Docskyhawk
Well-Known Member
I know that this subject has been talked about a lot but I can't find the one answer I want. If the CG is located in the diagram, how would the aircraft react in a full nose high stall? In level flight I can see the canard stalling first causing the nose to drop and pulling out of the stall but what if you went into a 50+ degree nose up attitude and went into a full stall? The way I see it, the aircraft would be pulled into a "tail slide" and if there isn't enough altitude to work out the attitude, the occupants are going to have a bad day. Correct me if I am wrong?
