perhaps add a comment on the modelling options used in this setup:
Model used to compute blade cross-sectional props, and to what degree the user should expect differences relative to the reference data in the yaml which is computed using BECAS.
Rotor performance: with aeroelastic analysis or not and if so, with torsional deflection or not. this will strongly affect predicted steady state performance.
perhaps add a comment on the modelling options used in this setup: