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Joined Jul 2009
745 Posts
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Hi Stuart,
Here is the link to the Becker servos, http://www.becker-fm.de/shop/group/S...niversalservos all in German btw. I can translate if need be. Unless you have a Becker Rx you will have to change out the plugs. Becker uses 4 Pole plugs (only three pins connected). Also the servo square drive for the servo arms as opposed to the common round with ridges. I'll update this with a pic later. Cannot do it from work. Jens |
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Grand idea! When you mentioned gull wing, I almost immediately thought of an old timer aircraft called Spook - plans attached, (NOTE: not a flying wing!) Might give some ideas for construction. The plans are updated and have ailerons. Anyway, if it helps at all, shiny... Interesting project, that's for sure.
Mark |
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Quote:
Based on my modest flying experience, weight shifting or CG adjustment is probably one of the most effective ways to improve performance on these flying wings. The price is loss of control. Having an instant method to recover control may best be done by weight shift. Having a very forward CG will solve most control problems in a flying wing. Personally, I'd like to have a system that had fine adjustment of the CG on a slider on the Tx then a secondary control with a switch that would throw the CG way way forward for maximum control. Kind of a panic switch. I hope you get a chance to build a prototype Bruce. Should be interesting. ![]() ![]() ![]() Kent |
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Perhaps the use of the term "pendulum" was bad wording. The intent isn't to have a free hanging weight in the fuselage, Instead it's simply about having a CG location that sits well below the wing to achieve stability of the same sort found on hang gliders. The movable trim weight would be fully controlled by a servo running off the throttle channel. The idea would be to work with it and find the limits of CG location which produces a still stable but oscillating sort of slow trim and on the other end a high speed almost dive at the fast end. These limits would be found and then the trim weight tuned up to where I can use the throttle stick as a... um... a throttle.
I'd be able to stuff it forward for high speed trim or pull it back for slow almost oscillating flight. Mostly it would be used to vary between the minimum sink and best L/D speeds.Yes, if the model is disturbed by some turbulence or at some trim setting the model could be upset by this and depending on the damping ability and resonance in the system there's a risk of some fugoid oscillations. Hopefully the system isn't so strongly resonant that it runs away at a speed of oscilation which is beyond my ability to stab in some correction to counter it. Herk, that's a good point about the rudder hinge angle. It's not the sort of thing which is of any concern on any sort of normal planform but on something this closely coupled the elevator aspect could well be powerful enough to produce a noticable trim change. As I mentioned above I still don't have a proper shop yet to be able to make up the traveler for the trim weight. Or even have a decent spot to build a wing. So I'll have to content myself with some little all sheet test gliders to try out the idea for now. But by doing so I'll get more of a handle on the pitch oscillation issue. There's likely some relationship between the chord to lengthwise weight distribution which will play out to my advantage. For example I've seen descriptions of some plank gliders where it was found that the model tended to pitch oscillate rapidly. The conclusion being that a longer nose and tail so some weight could be placed out further to lengthen the period of resonance would have been worth trying. So I'll try this with the test gliders to see if it makes much difference. If made as electric powered models there's no doubt that some extreme downthrust will be needed. And for the same sort of reason why gliders with power pylons require lots of thrust angle. With the high wing placement and resulting higher center of drag compared to the thrust line there's bound to be a strong pitch up force from a nose mounted motor. |
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