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airfoil_v0 / README.md
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metadata
dataset_info:
  features:
    - name: initial_design
      struct:
        - name: angle_of_attack
          dtype: float32
        - name: coords
          sequence:
            sequence: float64
    - name: optimal_design
      struct:
        - name: angle_of_attack
          dtype: float32
        - name: coords
          sequence:
            sequence: float64
    - name: mach
      dtype: float64
    - name: reynolds
      dtype: float64
    - name: cl_target
      dtype: float64
    - name: area_ratio_min
      dtype: float64
    - name: area_initial
      dtype: float64
    - name: cd
      dtype: float64
    - name: cl
      dtype: float64
    - name: cl_con_violation
      dtype: float64
    - name: area_ratio
      dtype: float64
  splits:
    - name: train
      num_bytes: 4673504
      num_examples: 748
    - name: val
      num_bytes: 874720
      num_examples: 140
    - name: test
      num_bytes: 293656
      num_examples: 47
  download_size: 6693772
  dataset_size: 5841880
configs:
  - config_name: default
    data_files:
      - split: train
        path: data/train-*
      - split: val
        path: data/val-*
      - split: test
        path: data/test-*
license: cc-by-nc-sa-4.0

This dataset is part of the EngiBench toolkit: https://github.com/IDEALLab/EngiBench.