Following on from the discussion on sharp vs round LE, it seems to me that the desired profile characteristics are:
Does not exibit hysterisis loops or other anomolies in the performance curves.
Has a slow and controlled stall.
Seems heigh CL max is not necessarily required. We are mostely interested in smooth handling and and stable Cmo.
If these are the requirements, then the following might be a guide
to the profile shape we are loofing for.
If the max thick point is fairly forward say around 15-20% of chord,
that allows for a smoothly rounded and blended LE. The section need
not be so thick as the airflow on a thinner section of this type
would likely be quite stable over most of it's trim range closser
to Cl max. It would also allow the aft part of the profile to be quite straight or even concave which would help boundary layer
reattachment should a seperation bubble form or in the case of
flaps a less severe preasure gradient over the convex side of the
flap hinge.
This would be somewhat of a departure from current practice and
has most likely been looked into before. Not seriously proposing
a change, just curious.
Does anyone have good solid quantitative information to share
on this type of section?
Regards,
Ken

Steve