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airfoil_v0 / README.md
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---
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.