72466514941804,
+    "Mx": 22.150820395317965,
+    "MxPressure": 22.13731687600816,
+    "MxSkinFriction": 0.013503519329385582,
+    "My": 37777.156561252064,
+    "MyPressure": 37631.481548021555,
+    "MySkinFriction": 145.6750132305089,
+    "Mz": -37.37490221343375,
+    "MzPressure": -37.522635645705485,
+    "MzSkinFriction": 0.14773343226656893
+  }
+}

case_759/results_10/alpha_-3.3909490722383806/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
+CL,-0.2147700451792219
+CD,0.01850543682023805
+CFx,0.005769672014461185
+CFy,-0.0001344234345199062
+CFz,-0.215488594554418
+CMx,0.0002847025676171505
+CMy,0.304149055458573
+CMz,-0.0003621880499766556
+CLPressure,-0.2148804240554117
+CDPressure,0.009922571483764553
+CFxPressure,-0.002804695069206164
+CFyPressure,-0.0001347673454407287
+CFzPressure,-0.2150911150016493
+CMxPressure,0.0002845032763972056
+CMyPressure,0.3027769794724136
+CMzPressure,-0.0003639149971884961
+CLSkinFriction,0.0001103788761897776
+CDSkinFriction,0.008582865336473518
+CFxSkinFriction,0.008574367083667357
+CFySkinFriction,3.439109208390897e-07
+CFzSkinFriction,-0.0003974795527687555
+CMxSkinFriction,1.992912202038187e-07
+CMySkinFriction,0.001372075986159153
+CMzSkinFriction,1.726947211887051e-06

case_759/results_10/alpha_-3.3909490722383806/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
+CL,-4.31803384019177
+CD,0.3720588797689996
+CFx,0.11600146093213706
+CFy,-0.002702634525626637
+CFz,-4.3324805499987935
+CMx,0.010457165942639405
+CMy,11.171438216547148
+CMz,-0.01330321876878888
+CLPressure,-4.320253049682705
+CDPressure,0.19949709193785828
+CFxPressure,-0.05638946627843278
+CFyPressure,-0.002709548986127326
+CFzPressure,-4.324489071679705
+CMxPressure,0.010449845947687069
+CMyPressure,11.121041669746507
+CMzPressure,-0.013366649786357642
+CLSkinFriction,0.0022192094909328085
+CDSkinFriction,0.1725617878311416
+CFxSkinFriction,0.17239092721057
+CFySkinFriction,6.9144605010232225e-06
+CFzSkinFriction,-0.00799147831909021
+CMxSkinFriction,7.319994961846918e-06
+CMySkinFriction,0.050396546800628654
+CMzSkinFriction,6.343101757046983e-05

case_759/results_10/alpha_-3.3909490722383806/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
+L,-20436.327154004364
+D,1760.8748029575352
+Fx,549.0100109651585
+Fy,-12.790988998122446
+Fz,-20504.700330047417
+LPressure,-20446.830196096784
+DPressure,944.176907361498
+FxPressure,-266.8792379947096
+FyPressure,-12.823713655250016
+FzPressure,-20466.878378803565
+LSkinFriction,10.503042092407545
+DSkinFriction,816.6978955960384
+FxSkinFriction,815.8892489598688
+FySkinFriction,0.03272465712915207
+FzSkinFriction,-37.821951243857626
+Mx,49.491521423092955
+MxPressure,49.45687745846739
+MxSkinFriction,0.03464396467057878
+My,52872.018752860284
+MyPressure,52633.502716171635
+MySkinFriction,238.5160366885867
+Mz,-62.96127844801388
+MzPressure,-63.2614838365592
+MzSkinFriction,0.3002053885534047