DanSavage
Posts: 577
Joined: 4/17/2002 From: Trabuco Canyon,
CA, USA Status: offline
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quote:
ORIGINAL: petronio Thanks for the video DanSavage, I had already seen it but it was funny to see it again hehe. I read some time ago the post where the video was and according to the guy he had some problems with his radio and the elevator or something like that. At least the thought that it wasn't presumably the model consoles me , Im quite conscious that because of that little tail moment one should have very little throw on the elevator. I also abandoned the original idea of using a reflexed airfoil, as if it were a flying wing and using ailevons to control it. Instead I will go for the S-3021 and have the elevator working as a whole, inserting some carbon tubes in it and moving both elevators with one servo (if its possible) and if not with two. I used an excel program that I have to calculate the CG but I calculated it again using the usual method (attached image), according to this the CG is in fact slightly forward. In the program I have to input the data about the wing and in the second case I used the top view of the wing in the plan. byeeee You're welcome. The only problem I saw with that model was that it was massively tail-heavy. That's what caused the uncontrollable pitching up and down. When a model is that tail-heavy, the elevator doesn't respond to input so it can make it seem like there's a problem with the radio. I don't think you'll need to make it into a flying wing. I think the tail area is sufficient to fly the model. Your method is fine. But, if you only calculated it using the visible part of the wing, then it'll end up as tail-heavy as the model seen in the video, and probably with the same results. To correctly calculate the CG, carry the wing leading and trailing edges all the way to the fuselage centerline. I've got a 3-view of a Bug at home. I'll calculate the CG then post my results and you can compare what I got to your results. Cool project. Dan
< Message edited by DanSavage -- 12/14/2007 10:01:19 PM >
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