AIRSPEED DOES NOT MATTER:
Airspeed does not affect the nosewheel thunk because the aircraft is designed to have stabilator authority well below the stall speed of the wing. This means that no matter what airspeed you touch down at, you will have enough stabilator authority to control the nosewheel touchdown. Kinetic forward energy does not bang the nosewheel down, its the kinetic energy of the nosewheel in the downward direction. Excessive nose-down kinetic energy is a function of the pilot NOT properly controlling the forward rotation induced after touchdown. In fact, the SLOWER you land an Arrow, the more likely you are to thunk the nose because the nose will be higher, the aircraft slower, stabilator authority reduced, and forward rotation on touchdown will happen faster.
A pilot with proper touchdown technique will only have to deal with excessive airspeed on the rollout AFTER landing, NOT on the touchdown. The sink rate a pilot has at the moment of touchdown is only affected by airspeed if they were taught to try and stall the plane onto the runway. Unless I'm mistaken, a landing consists of a pilot CONTROLLING the plane/runway meeting.
TRIM DOES NOT MATTER:
Trim has nothing to do with sink rate or the flare. It has everything to do with airspeed, and airspeed does not matter.
Nose-heavy is what a pilot calls a plane they can't land right yet. All aircraft have an operating W&B envelope that is fairly tight across all models and is designed to allow normal stall characteristics at the aft end and ensure control authority at the forward end. This is for all aircraft. If one aircraft "feels" nose heavy, it's really in the mind of the pilot.