{
  "airfoil_dir": "coord_seligFmt",
  "working_dir": "skin_cfrp_0001_45/evals",
  "output_csv": "skin_cfrp_0001_45/results.csv",
  "airfoil_files": null,
  "sample_size": null,
  "seed": 0,
  "jobs": 10,
  "solver_timeout": 10,
  "failed_case": "continue",
  "properties": [
    "mu",
    "ea", "gj", "ga22", "ga33", "ei22", "ei33",
    "stf12r", "stf13r", "stf14r", "stf15r", "stf16r",
    "stf23r", "stf24r", "stf25r", "stf26r",
    "stf34r", "stf35r", "stf36r",
    "stf45r", "stf46r",
    "stf56r",
    "cmp12r", "cmp13r", "cmp14r", "cmp15r", "cmp16r",
    "cmp23r", "cmp24r", "cmp25r", "cmp26r",
    "cmp34r", "cmp35r", "cmp36r",
    "cmp45r", "cmp46r",
    "cmp56r",
    "tc2", "tc3", "sc2", "sc3"
  ],
  "material_file": "data/materials.xml",
  "template_file": "data/airfoil_skin_only.template.xml",
  "template_params": {
    "mesh_size": 0.0025,
    "element_shape": "tri",
    "element_type": "linear",
    "translate_x": -0.25,
    "translate_y": 0.0,
    "scale": 1.0,
    "material_name": "carbon_epoxy_ud",
    "lamina_thickness": 0.001,
    "fiber_angle": 45
  }
}