Category
page 1Helicopter aerodynamics
helicopter rotor
rotary wings and control system that generates the lift and thrust for a helicopter

autorotation
thumb|upright=1.14|Airflow through a helicopter rotor. Above, the rotor is powered and pushing air downward, generating lift and thrust. Below, the helicopter rotor has lost power, and the craft is making an emergency landing.

vortex ring state
Aerodynamic condition related to helicopter flight
ground resonance
imbalance helicopter rotation when the blades become bunched in the rotational plane, typically on the ground when the landing gear is prevented from freely moving
vortex ring
torus-shaped vortex in a fluid or gas
brownout
in-flight visual impairment by pilots
retreating blade stall
loss of lift in rotary wing aircraft where the retreating rotor blade has a lower relative blade speed combined with an increased angle of attack
Loss of tail-rotor effectiveness
potential dangerous event during helicopter flight
Dissymmetry of lift
Term in rotorcraft aerodynamics
blade element theory
mathematical process by William Froude