Swing tests? It'll swing stable.Looking at it some more, I grow concerned about the tail. I know symmetry is over rated, but those big pods at the top look like a whole lot of asymmetric drag. A little cant of the canards might be a good idea. Drag is proportional to the square of airspeed, and lift approximately so (I just looked it up) so a fixed cant angle should do quite well. Don't ask me how to determine the desired angle any better than by trial and error, using swing tests or CFD.
Angling canards sounds like borrowing from Peter to pay Paul. Not sure of what the effect would be, and the effect could be dramatically different at different airspeed. You may cause more problems than you fix. so, like those rockets, which are stable during active boost/thrust, but then go unstable during coast..It looks a lot draggier than yours. I never had very serious doubts about yours, but this on looks a lot worse to me. If it swings stable but with a really high pitch angle then consider canting the canards to compensate.
Here's how I see it. The drag from those pods will induce an upward pitch torque. If it's as drastic as I suspect, something must be done about it. A slight cant to the canards, slanting down to the front, will create a downward pitch touque to counter that created by the pods. I too was concerned about airspeed sensitivity; so, as I said, I checked and found that that both effects are proportional to the square of the speed, and therefore they are proportional to each other, and that's just what's needed.Angling canards sounds like borrowing from Peter to pay Paul. Not sure of what the effect would be, and the effect could be dramatically different at different airspeed. You may cause more problems than you fix. so, like those rockets, which are stable during active boost/thrust, but then go unstable during coast..
As is, it has finage both horizontal and vertical, which is all you need to keep it stable (assuming the asymmetric drag is either dealt with or has been exaggerated by me). The lack of a ventral fin gives it a large yaw-roll coupling, which something real aeroplanes face as well. (The main reason that planes don't have ventral tail fins is that they would hit the ground when the nose is up for takeoff and landing.)but does it really hurt to go ahead and throw a ventral thin on
That, I ike. Or I would, if I were going to build this, which I'm most probably not. (I feel myself becoming defensive, which there's no reason for, and can only lead in a bad direction, so I'll mostly bow out now.)Thinking outside the box, maybe a detachable Lexan fin ... that couldALSOfit into a display stand.
He does seem to like putting engines in relatively silly and impractical locations. That tends to ping my BS-meter, even though many of my own designs have ridiculous aspects to them as well.Derek Meddings was a genius designer in that his stuff looked fantastic and cool, but aerodynamically, his designs are a disaster. None of this stuff was ever meant to fly. Sky1 from UFO is a perfect example, it's both draggy and unstable. With this design, those boxes on the tail would be ripped off by the airflow on an actual supersonic jet. If those were meant to be the engines, the stress on the tail/rudder would be more than the structure could bear.
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