calkit.yaml

name: nacafoil-openfoam
title: Simulating a NACA airfoil with OpenFOAM
description:
dependencies:
  - docker
  - uv
datasets:
  - path: processed/NACA0012_6e6_Ladson_80grit.csv
    imported_from:
      url: http://turbmodels.larc.nasa.gov/naca0012_val.html
  - path: processed/NACA0012_6e6_Ladson_120grit.csv
    imported_from:
      url: http://turbmodels.larc.nasa.gov/naca0012_val.html
  - path: processed/NACA0012_6e6_Ladson_180grit.csv
    imported_from:
      url: http://turbmodels.larc.nasa.gov/naca0012_val.html
  - path: processed/all-simulated.csv
    title: All simulation results
    stage: aggregate-results
environments:
  foam:
    kind: docker
    image: openfoam-2406-foampy
    wdir: /work
    path: Dockerfile
    default: true
    layers:
      - miniforge
      - foampy
  py:
    path: requirements.txt
    kind: uv-venv
    prefix: .venv
figures:
  - path: figures/naca0012-clcd.json
    title: NACA 0012 lift-to-drag ratio
    description: >
      Plotted against the Ladson 180 grit experimental data.
    stage: plot-clcd
  - path: figures/naca0012-re2e5-aoa-0-umag.png
    title: Velocity magnitude at 0 degrees angle of attack
    stage: plot-flow@0
  - path: figures/naca0012-re2e5-aoa-0-umag.html
    title: Velocity magnitude at 0 degrees angle of attack (interactive)
    stage: plot-flow@0
app:
  path: app
  url: https://petebachant-nacafoil-openfoam.hf.space
  title: NACA 0012
  kind: hf
questions:
  - How well does a 2-D steady RANS simulation predict airfoil loading?