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Why does the canard rotor wing (CRW) use a canard? The CRW is a helicopter using engine exhaust to drive the rotor. The exhaust can be used in the normal way to drive the aircraft once high enough speed has been reached. Why can't the CRW use a tail instead?

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  • $\begingroup$ Well, it has to use a canard because if it didn't then it wouldn't be a canard rotor wing, would it? $\endgroup$ Dec 17 '15 at 0:04
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The Canard rotor/wing demonstrator, later called the X-50 Dragonfly was a Stop-Rotor Rotary Wing Aircraft made by Boeing and DARPA to demonstrate the principle that a helicopter's rotor could be stopped in flight and act as a fixed wing (like in movie The Sixth Day).

X-50

Image from boeing.com

The canard is used in case of Boeing X-50 Dragonfly in order to overcome the transient aerodynamic loads that occurred during conversion from rotary to fixed-wing flight. During transition from rotary mode to fixed wing mode, the rotor is being unloaded and the aircraft has to produce enough lift. The designers used both a canard and horizontal stabilizer to overcome this problem.

From Canard Rotor/Wing Aircraft:

During development, analysis and testing indicated that the X-wing design encountered high transient aerodynamic loads during the conversion from rotary to fixed-wing flight. The CRW design addresses this issue by generating positive lift on both the canard and horizontal tail during conversion. By deploying the flapped canard and the full-flying horizontal tail, enough lift can be produced to support the weight of the aircraft, and the main rotor can be completely unloaded throughout the conversion maneuver.

The aircraft never made a conversion flight and the program was canceled.

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