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What the hell?


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the whole point here is to defeat a condition called "retreating blade stall" that limits the top speed of a helicopter.

A helicopter's top forward speed can't approach the speed at which the retreating side of the rotor would cancel each other out... thus making all the lift come from the advancing side of the rotor and roll the aircraft over.

By making wings they introduce a new source of lift on both sides during fast forward flight.

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Catalyst,

I don't think this helo is being tested in order to defeat Retreating Blade Stall, as I doubt they can ever get around that. I think this prototype is testing to see if they can better performance from this Vectored Thrust Ducted Propeller. As a normal tail rotor uses up between 10% of a helo's power, just to stop it spinning around.

So if they can use this new rotor for anti-torque AND an extra bit of thrust, along with the little wings, I guess these guys will be happier?

But just seems... a bit daft to me. But I'd like to see how it pans out.

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Seems to me that once you had enough forward speed, you could rely on the wings to provide lift, and stop the rotor entirely: no retreating blade stall (no retreating blade at all...). I'm not sure about the practicalities of this though, as the aerodynamic loads on the rotors would probably rip the forward facing one(s) off. Might be simpler to leave the rotor off altogether...

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Seems to me that once you had enough forward speed, you could rely on the wings to provide lift, and stop the rotor entirely: no retreating blade stall (no retreating blade at all...). I'm not sure about the practicalities of this though, as the aerodynamic loads on the rotors would probably rip the forward facing one(s) off. Might be simpler to leave the rotor off altogether...

You mean like this?

http://www.aviastar.org/helicopters_eng/sik_x-wing.php

sik_x-wing_1.jpg

"This then progressed into trials involving an X-wing in place of the main rotor. Using a compressed air system this airfoil could be blown to affect cyclic and collective pitch. The wing could be stopped in flight and Sikorsky believed the design had potential for future use as a high-speed 'convertiplane'. First flight took place on 2 December 1987, but after three further flights all funding was suspended and the S-72X1 was placed in storage at Edwards AFB. "

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