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Datasets:
ShapeBench
/
COCOANet

Tasks:
Tabular Regression
Size:
1K<n<10K
Tags:
aerodynamics
CFD
Flow360
drone
surrogate-model
shape-optimisation
License:
Dataset card Files
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  1. case_1524/reference_area/input.json +131 -0
  2. case_1524/reference_area/mac.txt +1 -0
  3. case_1524/reference_area/reference_area.txt +1 -0
  4. case_1524/reference_area/reference_area_m2.txt +1 -0
  5. case_1524/results/alpha_8.563814831742967/force_coefficents_corected.csv +25 -0
  6. case_1524/results/alpha_8.563814831742967/force_coefficients.csv +25 -0
  7. case_1524/results/alpha_8.563814831742967/forces_actual.csv +25 -0
  8. case_1524/results/alpha_8.563814831742967/forces_summary.json +64 -0
  9. case_1524/results_10/alpha_-3.6854144049433213/force_coefficents_corected.csv +25 -0
  10. case_1524/results_10/alpha_-3.6854144049433213/force_coefficients.csv +25 -0
  11. case_1524/results_10/alpha_-3.6854144049433213/forces_actual.csv +25 -0
  12. case_1524/results_10/alpha_-3.6854144049433213/forces_summary.json +64 -0
  13. case_1524/results_2/alpha_3.220884539846118/force_coefficents_corected.csv +25 -0
  14. case_1524/results_2/alpha_3.220884539846118/force_coefficients.csv +25 -0
  15. case_1524/results_2/alpha_3.220884539846118/forces_actual.csv +25 -0
  16. case_1524/results_2/alpha_3.220884539846118/forces_summary.json +64 -0
  17. case_1524/results_3/alpha_3.422856263052932/force_coefficents_corected.csv +25 -0
  18. case_1524/results_3/alpha_3.422856263052932/force_coefficients.csv +25 -0
  19. case_1524/results_3/alpha_3.422856263052932/forces_actual.csv +25 -0
  20. case_1524/results_3/alpha_3.422856263052932/forces_summary.json +64 -0
  21. case_1524/results_4/alpha_-5.258467345689072/force_coefficents_corected.csv +25 -0
  22. case_1524/results_4/alpha_-5.258467345689072/force_coefficients.csv +25 -0
  23. case_1524/results_4/alpha_-5.258467345689072/forces_actual.csv +25 -0
  24. case_1524/results_4/alpha_-5.258467345689072/forces_summary.json +64 -0
  25. case_1524/results_8/alpha_-7.4321127148671815/force_coefficents_corected.csv +25 -0
  26. case_1524/results_8/alpha_-7.4321127148671815/force_coefficients.csv +25 -0
  27. case_1524/results_8/alpha_-7.4321127148671815/forces_actual.csv +25 -0
  28. case_1524/results_8/alpha_-7.4321127148671815/forces_summary.json +64 -0
  29. case_1524/results_9/alpha_-1.8592674422095605/force_coefficents_corected.csv +25 -0
  30. case_1524/results_9/alpha_-1.8592674422095605/force_coefficients.csv +25 -0
  31. case_1524/results_9/alpha_-1.8592674422095605/forces_actual.csv +25 -0
  32. case_1524/results_9/alpha_-1.8592674422095605/forces_summary.json +64 -0
  33. case_1553/design_parameter_sample_1553.json +117 -0
  34. case_1553/param_10.json +19 -0
  35. case_1553/param_2.json +19 -0
  36. case_1553/param_3.json +19 -0
  37. case_1553/param_4.json +19 -0
  38. case_1553/param_5.json +19 -0
  39. case_1553/param_6.json +19 -0
  40. case_1553/param_7.json +19 -0
  41. case_1553/param_8.json +19 -0
  42. case_1553/param_9.json +19 -0
  43. case_1553/params.json +19 -0
  44. case_1553/results/alpha_-6.522116775860017/force_coefficents_corected.csv +25 -0
  45. case_1553/results/alpha_-6.522116775860017/force_coefficients.csv +25 -0
  46. case_1553/results/alpha_-6.522116775860017/forces_actual.csv +25 -0
  47. case_1553/results/alpha_-6.522116775860017/forces_summary.json +64 -0
  48. case_1553/results_10/alpha_-6.435705560328811/force_coefficents_corected.csv +25 -0
  49. case_1553/results_10/alpha_-6.435705560328811/force_coefficients.csv +25 -0
  50. case_1553/results_10/alpha_-6.435705560328811/forces_actual.csv +25 -0
case_1524/reference_area/input.json ADDED
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+ {
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+ "inputs": [
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+ "name": "Fore Top Angle",
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+ "description": "",
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+ "name": "Aft Top Angle",
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+ "units": "deg",
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+ "value": 12.706031079473806
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+ },
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+ {
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+ "description": "",
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+ "name": "Top Height Aft",
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+ "units": "mm",
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+ {
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+ "description": "",
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+ "name": "Bottom Height Aft",
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+ "units": "mm",
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+ "value": 146.0662553256861
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+ {
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+ "description": "",
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+ "name": "Wing span",
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+ "units": "mm",
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+ "value": 13945.018212347375
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+ {
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+ "description": "",
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+ "name": "Rear tail offset",
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+ "units": "mm",
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+ "value": 1561.5208849875423
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+ {
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+ "description": "",
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+ "name": "Root Chord",
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+ {
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+ "description": "",
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+ "name": "Tail Root chord",
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+ "value": 873.021610100225
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+ {
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+ "description": "",
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+ "name": "File Path_0",
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+ "type": "file_path",
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+ "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/CCA_Drone/cases/case_1524/reference_area/../design_1524.stl"
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+ },
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+ {
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+ "description": "",
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+ "name": "File Surface Reference",
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+ "type": "file_path",
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+ "value": "/scratch/data_generation/Dataset_generation_ntop/Dataset_Generation/CCA_Drone/cases/case_1524/reference_area/reference_area.txt"
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+ }
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+ ],
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+ "title": "CCA_1_automated"
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+ }
case_1524/reference_area/mac.txt ADDED
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case_1524/results_2/alpha_3.220884539846118/force_coefficents_corected.csv ADDED
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case_1524/results_4/alpha_-5.258467345689072/force_coefficents_corected.csv ADDED
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case_1524/results_4/alpha_-5.258467345689072/force_coefficients.csv ADDED
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case_1524/results_8/alpha_-7.4321127148671815/force_coefficents_corected.csv ADDED
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case_1524/results_8/alpha_-7.4321127148671815/force_coefficients.csv ADDED
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case_1524/results_9/alpha_-1.8592674422095605/force_coefficents_corected.csv ADDED
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+ }
case_1553/results_10/alpha_-6.435705560328811/force_coefficents_corected.csv ADDED
@@ -0,0 +1,25 @@
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
1
+ ,value
2
+ CL,-0.4432773231621514
3
+ CD,0.04626668134721837
4
+ CFx,-0.003711039294658778
5
+ CFy,-2.994264187580365e-05
6
+ CFz,-0.4456698545112076
7
+ CMx,0.0004407675708658455
8
+ CMy,0.6730441156535527
9
+ CMz,-0.0001418379143382115
10
+ CLPressure,-0.4436086454275771
11
+ CDPressure,0.03514313136911995
12
+ CFxPressure,-0.01480162888290985
13
+ CFyPressure,-2.916168871349138e-05
14
+ CFzPressure,-0.4447522701043016
15
+ CMxPressure,0.0004394815937367143
16
+ CMyPressure,0.6697250998224921
17
+ CMzPressure,-0.0001466481005936342
18
+ CLSkinFriction,0.0003313222654256321
19
+ CDSkinFriction,0.01112354997809844
20
+ CFxSkinFriction,0.01109058958825108
21
+ CFySkinFriction,-7.809531622782423e-07
22
+ CFzSkinFriction,-0.0009175844069060583
23
+ CMxSkinFriction,1.285977128711145e-06
24
+ CMySkinFriction,0.003319015831061424
25
+ CMzSkinFriction,4.810186255624728e-06
case_1553/results_10/alpha_-6.435705560328811/force_coefficients.csv ADDED
@@ -0,0 +1,25 @@
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
1
+ ,value
2
+ CL,-5.130751617820713
3
+ CD,0.5355176946116892
4
+ CFx,-0.042953744461910484
5
+ CFy,-0.0003465736914990086
6
+ CFz,-5.158444178320512
7
+ CMx,0.008449386369545519
8
+ CMy,12.902060298435192
9
+ CMz,-0.0027189916393799626
10
+ CLPressure,-5.134586535964566
11
+ CDPressure,0.40676720577795084
12
+ CFxPressure,-0.1713227304199166
13
+ CFyPressure,-0.00033753448175014863
14
+ CFzPressure,-5.147823518444127
15
+ CMxPressure,0.008424734561325862
16
+ CMyPressure,12.838435728532781
17
+ CMzPressure,-0.0028112015133997426
18
+ CLSkinFriction,0.003834918143851785
19
+ CDSkinFriction,0.1287504888337386
20
+ CFxSkinFriction,0.12836898595800622
21
+ CFySkinFriction,-9.039209748466138e-06
22
+ CFzSkinFriction,-0.0106206598763866
23
+ CMxSkinFriction,2.4651808211603628e-05
24
+ CMySkinFriction,0.06362456990242531
25
+ CMzSkinFriction,9.220987402365212e-05
case_1553/results_10/alpha_-6.435705560328811/forces_actual.csv ADDED
@@ -0,0 +1,25 @@
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
1
+ ,value_SI
2
+ L,-36200.409035406614
3
+ D,3778.3859041836254
4
+ Fx,-303.06341739925296
5
+ Fy,-2.4452770914885753
6
+ Fz,-36395.79600636201
7
+ LPressure,-36227.466592615696
8
+ DPressure,2869.977018611892
9
+ FxPressure,-1208.7805803583142
10
+ FyPressure,-2.3815002582602784
11
+ FzPressure,-36320.861131242404
12
+ LSkinFriction,27.05755720907478
13
+ DSkinFriction,908.4088855717348
14
+ FxSkinFriction,905.7171629590619
15
+ FySkinFriction,-0.06377683322551816
16
+ FzSkinFriction,-74.9348751196088
17
+ Mx,59.6152894272547
18
+ MxPressure,59.4413567157365
19
+ MxSkinFriction,0.1739327114613855
20
+ My,91031.46965458016
21
+ MyPressure,90582.56165303722
22
+ MySkinFriction,448.90800154304026
23
+ Mz,-19.184052716083926
24
+ MzPressure,-19.834646509208756
25
+ MzSkinFriction,0.6505937931521527