Why the helicopter drifts, rolls, and surges as it starts to fly.
In a hover the tail rotor produces a sideward thrust to counter main-rotor torque, and that thrust makes the whole helicopter drift sideways — this is translating tendency (tail-rotor drift). The pilot (and often a slight rigging offset) counters it with cyclic so the helicopter holds position.
In forward flight the advancing blade sees higher relative wind than the retreating blade, so it would make more lift — an imbalance called dissymmetry of lift. The rotor equalizes it through blade flapping: the advancing blade flaps up (reducing angle of attack) and the retreating blade flaps down (increasing it), keeping lift balanced across the disc.
As airspeed increases (roughly 16–24 kt), the rotor moves into undisturbed air and becomes markedly more efficient — effective translational lift. You feel it as a tendency to climb and a slight pitch/roll change, with some airframe vibration smoothing out. Transverse flow effect and gyroscopic precession contribute to the pitch-up/roll you anticipate with cyclic.
Curated reference clip — “Effective Translational Lift (ETL) in Helicopters,” Helicopter Lessons In 10 Minutes or Less (YouTube). Embedded with the creator's player; we don't host or alter it.