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Originally Posted by RyanW
On the other hand, helicopter rotors generate lift like a wing when the helicopter is moving, requiring much less down thrust (and thus power) than when hovering.
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They don't, really, except for specialized configurations (like X-wings). What is happening is that the rotor in forward flight is working on undisturbed air, rather than eating it's own downwash at a hover. This would apply to ducted fans as well. The benefit happens at relatively low airspeeds (~ 35 knots), and is called "effective translational lift."
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A helicopter operating at the edge of its capacity can even stall...
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It's called "retreating blade stall." It occurs when the forward airspeed gets close to the rotational velocity of rotor system. The advancing blade gets extra lift; the retreating blade has to increase its pitch to compensate for the loss of lift until it stalls. The helicopter pitches up (from gyroscopic precession -- the effect is felt 90 degrees out of phase) and rolls over. Note that if the rotor really acted like a fixed wing as high speeds, this wouldn't happen.
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...(fully loaded Hinds in the high altitudes of Afghanistan had to make rolling takeoffs).
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Same thing happened to Cobras during summer gunnery at Fort Carson, Colorado (5,874 ft above sea level at the airfield; higher at the range). This is just due to the reduction in effective lift at high altitude on hot days.
Another effect of high-hot conditions is loss of tail-rotor effectiveness at a hover. The Cobra operator's manual says that they aren't subject to this problem, but I can assure you that they are.