Originally posted by Widewing:
I think, of greater significance is the angle of incidence of the wing. This should determine the angle of the nose relative to the ground while in level flight.
Widewing
I have to disagree. AoA of the airfoil in level flight is pitch + angle of incidence. AoA will have to be adjusted so that lift equals weight for the given airspeed. You can't change the angle of incidence on most planes so you will have to raise or lower the nose. Angle of incidence is normally set to give the pitch for lowest fuselage drag at the design speed and weight(*) and that's it.
However, I recall reading at least one reference to the seemingly tail-high attitude of the 190s (Clostermann, I think). Probably had a fuselage design that created this illusion. I'm fairly sure they didn't design the thing to fly around with the thrust vector pointing downwards.

Cheers,
/ft
(*) Except for on the DC-10 where they messed up bigtime, if ramp rumors are true

Getting the W&B right was a PITA at least, nose heavy crates those. Especially the ones retrofitted with a galley in the forward cargo bay...