Add files using upload-large-folder tool

case_1593/results_10/alpha_7.1020711400188326/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
+CL,10.611147270489859
+CD,0.7460747189566785
+CFx,-0.571583666679896
+CFy,0.0011643757719302715
+CFz,10.62197561634724
+CMx,0.0013279531828609198
+CMy,-33.29226359136965
+CMz,0.005191754514257066
+CLPressure,10.625315341950808
+CDPressure,0.5621405459004092
+CFxPressure,-0.7558583019173694
+CFyPressure,0.0011295858305846803
+CFzPressure,10.613293849539021
+CMxPressure,0.001302071598763494
+CMyPressure,-33.32188523939549
+CMzPressure,0.005167057545388103
+CLSkinFriction,-0.014168071460950008
+CDSkinFriction,0.18393417305626925
+CFxSkinFriction,0.18427463523747373
+CFySkinFriction,3.478994134585417e-05
+CFzSkinFriction,0.008681766808213393
+CMxSkinFriction,2.588158409509522e-05
+CMySkinFriction,0.029621648025836014
+CMzSkinFriction,2.469696886961303e-05

case_1593/results_7/alpha_1.7716551457363359/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
+CL,0.255120078188002
+CD,0.02584804274901675
+CFx,0.0179483209014937
+CFy,7.813699563480943e-05
+CFz,0.2557972505431291
+CMx,-3.152775759889882e-05
+CMy,-0.4396541688584913
+CMz,0.0002163942469710278
+CLPressure,0.2554950932548828
+CDPressure,0.01359679433703793
+CFxPressure,0.005691334790360899
+CFyPressure,7.794340442307016e-05
+CFzPressure,0.2557933232159686
+CMxPressure,-3.368227829672473e-05
+CMyPressure,-0.4415649420100969
+CMzPressure,0.0002199745147498474
+CLSkinFriction,-0.0003750150668806168
+CDSkinFriction,0.01225124841197881
+CFxSkinFriction,0.01225698611113279
+CFySkinFriction,1.935912117380399e-07
+CFzSkinFriction,3.927327160450699e-06
+CMxSkinFriction,2.154520697754748e-06
+CMySkinFriction,0.001910773151605504
+CMzSkinFriction,-3.580267778660516e-06

case_1593/results_7/alpha_1.7716551457363359/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
+CL,3.7479648382687514
+CD,0.3797331674145683
+CFx,0.2636784847454868
+CFy,0.0011479093072063711
+CFz,3.7579131661090766
+CMx,-0.0008708147534778858
+CMy,-12.143500389111212
+CMz,0.005976933254418639
+CLPressure,3.7534741783978114
+CDPressure,0.19975028014391075
+CFxPressure,0.08361130503170044
+CFyPressure,0.0011450652619248312
+CFzPressure,3.757855469810885
+CMxPressure,-0.0009303238512770201
+CMyPressure,-12.196277039837103
+CMzPressure,0.006075822304596648
+CLSkinFriction,-0.005509340129057929
+CDSkinFriction,0.17998288727065734
+CFxSkinFriction,0.18006717971378614
+CFySkinFriction,2.8440452815216207e-06
+CFzSkinFriction,5.769629819139541e-05
+CMxSkinFriction,5.950909779716885e-05
+CMySkinFriction,0.0527766507258869
+CMzSkinFriction,-9.888905017361493e-05

case_1593/results_7/alpha_1.7716551457363359/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
+L,3401.380022988046
+D,344.6181769161174
+Fx,239.29539609003825
+Fy,1.041758915629887
+Fz,3410.408401064786
+LPressure,3406.379898991015
+DPressure,181.2788117781816
+FxPressure,75.87953326748715
+FyPressure,1.0391778671882554
+FzPressure,3410.3560401050286
+LSkinFriction,-4.999876002967
+DSkinFriction,163.3393651379356
+FxSkinFriction,163.41586282255093
+FySkinFriction,0.002581048441614914
+FzSkinFriction,0.052360959757355545
+Mx,-0.790288072065032
+MxPressure,-0.8442941967685699
+MxSkinFriction,0.054006124701754164
+My,-11020.556866203091
+MyPressure,-11068.453112087345
+MySkinFriction,47.89624588425156
+Mz,5.424229481219781
+MzPressure,5.513973983711728
+MzSkinFriction,-0.08974450248795995

case_1593/results_7/alpha_1.7716551457363359/forces_summary.json

@@ -0,0 +1,64 @@
+{
+  "case_id": "case-5c9e6e9c-bba4-4c28-b09c-27e1dce609a5",
+  "case_name": "alpha_case",
+  "case_status": "Flow360Status.COMPLETED",
+  "reference": {
+    "density_kg_m3": 0.9248920467058871,
+    "velocity_magnitude_m_s": 44.299548485686095,
+    "reference_area_m2": 1.0,
+    "reference_length_m": 1.0,
+    "dynamic_pressure_Pa": 907.5271966956876
+  },
+  "force_coefficients": {
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+    "CD": 0.3797331674145683,
+    "CFx": 0.2636784847454868,
+    "CFy": 0.0011479093072063711,
+    "CFz": 3.7579131661090766,
+    "CMx": -0.0008708147534778858,
+    "CMy": -12.143500389111212,
+    "CMz": 0.005976933254418639,
+    "CLPressure": 3.7534741783978114,
+    "CDPressure": 0.19975028014391075,
+    "CFxPressure": 0.08361130503170044,
+    "CFyPressure": 0.0011450652619248312,
+    "CFzPressure": 3.757855469810885,
+    "CMxPressure": -0.0009303238512770201,
+    "CMyPressure": -12.196277039837103,
+    "CMzPressure": 0.006075822304596648,
+    "CLSkinFriction": -0.005509340129057929,
+    "CDSkinFriction": 0.17998288727065734,
+    "CFxSkinFriction": 0.18006717971378614,
+    "CFySkinFriction": 2.8440452815216207e-06,
+    "CFzSkinFriction": 5.769629819139541e-05,
+    "CMxSkinFriction": 5.950909779716885e-05,
+    "CMySkinFriction": 0.0527766507258869,
+    "CMzSkinFriction": -9.888905017361493e-05
+  },
+  "forces_N_and_moments_Nm": {
+    "L": 3401.380022988046,
+    "D": 344.6181769161174,
+    "Fx": 239.29539609003825,
+    "Fy": 1.041758915629887,
+    "Fz": 3410.408401064786,
+    "LPressure": 3406.379898991015,
+    "DPressure": 181.2788117781816,
+    "FxPressure": 75.87953326748715,
+    "FyPressure": 1.0391778671882554,
+    "FzPressure": 3410.3560401050286,
+    "LSkinFriction": -4.999876002967,
+    "DSkinFriction": 163.3393651379356,
+    "FxSkinFriction": 163.41586282255093,
+    "FySkinFriction": 0.002581048441614914,
+    "FzSkinFriction": 0.052360959757355545,
+    "Mx": -0.790288072065032,
+    "MxPressure": -0.8442941967685699,
+    "MxSkinFriction": 0.054006124701754164,
+    "My": -11020.556866203091,
+    "MyPressure": -11068.453112087345,
+    "MySkinFriction": 47.89624588425156,
+    "Mz": 5.424229481219781,
+    "MzPressure": 5.513973983711728,
+    "MzSkinFriction": -0.08974450248795995
+  }
+}

case_1599/design_parameter_sample_1599.json

@@ -0,0 +1,117 @@
+{
+    "inputs": [
+        {
+            "description": "",
+            "name": "Dihedral angle",
+            "type": "real",
+            "units": "deg",
+            "value": 5.337102947259212
+        },
+        {
+            "description": "",
+            "name": "Max Wing Blend",
+            "type": "real",
+            "units": "mm",
+            "value": 90.06063175736271
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 1",
+            "type": "real",
+            "units": "deg",
+            "value": 21.46161317266447
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 2",
+            "type": "real",
+            "units": "deg",
+            "value": 6.314614762160802
+        },
+        {
+            "description": "",
+            "name": "Wing Position",
+            "type": "real",
+            "value": 0.3677306802354
+        },
+        {
+            "description": "",
+            "name": "Rear Point",
+            "type": "point",
+            "units": "mm",
+            "value": [
+                7326.296841523287,
+                0.0,
+                0.0
+            ]
+        },
+        {
+            "description": "",
+            "name": "Inlet Location",
+            "type": "real",
+            "value": 0.3473791090662582
+        },
+        {
+            "description": "",
+            "name": "NACA 4-digit code",
+            "type": "text",
+            "value": "2408"
+        },
+        {
+            "description": "",
+            "name": "Fore Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 4.0339001038977305
+        },
+        {
+            "description": "",
+            "name": "Aft Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 23.50353257564185
+        },
+        {
+            "description": "",
+            "name": "Top Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 178.84972799509808
+        },
+        {
+            "description": "",
+            "name": "Bottom Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 76.97846077960696
+        },
+        {
+            "description": "",
+            "name": "Wing span",
+            "type": "real",
+            "units": "mm",
+            "value": 12964.899311329755
+        },
+        {
+            "description": "",
+            "name": "Rear tail offset",
+            "type": "real",
+            "units": "mm",
+            "value": 1187.074944071611
+        },
+        {
+            "description": "",
+            "name": "Root Chord",
+            "type": "real",
+            "units": "mm",
+            "value": 2463.412692435585
+        },
+        {
+            "description": "",
+            "name": "Tail Root chord",
+            "type": "real",
+            "units": "mm",
+            "value": 941.1409401190292
+        }
+    ]
+}

case_1599/param_2.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1599_2",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 104.72282988916623,
+  "alpha": 5.251837228122675,
+  "beta": 0,
+  "altitude_m": 413.7077282728259,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      5.251837228122675
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_1599/params.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_1599_1",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 161.75129447753417,
+  "alpha": 7.972944104555976,
+  "beta": 0,
+  "altitude_m": 5394.139994116223,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      7.972944104555976
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_1599/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": 5.337102947259212
+        },
+        {
+            "description": "",
+            "name": "Max Wing Blend",
+            "type": "real",
+            "units": "mm",
+            "value": 90.06063175736271
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 1",
+            "type": "real",
+            "units": "deg",
+            "value": 21.46161317266447
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 2",
+            "type": "real",
+            "units": "deg",
+            "value": 6.314614762160802
+        },
+        {
+            "description": "",
+            "name": "Wing Position",
+            "type": "real",
+            "value": 0.3677306802354
+        },
+        {
+            "description": "",
+            "name": "Rear Point",
+            "type": "point",
+            "units": "mm",
+            "value": [
+                7326.296841523287,
+                0.0,
+                0.0
+            ]
+        },
+        {
+            "description": "",
+            "name": "Inlet Location",
+            "type": "real",
+            "value": 0.3473791090662582
+        },
+        {
+            "description": "",
+            "name": "NACA 4-digit code",
+            "type": "text",
+            "value": "2408"
+        },
+        {
+            "description": "",
+            "name": "Fore Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 4.0339001038977305
+        },
+        {
+            "description": "",
+            "name": "Aft Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 23.50353257564185
+        },
+        {
+            "description": "",
+            "name": "Top Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 178.84972799509808
+        },
+        {
+            "description": "",
+            "name": "Bottom Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 76.97846077960696
+        },
+        {
+            "description": "",
+            "name": "Wing span",
+            "type": "real",
+            "units": "mm",
+            "value": 12964.899311329755
+        },
+        {
+            "description": "",
+            "name": "Rear tail offset",
+            "type": "real",
+            "units": "mm",
+            "value": 1187.074944071611
+        },
+        {
+            "description": "",
+            "name": "Root Chord",
+            "type": "real",
+            "units": "mm",
+            "value": 2463.412692435585
+        },
+        {
+            "description": "",
+            "name": "Tail Root chord",
+            "type": "real",
+            "units": "mm",
+            "value": 941.1409401190292
+        },
+        {
+            "description": "",
+            "name": "File Path_0",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/CCA_Drone/cases/case_1599/reference_area/../design_1599.stl"
+        },
+        {
+            "description": "",
+            "name": "File Surface Reference",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/CCA_Drone/cases/case_1599/reference_area/reference_area.txt"
+        }
+    ],
+    "title": "CCA_1_automated"
+}

case_1599/reference_area/mac.txt

@@ -0,0 +1 @@
+1.915987649672

case_1599/reference_area/reference_area.txt

@@ -0,0 +1 @@
+8225938.6721550049

case_1599/reference_area/reference_area_m2.txt

@@ -0,0 +1 @@
+16.451877344310

case_1599/results/alpha_7.972944104555976/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
+CL,16.62503624919447
+CD,1.126532880208723
+CFx,-1.1903399590375432
+CFy,-0.0008304572901435
+CFz,16.620589562321186
+CMx,-0.02007439287015504
+CMy,-64.73104661725264
+CMz,-0.003554933459694557
+CLPressure,16.64399844068979
+CDPressure,0.9565057502735844
+CFxPressure,-1.3613537115842027
+CFyPressure,-0.0008351494914278914
+CFzPressure,16.615784766779658
+CMxPressure,-0.020088964680416436
+CMyPressure,-64.7527944713657
+CMzPressure,-0.0034780910144540348
+CLSkinFriction,-0.01896219149533247
+CDSkinFriction,0.1700271299351384
+CFxSkinFriction,0.17101375254665982
+CFySkinFriction,4.692201283560201e-06
+CFzSkinFriction,0.00480479554152945
+CMxSkinFriction,1.4571810275665088e-05
+CMySkinFriction,0.021747854113057977
+CMzSkinFriction,-7.6842445248144e-05

case_818/design_parameter_sample_818.json

@@ -0,0 +1,117 @@
+{
+    "inputs": [
+        {
+            "description": "",
+            "name": "Dihedral angle",
+            "type": "real",
+            "units": "deg",
+            "value": 13.963225769896468
+        },
+        {
+            "description": "",
+            "name": "Max Wing Blend",
+            "type": "real",
+            "units": "mm",
+            "value": 806.5677520089465
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 1",
+            "type": "real",
+            "units": "deg",
+            "value": 33.71582446186481
+        },
+        {
+            "description": "",
+            "name": "Inlet Angle 2",
+            "type": "real",
+            "units": "deg",
+            "value": 8.419539684039265
+        },
+        {
+            "description": "",
+            "name": "Wing Position",
+            "type": "real",
+            "value": 0.22582556397350642
+        },
+        {
+            "description": "",
+            "name": "Rear Point",
+            "type": "point",
+            "units": "mm",
+            "value": [
+                5989.554550832743,
+                0.0,
+                0.0
+            ]
+        },
+        {
+            "description": "",
+            "name": "Inlet Location",
+            "type": "real",
+            "value": 0.418140848661514
+        },
+        {
+            "description": "",
+            "name": "NACA 4-digit code",
+            "type": "text",
+            "value": "2408"
+        },
+        {
+            "description": "",
+            "name": "Fore Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 0.28111891805917366
+        },
+        {
+            "description": "",
+            "name": "Aft Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 32.14786884032667
+        },
+        {
+            "description": "",
+            "name": "Top Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 53.133059969526805
+        },
+        {
+            "description": "",
+            "name": "Bottom Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 112.91104256161812
+        },
+        {
+            "description": "",
+            "name": "Wing span",
+            "type": "real",
+            "units": "mm",
+            "value": 11445.722028829421
+        },
+        {
+            "description": "",
+            "name": "Rear tail offset",
+            "type": "real",
+            "units": "mm",
+            "value": 1183.1399659210317
+        },
+        {
+            "description": "",
+            "name": "Root Chord",
+            "type": "real",
+            "units": "mm",
+            "value": 1865.304192835601
+        },
+        {
+            "description": "",
+            "name": "Tail Root chord",
+            "type": "real",
+            "units": "mm",
+            "value": 1032.049560602301
+        }
+    ]
+}

case_818/param_10.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_818_10",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 87.11281373195843,
+  "alpha": -5.1690216019160005,
+  "beta": 0,
+  "altitude_m": 9034.149394779666,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      -5.1690216019160005
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_818/param_2.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_818_2",
+  "max_steps": 3500,
+  "volume_mesh_params": {
+    "boundary_layer_growth_rate": 1.2,
+    "boundary_layer_first_layer_thickness": 1.78684e-05
+  },
+  "velocity_magnitude": 135.95167291665425,
+  "alpha": -1.9372327240715963,
+  "beta": 0,
+  "altitude_m": 8149.581811737836,
+  "sweep_schema": {
+    "variable": "alpha",
+    "values": [
+      -1.9372327240715963
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_818/param_3.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_818_3",
+  "max_steps": 3500,
+  "volume_mesh_params": {
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+    "boundary_layer_first_layer_thickness": 1.78684e-05
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+  "velocity_magnitude": 141.10666331474934,
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+    "values": [
+      4.106757888009488
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+    "unit": "fl.u.deg"
+  }
+}

case_818/param_5.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_818_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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+    "values": [
+      -5.3248985594344616
+    ],
+    "unit": "fl.u.deg"
+  }
+}

case_818/param_6.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_818_6",
+  "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": 109.86496602250162,
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+      -3.005635423591282
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+    "unit": "fl.u.deg"
+  }
+}

case_818/param_7.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_818_7",
+  "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": 29.6038005684161,
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+    "values": [
+      2.1374796078254725
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+    "unit": "fl.u.deg"
+  }
+}

case_818/param_8.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_818_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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+    "unit": "fl.u.deg"
+  }
+}

case_818/param_9.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_818_9",
+  "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": [
+      -1.240827393620778
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+    "unit": "fl.u.deg"
+  }
+}

case_818/params.json

@@ -0,0 +1,19 @@
+{
+  "job_name": "CCA_generation_818_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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+      9.420774954024775
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+    "unit": "fl.u.deg"
+  }
+}

case_818/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": 13.963225769896468
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+        {
+            "description": "",
+            "name": "Max Wing Blend",
+            "type": "real",
+            "units": "mm",
+            "value": 806.5677520089465
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+            "name": "Inlet Angle 1",
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+        {
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+            "name": "Inlet Angle 2",
+            "type": "real",
+            "units": "deg",
+            "value": 8.419539684039265
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+        {
+            "description": "",
+            "name": "Wing Position",
+            "type": "real",
+            "value": 0.22582556397350642
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+        {
+            "description": "",
+            "name": "Rear Point",
+            "type": "point",
+            "units": "mm",
+            "value": [
+                5989.554550832743,
+                0.0,
+                0.0
+            ]
+        },
+        {
+            "description": "",
+            "name": "Inlet Location",
+            "type": "real",
+            "value": 0.418140848661514
+        },
+        {
+            "description": "",
+            "name": "NACA 4-digit code",
+            "type": "text",
+            "value": "2408"
+        },
+        {
+            "description": "",
+            "name": "Fore Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 0.28111891805917366
+        },
+        {
+            "description": "",
+            "name": "Aft Top Angle",
+            "type": "real",
+            "units": "deg",
+            "value": 32.14786884032667
+        },
+        {
+            "description": "",
+            "name": "Top Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 53.133059969526805
+        },
+        {
+            "description": "",
+            "name": "Bottom Height Aft",
+            "type": "real",
+            "units": "mm",
+            "value": 112.91104256161812
+        },
+        {
+            "description": "",
+            "name": "Wing span",
+            "type": "real",
+            "units": "mm",
+            "value": 11445.722028829421
+        },
+        {
+            "description": "",
+            "name": "Rear tail offset",
+            "type": "real",
+            "units": "mm",
+            "value": 1183.1399659210317
+        },
+        {
+            "description": "",
+            "name": "Root Chord",
+            "type": "real",
+            "units": "mm",
+            "value": 1865.304192835601
+        },
+        {
+            "description": "",
+            "name": "Tail Root chord",
+            "type": "real",
+            "units": "mm",
+            "value": 1032.049560602301
+        },
+        {
+            "description": "",
+            "name": "File Path_0",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/CCA_Drone/cases/case_818/reference_area/../design_818.stl"
+        },
+        {
+            "description": "",
+            "name": "File Surface Reference",
+            "type": "file_path",
+            "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/CCA_Drone/cases/case_818/reference_area/reference_area.txt"
+        }
+    ],
+    "title": "CCA_1_automated"
+}

case_818/reference_area/mac.txt

@@ -0,0 +1 @@
+1.450792149983

case_818/reference_area/reference_area.txt

@@ -0,0 +1 @@
+5311549.8339171372

case_818/reference_area/reference_area_m2.txt

@@ -0,0 +1 @@
+10.623099667834

case_818/results/alpha_9.420774954024775/force_coefficents_corected.csv

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case_818/results/alpha_9.420774954024775/force_coefficients.csv

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case_818/results/alpha_9.420774954024775/forces_actual.csv

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case_818/results/alpha_9.420774954024775/forces_summary.json

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

case_818/results_10/alpha_-5.1690216019160005/force_coefficents_corected.csv

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case_818/results_10/alpha_-5.1690216019160005/force_coefficients.csv

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case_818/results_10/alpha_-5.1690216019160005/forces_actual.csv

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case_818/results_10/alpha_-5.1690216019160005/forces_summary.json

@@ -0,0 +1,64 @@
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+    "MzSkinFriction": 0.22557449885482458
+  }
+}

case_818/results_2/alpha_-1.9372327240715963/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
+CL,0.002502427758219115
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+CFySkinFriction,2.889169671979869e-07
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+CMxSkinFriction,1.627160330514796e-06
+CMySkinFriction,0.004549107643313928
+CMzSkinFriction,2.030668549724677e-06

case_818/results_2/alpha_-1.9372327240715963/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
+CL,0.02658353948711606
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case_818/results_2/alpha_-1.9372327240715963/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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+MzSkinFriction,0.14943060380238032

case_818/results_2/alpha_-1.9372327240715963/forces_summary.json

@@ -0,0 +1,64 @@
+{
+  "case_id": "case-cb57f228-ff19-41e9-ba7f-d1f7d5941e69",
+  "case_name": "alpha_case",
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+    "MzSkinFriction": 0.14943060380238032
+  }
+}

case_818/results_3/alpha_4.106757888009488/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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+CMzSkinFriction,-8.188632269261171e-07

case_818/results_3/alpha_4.106757888009488/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_818/results_3/alpha_4.106757888009488/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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case_818/results_3/alpha_4.106757888009488/forces_summary.json

@@ -0,0 +1,64 @@
+{
+  "case_id": "case-32c77fac-7027-4232-bfb0-30953793bc41",
+  "case_name": "alpha_case",
+  "case_status": "Flow360Status.COMPLETED",
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+}

case_818/results_5/alpha_-5.3248985594344616/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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+CMzSkinFriction,-1.649080497205049e-06

case_818/results_5/alpha_-5.3248985594344616/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
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case_818/results_5/alpha_-5.3248985594344616/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
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case_818/results_5/alpha_-5.3248985594344616/forces_summary.json

@@ -0,0 +1,64 @@
+{
+  "case_id": "case-a8b5f47f-892f-4a25-b4e6-6c3b83fe60b3",
+  "case_name": "alpha_case",
+  "case_status": "Flow360Status.COMPLETED",
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+    "MzSkinFriction": -0.37915243683497346
+  }
+}

case_818/results_6/alpha_-3.005635423591282/force_coefficents_corected.csv

@@ -0,0 +1,25 @@
+,value
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+CDSkinFriction,0.01403837295199716
+CFxSkinFriction,0.0140219272626849
+CFySkinFriction,1.904416886930966e-06
+CFzSkinFriction,-0.0006815115946325743
+CMxSkinFriction,7.758386440799849e-07
+CMySkinFriction,0.004792007193127278
+CMzSkinFriction,8.136725164919485e-06

case_818/results_6/alpha_-3.005635423591282/force_coefficients.csv

@@ -0,0 +1,25 @@
+,value
+CL,-1.114613536185031
+CD,0.26014796898122683
+CFx,0.20134626040218764
+CFy,-0.00012977609852358283
+CFz,-1.126720898995848
+CMx,-0.0030782495099113023
+CMy,1.2434496864221258
+CMz,-0.002929684989722623
+CLPressure,-1.11519413248962
+CDPressure,0.11101693393793585
+CFxPressure,0.0523899295555669
+CFyPressure,-0.0001500069089235657
+CFzPressure,-1.1194811334012817
+CMxPressure,-0.003090206664962488
+CMyPressure,1.169595704727561
+CMzPressure,-0.003055087462457614
+CLSkinFriction,0.0005805963045882971
+CDSkinFriction,0.14913103504329084
+CFxSkinFriction,0.1489563308466205
+CFySkinFriction,2.023081039897381e-05
+CFzSkinFriction,-0.007239765594566319
+CMxSkinFriction,1.1957155051852773e-05
+CMySkinFriction,0.07385398169456155
+CMzSkinFriction,0.00012540247273532857

case_818/results_6/alpha_-3.005635423591282/forces_actual.csv

@@ -0,0 +1,25 @@
+,value_SI
+L,-3843.230474388844
+D,897.0002335168499
+Fx,694.2496737752355
+Fy,-0.44747299445170763
+Fz,-3884.97712846078
+LPressure,-3845.232392846385
+DPressure,382.790671234644
+FxPressure,180.64249830321012
+FyPressure,-0.517229609212476
+FzPressure,-3860.0141373816464
+LSkinFriction,2.001918457538698
+DSkinFriction,514.2095622822055
+FxSkinFriction,513.6071754720244
+FySkinFriction,0.06975661475728906
+FzSkinFriction,-24.962991079134195
+Mx,-10.613923068578037
+MxPressure,-10.655151800499773
+MxSkinFriction,0.04122873192403479
+My,4287.462490885678
+MyPressure,4032.8111127272937
+MySkinFriction,254.65137815837218
+Mz,-10.10166687137059
+MzPressure,-10.534059435369407
+MzSkinFriction,0.4323925639999808