Mart,
...... in cruise where mass flow is high enough to reduce required thrust.
Are you saying that the thrust [lift] from the rotors is less in forward flight than it is in hover????
So your intermesher is a sub 200kts machine then?
Who said that????
Please, look at the [Line of zero airflow. Mu = 1.0], in the drawing on post #465.
P.S. You have a couple of PPRuNe private messages and emails, dated mid-March and a week ago.
Dave