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(Bob Kuykendall) wrote in message . com...
Earlier, (Fred the Red Shirt) wrote: On a related note it appears that the Marske Monarch useds flaps (and spoilers both ... this is a flying wing with neither elevator nor canards. I'm curious as to how pitch is controlled. I don't think that that's quite an accurate assessment of the Monarch configuration. The movable control surface on the wing inboard trailing edge performs the same function as the elevator on a conventional tailed aircraft. It responds to fore-and-aft motion of the stick and controls the pitch attitude. It is sometimes (but not always) called an "elevon" on a tailless aircraft. Its location aft of the CG gives it adequate moment arm to perform its function. I see. There was some discussion on the site of cg shifting for pitch control but it was't clear if that was used in the Monarch or not. It seems to me that it would be wasteful to add weight for that purpose though I suppose you could put the pilot's seat on wheels and roll him back and forth for pitch control. Another interesting tailless aircraft is the Brightstar SWIFT, which is a swept-wing tailless glider that uses flaps for pitch control. The name is an acronym meaning Swept Wing with Inboard Flaps for Trim. The sweep of the SWIFT wing places the flaps far enough forward so that deflecting them down causes a pitch-up moment. The value of this feature is that pitching up is done by effectively increasing the wing camber, which better suits the wing to slower flight. Oh, cool. The flaps are functionally similar to canards. Thanks for the info. -- FF |
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