pymead.analysis.calc\_aero\_data
================================

.. automodule:: pymead.analysis.calc_aero_data

   
   
   

   
   
   .. rubric:: Functions

   .. autosummary::
      :toctree:
   
      calculate_CPK_mses_inviscid_only
      calculate_Cl_alfa_xfoil_inviscid
      calculate_Cl_integral_form
      calculate_aero_data
      calculate_performance_parameters_from_polar
      compute_alpha_zero_lift
      convert_xfoil_string_to_aero_data
      estimate_LD_max
      line_integral_CPK_inviscid
      read_alfa_from_xfoil_cp_file
      read_alfa_from_xfoil_log_file
      read_forces_from_xfoil_polar_file
      run_mplot
      run_mpolar
      run_mses
      run_mset
      run_xfoil
      update_mses_settings_from_stencil
      update_xfoil_settings_from_stencil
      write_blade_file
      write_gridpar_file
      write_input_file
      write_mses_file
      write_spec_file
   
   

   
   
   .. rubric:: Classes

   .. autosummary::
      :toctree:
      :template: custom-class-template.rst
   
      AirfoilMSETMeshingParameters
      MPLOTSettings
      MPOLARSettings
      MSESSettings
      MSETSettings
      XFOILSettings