Add files using upload-large-folder tool

case_183/design_parameter_sample_183.json

@@ -0,0 +1,117 @@
+{
+    "inputs": [
+        {
+            "description": "",
+            "name": "Dihedral angle",
+            "type": "real",
+            "units": "deg",
+            "value": 7.842401423372058
+        },
+        {
+            "description": "",
+            "name": "Max Wing Blend",
+            "type": "real",
+            "units": "mm",
+            "value": 825.0829613063933
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 1",
+            "type": "real",
+            "units": "deg",
+            "value": 11.802200068444568
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 2",
+            "type": "real",
+            "units": "deg",
+            "value": 6.968343247179275
+        },
+        {
+            "description": "",
+            "name": "Wing Position",
+            "type": "real",
+            "value": 0.4025034828519125
+        },
+        {
+            "description": "",
+            "name": "Rear Point",
+            "type": "point",
+            "units": "mm",
+            "value": [
+                5670.774702661218,
+                0.0,
+                0.0
+            ]
+        },
+        {
+            "description": "",
+            "name": "Inlet Location",
+            "type": "real",
+            "value": 0.3075034650330421
+        },
+        {
+            "description": "",
+            "name": "NACA 4-digit code",
+            "type": "text",
+            "value": "2408"
+        },
+        {
+            "description": "",
+            "name": "Fore Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 4.8505420550723155
+        },
+        {
+            "description": "",
+            "name": "Aft Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 29.882281300013094
+        },
+        {
+            "description": "",
+            "name": "Top Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 212.5245659004878
+        },
+        {
+            "description": "",
+            "name": "Bottom Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 79.32147402510365
+        },
+        {
+            "description": "",
+            "name": "Wing span",
+            "type": "real",
+            "units": "mm",
+            "value": 16112.586420669319
+        },
+        {
+            "description": "",
+            "name": "Rear tail offset",
+            "type": "real",
+            "units": "mm",
+            "value": 1334.6575408615126
+        },
+        {
+            "description": "",
+            "name": "Root Chord",
+            "type": "real",
+            "units": "mm",
+            "value": 1677.3238332525345
+        },
+        {
+            "description": "",
+            "name": "Tail Root chord",
+            "type": "real",
+            "units": "mm",
+            "value": 802.0633209022207
+        }
+    ]
+}

case_183/param_2.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_183_2",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 140.7512136129031,
+  "alpha": 5.07677781789925,
+  "beta": 0,
+  "altitude_m": 5622.866532502374,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      5.07677781789925
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_183/params.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_183_1",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 46.14548206904425,
+  "alpha": -3.3888159616051423,
+  "beta": 0,
+  "altitude_m": 189.49775675395585,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      -3.3888159616051423
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_183/reference_area/input.json

@@ -0,0 +1,131 @@
+{
+    "description": "CCA Demo\n\nPresented in 7/17 webinar\n\nAntonsen 2025",
+    "inputs": [
+        {
+            "description": "",
+            "name": "Dihedral angle",
+            "type": "real",
+            "units": "deg",
+            "value": 7.842401423372058
+        },
+        {
+            "description": "",
+            "name": "Max Wing Blend",
+            "type": "real",
+            "units": "mm",
+            "value": 825.0829613063933
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 1",
+            "type": "real",
+            "units": "deg",
+            "value": 11.802200068444568
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 2",
+            "type": "real",
+            "units": "deg",
+            "value": 6.968343247179275
+        },
+        {
+            "description": "",
+            "name": "Wing Position",
+            "type": "real",
+            "value": 0.4025034828519125
+        },
+        {
+            "description": "",
+            "name": "Rear Point",
+            "type": "point",
+            "units": "mm",
+            "value": [
+                5670.774702661218,
+                0.0,
+                0.0
+            ]
+        },
+        {
+            "description": "",
+            "name": "Inlet Location",
+            "type": "real",
+            "value": 0.3075034650330421
+        },
+        {
+            "description": "",
+            "name": "NACA 4-digit code",
+            "type": "text",
+            "value": "2408"
+        },
+        {
+            "description": "",
+            "name": "Fore Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 4.8505420550723155
+        },
+        {
+            "description": "",
+            "name": "Aft Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 29.882281300013094
+        },
+        {
+            "description": "",
+            "name": "Top Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 212.5245659004878
+        },
+        {
+            "description": "",
+            "name": "Bottom Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 79.32147402510365
+        },
+        {
+            "description": "",
+            "name": "Wing span",
+            "type": "real",
+            "units": "mm",
+            "value": 16112.586420669319
+        },
+        {
+            "description": "",
+            "name": "Rear tail offset",
+            "type": "real",
+            "units": "mm",
+            "value": 1334.6575408615126
+        },
+        {
+            "description": "",
+            "name": "Root Chord",
+            "type": "real",
+            "units": "mm",
+            "value": 1677.3238332525345
+        },
+        {
+            "description": "",
+            "name": "Tail Root chord",
+            "type": "real",
+            "units": "mm",
+            "value": 802.0633209022207
+        },
+        {
+            "description": "",
+            "name": "File Path_0",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/CCA_Drone/cases/case_183/reference_area/../design_183.stl"
+        },
+        {
+            "description": "",
+            "name": "File Surface Reference",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/CCA_Drone/cases/case_183/reference_area/reference_area.txt"
+        }
+    ],
+    "title": "CCA_1_automated"
+}

case_183/reference_area/mac.txt

@@ -0,0 +1 @@
+1.304585203641

case_183/reference_area/reference_area.txt

@@ -0,0 +1 @@
+6738369.7633151077

case_183/reference_area/reference_area_m2.txt

@@ -0,0 +1 @@
+13.476739526630

case_183/results/alpha_-3.3888159616051423/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
+CL,-0.1583453476165537
+CD,0.02905142228213395
+CFx,0.01964058871714956
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+CLPressure,-0.1584766240286935
+CDPressure,0.01637411635876029
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+CLSkinFriction,0.0001312764121398641
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+CMxSkinFriction,-6.410694811301329e-07
+CMySkinFriction,0.004334703066074815
+CMzSkinFriction,-3.515653119489243e-06

case_183/results/alpha_-3.3888159616051423/force_coefficients.csv

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+,value
+CL,-2.133979005081977
+CD,0.39151845097445415
+CFx,0.26469109829069265
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+CLSkinFriction,0.001769178012399477
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+CMySkinFriction,0.07621082027715162
+CMzSkinFriction,-6.181064861008355e-05

case_183/results/alpha_-3.3888159616051423/forces_actual.csv

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+,value_SI
+L,-2732.9821410564373
+D,501.4168048790896
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+Fz,-2757.842716962419
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+My,6999.419062690949
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+Mz,13.917360272371194
+MzPressure,13.996521031858165
+MzSkinFriction,-0.07916075949021995

case_183/results/alpha_-3.3888159616051423/forces_summary.json

@@ -0,0 +1,64 @@
+{
+  "case_id": "case-3fc4f317-e079-425b-89cc-a9a1716e90f1",
+  "case_name": "alpha_case",
+  "case_status": "Flow360Status.COMPLETED",
+  "reference": {
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+    "CMzSkinFriction": -6.181064861008355e-05
+  },
+  "forces_N_and_moments_Nm": {
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+    "MzSkinFriction": -0.07916075949021995
+  }
+}

case_183/results_2/alpha_5.07677781789925/force_coefficents_corected.csv

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+,value
+CL,0.8193695871324551
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+CFySkinFriction,-6.314879703032292e-07
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+CMxSkinFriction,7.165730990066308e-07
+CMySkinFriction,0.002280496922684594
+CMzSkinFriction,-5.519410901640036e-06

case_183/results_2/alpha_5.07677781789925/force_coefficients.csv

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+,value
+CL,11.042430501826463
+CD,0.5218694962806895
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+CMySkinFriction,0.040094682027364784
+CMzSkinFriction,-9.703982622310032e-05

case_183/results_2/alpha_5.07677781789925/forces_actual.csv

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+,value_SI
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+MzSkinFriction,-0.6614580712647786

case_183/results_2/alpha_5.07677781789925/forces_summary.json

@@ -0,0 +1,64 @@
+{
+  "case_id": "case-03e62a98-822a-4eb7-9de8-f5f05ae9509c",
+  "case_name": "alpha_case",
+  "case_status": "Flow360Status.COMPLETED",
+  "reference": {
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+    "reference_area_m2": 1.0,
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+  },
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+    "CMySkinFriction": 0.040094682027364784,
+    "CMzSkinFriction": -9.703982622310032e-05
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+    "D": 3557.248646222048,
+    "Fx": -3117.317518794976,
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+    "MzPressure": 45.78662477070918,
+    "MzSkinFriction": -0.6614580712647786
+  }
+}

case_29/design_parameter_sample_29.json

@@ -0,0 +1,117 @@
+{
+    "inputs": [
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+            "description": "",
+            "name": "Dihedral angle",
+            "type": "real",
+            "units": "deg",
+            "value": 0.868507904622298
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+            "description": "",
+            "name": "Max Wing Blend",
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+            "units": "mm",
+            "value": 886.8593998042256
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+            "name": "Inlet Angle 1",
+            "type": "real",
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+            "value": 2.902432035147105
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+        {
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+            "name": "Inlet Angle 2",
+            "type": "real",
+            "units": "deg",
+            "value": 8.89084937290557
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+        {
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+            "name": "Wing Position",
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+            "value": 0.46885576552169095
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+            "name": "Rear Point",
+            "type": "point",
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+            "value": [
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+                0.0
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+        {
+            "description": "",
+            "name": "Inlet Location",
+            "type": "real",
+            "value": 0.4989126382676745
+        },
+        {
+            "description": "",
+            "name": "NACA 4-digit code",
+            "type": "text",
+            "value": "0012"
+        },
+        {
+            "description": "",
+            "name": "Fore Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 7.190884596360217
+        },
+        {
+            "description": "",
+            "name": "Aft Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 25.446680883145728
+        },
+        {
+            "description": "",
+            "name": "Top Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 44.692726796585845
+        },
+        {
+            "description": "",
+            "name": "Bottom Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 178.77643873382073
+        },
+        {
+            "description": "",
+            "name": "Wing span",
+            "type": "real",
+            "units": "mm",
+            "value": 17075.089078467954
+        },
+        {
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+            "name": "Rear tail offset",
+            "type": "real",
+            "units": "mm",
+            "value": 1016.7374063581833
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+        {
+            "description": "",
+            "name": "Root Chord",
+            "type": "real",
+            "units": "mm",
+            "value": 2334.9279463667585
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+        {
+            "description": "",
+            "name": "Tail Root chord",
+            "type": "real",
+            "units": "mm",
+            "value": 1118.4511588040095
+        }
+    ]
+}

case_29/param_10.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_29_10",
+  "max_steps": 3500,
+  "volume_mesh_params": {
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+    "boundary_layer_first_layer_thickness": 1.78684e-05
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+    "values": [
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+    "unit": "fl.u.deg"
+  }
+}

case_29/param_2.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_29_2",
+  "max_steps": 3500,
+  "volume_mesh_params": {
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+    "unit": "fl.u.deg"
+  }
+}

case_29/param_3.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_29_3",
+  "max_steps": 3500,
+  "volume_mesh_params": {
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+    "values": [
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+    "unit": "fl.u.deg"
+  }
+}

case_29/param_4.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_29_4",
+  "max_steps": 3500,
+  "volume_mesh_params": {
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+    "boundary_layer_first_layer_thickness": 1.78684e-05
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+    "values": [
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+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_29/param_5.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_29_5",
+  "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": 170.09199464376138,
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+    "values": [
+      -6.885595817041925
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+    "unit": "fl.u.deg"
+  }
+}

case_29/param_6.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_29_6",
+  "max_steps": 3500,
+  "volume_mesh_params": {
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+    "boundary_layer_first_layer_thickness": 1.78684e-05
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+    "unit": "fl.u.deg"
+  }
+}

case_29/param_7.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_29_7",
+  "max_steps": 3500,
+  "volume_mesh_params": {
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+    "unit": "fl.u.deg"
+  }
+}

case_29/param_8.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_29_8",
+  "max_steps": 3500,
+  "volume_mesh_params": {
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+    "unit": "fl.u.deg"
+  }
+}

case_29/param_9.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_29_9",
+  "max_steps": 3500,
+  "volume_mesh_params": {
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+      -7.302822020862866
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+    "unit": "fl.u.deg"
+  }
+}

case_29/params.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_29_1",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
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+    "values": [
+      4.575032369325799
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+    "unit": "fl.u.deg"
+  }
+}

case_29/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": 0.868507904622298
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+        {
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+            "name": "Max Wing Blend",
+            "type": "real",
+            "units": "mm",
+            "value": 886.8593998042256
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+            "name": "Inlet Angle 1",
+            "type": "real",
+            "units": "deg",
+            "value": 2.902432035147105
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+            "name": "Inlet Angle 2",
+            "type": "real",
+            "units": "deg",
+            "value": 8.89084937290557
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+        {
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+            "name": "Wing Position",
+            "type": "real",
+            "value": 0.46885576552169095
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+            "name": "Rear Point",
+            "type": "point",
+            "units": "mm",
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+            "type": "real",
+            "value": 0.4989126382676745
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+        {
+            "description": "",
+            "name": "NACA 4-digit code",
+            "type": "text",
+            "value": "0012"
+        },
+        {
+            "description": "",
+            "name": "Fore Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 7.190884596360217
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+        {
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+            "name": "Aft Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 25.446680883145728
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+        {
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+            "name": "Top Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 44.692726796585845
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+        {
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+            "name": "Bottom Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 178.77643873382073
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+        {
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+            "name": "Wing span",
+            "type": "real",
+            "units": "mm",
+            "value": 17075.089078467954
+        },
+        {
+            "description": "",
+            "name": "Rear tail offset",
+            "type": "real",
+            "units": "mm",
+            "value": 1016.7374063581833
+        },
+        {
+            "description": "",
+            "name": "Root Chord",
+            "type": "real",
+            "units": "mm",
+            "value": 2334.9279463667585
+        },
+        {
+            "description": "",
+            "name": "Tail Root chord",
+            "type": "real",
+            "units": "mm",
+            "value": 1118.4511588040095
+        },
+        {
+            "description": "",
+            "name": "File Path_0",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/CCA_Drone/cases/case_29/reference_area/../design_29.stl"
+        },
+        {
+            "description": "",
+            "name": "File Surface Reference",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/CCA_Drone/cases/case_29/reference_area/reference_area.txt"
+        }
+    ],
+    "title": "CCA_1_automated"
+}

case_29/reference_area/mac.txt

@@ -0,0 +1 @@
+1.816055069396

case_29/reference_area/reference_area.txt

@@ -0,0 +1 @@
+13254849.59371659

case_29/reference_area/reference_area_m2.txt

@@ -0,0 +1 @@
+26.509699187433

case_29/results/alpha_4.575032369325799/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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+CMzSkinFriction,8.048013576535205e-08

case_29/results/alpha_4.575032369325799/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
+CL,9.705534022679245
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case_29/results/alpha_4.575032369325799/forces_actual.csv

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+,value_SI
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+MzSkinFriction,0.0021979408642627727

case_29/results/alpha_4.575032369325799/forces_summary.json

@@ -0,0 +1,64 @@
+{
+  "case_id": "case-45676921-8b3e-4bf0-8421-764952b2b878",
+  "case_name": "alpha_case",
+  "case_status": "Flow360Status.COMPLETED",
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+    "MzSkinFriction": 0.0021979408642627727
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+}

case_29/results_10/alpha_6.369208882879626/force_coefficents_corected.csv

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+CMzSkinFriction,-1.271161103237159e-06

case_29/results_10/alpha_6.369208882879626/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_29/results_10/alpha_6.369208882879626/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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case_29/results_10/alpha_6.369208882879626/forces_summary.json

@@ -0,0 +1,64 @@
+{
+  "case_id": "case-072a7525-ff21-4934-ad1e-1fb6217edd8c",
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+}

case_29/results_2/alpha_0.466613390266442/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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case_29/results_2/alpha_0.466613390266442/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_29/results_2/alpha_0.466613390266442/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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case_29/results_2/alpha_0.466613390266442/forces_summary.json

@@ -0,0 +1,64 @@
+{
+  "case_id": "case-04a747e1-027c-442e-8e92-9fa9aa761247",
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+}

case_29/results_3/alpha_-2.6071453444853114/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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case_29/results_3/alpha_-2.6071453444853114/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_29/results_3/alpha_-2.6071453444853114/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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+MzSkinFriction,-1.428866213621475

case_29/results_3/alpha_-2.6071453444853114/forces_summary.json

@@ -0,0 +1,64 @@
+{
+  "case_id": "case-66739009-7b23-4782-a252-560acd8dfb39",
+  "case_name": "alpha_case",
+  "case_status": "Flow360Status.COMPLETED",
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+}

case_29/results_4/alpha_-5.143739079628112/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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case_29/results_4/alpha_-5.143739079628112/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_29/results_4/alpha_-5.143739079628112/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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+FxPressure,-3419.7440741347727
+FyPressure,3.430272360993393
+FzPressure,-60219.7611211585
+LSkinFriction,15.970354697299442
+DSkinFriction,1103.0529596372407
+FxSkinFriction,1100.042686996429
+FySkinFriction,0.34005627824203083
+FzSkinFriction,-82.98777487866404
+Mx,-11.369683751314463
+MxPressure,-11.419802987588257
+MxSkinFriction,0.05011923632507225
+My,224265.10231582553
+MyPressure,223844.91179565503
+MySkinFriction,420.19052017051575
+Mz,22.273646673075195
+MzPressure,20.744481445450965
+MzSkinFriction,1.5291652276174221

case_29/results_4/alpha_-5.143739079628112/forces_summary.json

@@ -0,0 +1,64 @@
+{
+  "case_id": "case-52530d8a-d749-44ae-8e1b-3dd01e86a26d",
+  "case_name": "alpha_case",
+  "case_status": "Flow360Status.COMPLETED",
+  "reference": {
+    "density_kg_m3": 0.5985834563127778,
+    "velocity_magnitude_m_s": 136.34507363901292,
+    "reference_area_m2": 1.0,
+    "reference_length_m": 1.0,
+    "dynamic_pressure_Pa": 5563.826972914521
+  },
+  "force_coefficients": {
+    "CL": -10.832090363466309,
+    "CD": 0.5564625725228595,
+    "CFx": -0.416925508005725,
+    "CFy": 0.0006776502320413085,
+    "CFz": -10.838358056352094,
+    "CMx": -0.002043500598897783,
+    "CMy": 40.30770608208685,
+    "CMz": 0.004003296073279487,
+    "CLPressure": -10.834960753716581,
+    "CDPressure": 0.35820821180908125,
+    "CFxPressure": -0.6146388251796038,
+    "CFyPressure": 0.0006165310994918485,
+    "CFzPressure": -10.823442464029997,
+    "CMxPressure": -0.0020525086497444,
+    "CMyPressure": 40.232184229553326,
+    "CMzPressure": 0.0037284555300583517,
+    "CLSkinFriction": 0.0028703902502801282,
+    "CDSkinFriction": 0.19825436071377758,
+    "CFxSkinFriction": 0.19771331717387847,
+    "CFySkinFriction": 6.111913254985675e-05,
+    "CFzSkinFriction": -0.014915592322094127,
+    "CMxSkinFriction": 9.008050855833515e-06,
+    "CMySkinFriction": 0.07552185253352796,
+    "CMzSkinFriction": 0.00027484054321991137
+  },
+  "forces_N_and_moments_Nm": {
+    "L": -60267.87653730131,
+    "D": 3096.0614704200884,
+    "Fx": -2319.701387138342,
+    "Fy": 3.7703286392332163,
+    "Fz": -60302.748896037185,
+    "LPressure": -60283.84689199857,
+    "DPressure": 1993.0085107828443,
+    "FxPressure": -3419.7440741347727,
+    "FyPressure": 3.430272360993393,
+    "FzPressure": -60219.7611211585,
+    "LSkinFriction": 15.970354697299442,
+    "DSkinFriction": 1103.0529596372407,
+    "FxSkinFriction": 1100.042686996429,
+    "FySkinFriction": 0.34005627824203083,
+    "FzSkinFriction": -82.98777487866404,
+    "Mx": -11.369683751314463,
+    "MxPressure": -11.419802987588257,
+    "MxSkinFriction": 0.05011923632507225,
+    "My": 224265.10231582553,
+    "MyPressure": 223844.91179565503,
+    "MySkinFriction": 420.19052017051575,
+    "Mz": 22.273646673075195,
+    "MzPressure": 20.744481445450965,
+    "MzSkinFriction": 1.5291652276174221
+  }
+}