riff_raff wrote:
The principle of ground effects is different when considering an aircraft or a race car.
Then there is the additional lift effect produced by helicopter rotors operating in ground effect. The ground effect experienced by an aircraft during landing or a rotorcraft HIGE is momentarily increased lift. The ground effect sought by race cars is continuously greater levels of downforce.
IMO ...... the ground effect is continuous
ie there is continuous availability if much greater Cl and thereby much greater L:D ratio
eg the power required to hover a helicopter above ground effect is much higher than for hover in ground effect
the minimum power to sustain aeroplane flight in ground effect is much lower than minimum power for sustained flight outside GE
(the Dornier X spent maybe half its flight time in GE crossing the Atlantic in 1928?)
GE is available all the time, the aeroplane pilot accesses it only briefly (for various good reasons)
aeroplane pilots who accessed it longer are very few, .... well done olefud !
GE adds 50% - !00% to the efficiency to rotary or fixed-wing flight, that's why they invented WIGE vehicles
the modern helicopter HIGE lift is about 4 times its core minimum weight
(that is the notional weight of the minimum possible structural and lift system without redundant engine(s) fuel etc etc)
HIGEs everse analog ie 'super fan-car' capability
am I the only person who thinks that fan power in fan-cars would not have greatly increased but for the fan-car ban ?