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On Tue, 08 Oct 2019 17:37:00 +0000, James Lambert wrote:
Funnily enough.... the assumption is made that the tail is acting with a 'downward' force, counterbalancing the mass ahead of the lift... with neutral stability, the elevator actually exerts no force in pitch. And it is also possible that the tail generates lift to support a rearward C of G !!! Indeed, but every glider I know the W&B for has the CG in front of the CL at all flying speeds (CL approaches 30% MAC at the stall, but as airspeed rises it moves further back. I'm far from certain that I'd want to fly anything with the CL at or behind the CG. Here's why: I know quite a lot about trimming small aircraft with rear CG positions - virtually all competition free flight models are set up this way because having both wing and tail providing lift adds efficiency, especially if the tail is flying at its minimum drag AOA. Which is the case for a well- designed model. Numbers: the F1A gliders (F1A is the international class for towline gliders - typically 2.2-2.7m span, min weight 420g) all flew best with the CG at 55% of MAC, a main wing AOA of about 8 degrees and the flat bottomed lifting tail at about 3.5 dergees AOA. The stability was good - it has to be to handle rough thermals and the turbulence you get below 50-100ft on a windy day. But I would not want to fly an aircraft with that trim set-up because the trim sensitivity was extreme - my tail had a 90 mm chord and I used a 10BA bolt as the trim adjuster (thats 1.7mm diameter, with a 0.35mm pitch). I could easily see the effect of half a turn on the trim (both still air duration and dynamic recovery from upsets) and so used to fine tune them in terms of 1/4 turn adjustments. That gives a 0.09mm movement at the TE of a 90mm chord tailplane, so a very small angular change indeed. 1-2 turns took it from stalling to an under-elevated over fast glide. On the other hand, similarly sized models with the CG in front of the CL, so flying with down force on the tail, are easy to trim by adding or removing pieces of 0.8mm or 1.6mm balsa under the TE of the tailplane. Bottom line: I would not want to hand-fly anything with that amount of pitch sensitivity so am happy to leave anything with its CG behind the CL in the hands of other, better and braver pilots than myself. -- Martin | martin at Gregorie | gregorie dot org |
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On Tue, 08 Oct 2019 19:41:20 +0000, Martin Gregorie wrote:
I'm far from certain that I'd want to fly anything with the CL at or behind the CG. Here's why: Errrrm: this should, of course, read: I'm far from certain that I'd want to fly anything with the CG at or behind the CL. Here's why: -- Martin | martin at Gregorie | gregorie dot org |
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