Speaking of stall characteristics, it seems to be impossible to land this thing
Once you slow down around 300 km and put it nose down with zero throttle, it has a severe case of aileron conversion! Sometimes even total lack of control. Deploying landing gear only worsens the situation, flaps do not really help. Again, only making things worse (combat flaps are OK, but anything beyond that is suicidal). I have no problems with a plane being tricky but - this seems bugged. (Same when I throttle up, the plane starts dancing midair, before settling in general direction.)
Yes Koty, this bird was impossible to fly.
That's intentional, aerodynamics can be tricky at times.
The "mistake" the japs did was to put a large 6-blade prop on a plane with laminar flow wings.
The U.S. noticed the same when they built their P-51H, where a 5-blade prop was tested briefly and got quickly abandoned in favor of the "old" 4-blade one.
Thing is that when the airflow leaves the laminar surface on such a wing in prop lee and the gap between the blades is small enough to cause an interference "wave" pattern on lee side, the effect of rudders in that airflow zone in fact will be inverted.
Nevertheless, I understand that this is a little too much realism for the standard armchair pilot we are, so please find a new version of this bird released in first post.
It differs in FM only, in that it now has the Modact sounds by default and the prop wash control surface inversion has been removed and the plane generally is a little more stable in the air.
Here are some flight model data figures, blue is Ki-94-II, red is Ta-152H-1 for comparison, light is normal, dark is WEP power.
Note that the flight behaviour of the two is completely different, but since they fulfill the same role, the performance naturally is similar.
TAS vs. Altitude:
RoC vs. Altitude:
RoC vs. Speed:
Turn time vs. Speed:
Fan plot:
Hope that helps
Best regards - Mike