A theoretical analysis indicates that, for rotors, ground effect decreases rapidly with increases in either height above the ground or forward speed. The decrease with height above the ground in forward flights is greater than that in hovering. The major part of the decrease in ground effect with forward speed occurs at speeds less than 1.5 times the hovering mean induced velocity. Consequently, the total induced velocity at the rotor center increases rather than decreases when a helicopter gathers speed at low height above the ground
The performance of a Quad Tilt Rotor (QTR) in helicopter mode was experimentally studied in ground e...
Wind tunnel investigation of helicopter directional control in rearward flight in ground effec
In this paper, a comprehensive experimental survey of the aerodynamic interaction of a hovering roto...
The thrust produced by a helicopter rotor hovering near ground and/or ceiling planes is investigated...
A study is presented of ground effect as applied to the lifting airscrew of the type used in modern ...
Wind tunnel measurements show that the wake of a rotor, except at near-hovering speeds, is not like ...
The wake characteristics of a rotorcraft are affected by the proximity of a rotor to the ground surf...
A lifting surface theory has been developed for a helicopter rotor in forward flight for incompressi...
Wind tunnel measurements show that the wake of a rotor, except at near hovering speeds, is not like ...
The conclusion of a previous article by Pistolesi is that the increment of lift due to ground effect...
In what follows an estimate will be made of the magnitude of the ground effect. For the two cases wh...
The effect of the ground on a rotor wake in forward flight has been investigated experimentally in ...
Hovering and steady low-speed forward-flight tests were run on a 4-foot-diameter rotor at a ground h...
Rotorcraft operating in ground effect have been known to experience beneficial performance effects a...
There are concerns about the influence of the gust wind caused by helicopters affecting the moving v...
The performance of a Quad Tilt Rotor (QTR) in helicopter mode was experimentally studied in ground e...
Wind tunnel investigation of helicopter directional control in rearward flight in ground effec
In this paper, a comprehensive experimental survey of the aerodynamic interaction of a hovering roto...
The thrust produced by a helicopter rotor hovering near ground and/or ceiling planes is investigated...
A study is presented of ground effect as applied to the lifting airscrew of the type used in modern ...
Wind tunnel measurements show that the wake of a rotor, except at near-hovering speeds, is not like ...
The wake characteristics of a rotorcraft are affected by the proximity of a rotor to the ground surf...
A lifting surface theory has been developed for a helicopter rotor in forward flight for incompressi...
Wind tunnel measurements show that the wake of a rotor, except at near hovering speeds, is not like ...
The conclusion of a previous article by Pistolesi is that the increment of lift due to ground effect...
In what follows an estimate will be made of the magnitude of the ground effect. For the two cases wh...
The effect of the ground on a rotor wake in forward flight has been investigated experimentally in ...
Hovering and steady low-speed forward-flight tests were run on a 4-foot-diameter rotor at a ground h...
Rotorcraft operating in ground effect have been known to experience beneficial performance effects a...
There are concerns about the influence of the gust wind caused by helicopters affecting the moving v...
The performance of a Quad Tilt Rotor (QTR) in helicopter mode was experimentally studied in ground e...
Wind tunnel investigation of helicopter directional control in rearward flight in ground effec
In this paper, a comprehensive experimental survey of the aerodynamic interaction of a hovering roto...