Originally Posted by Owain Glyndwr
What you describe is a stall with a POSITIVE THS load.
Right, with the elevator in full up position almost masked to the airflow and counterbalanced by an assumed nose up wing/body moment. If the elevator goes down, the THS + elevator frontal area increases about 30% and could overcome the wing/body moment.
I did consider the wing body assembly
Sorry then, I thought you did not based this sentence in your post #295: “When it gets to this point I think the centre of lift/pressure will be fairly close to the centre of area of the exposed wing. For the A330, this is about 70% mac”.