
Mark2
Originally uploaded by Mikebert4
Right. Given the failings of Mark1, I tried a new tact with Mark2. You’ll notice that it looks considerably different from Mark1 with massively swept wings. It flew very well, though couldn’t cope without still-air conditions and really didn’t suceed outside.
The Techy Bit (read at your own peril):
The swept wings add a lot of lateral (roll) stability whilst also moving the centre of pressure rearwards (which is effectively the same as moving the CofG forwards). So, 2 is markedly more stable. Drag is reduced too.
The problems arise from the large leading-edge radius and the method of mounting the wings onto the glider. To explain this I’ll have to give you a tiny bit of theory.
When considering a full-sized aerofoil (such as on a large transport jet) we attempt to keep the flow over the wing as smooth as possible (‘laminar’ flow) this reduces friction and helps the aerofoil move through the air. This is why you see a very smooth surface on a wing.
Contary to some teachings, having the air flow over the wing in a turbulant manner doesn’t reduce the amount of lift the wing generates. Indeed turbulent flow brings a lot more energy into the layer immeadiately next to the wing surface (‘boundary layer’), which helps to delay the stall. Though it achieves this at the cost of increased skin-friction drag, which affects fuel burn and top speeds.
On a model aircraft we have a different battle to fight. The air flowing over the wings is too smooth, meaning that we don’t get as much of a difference in pressure between the top and bottom of the wing as we would like. Another affect of the reduced scale of models is that only a small proportion of the total lift is gained in the conventional manner (faster air over the top surface droppping the pressure, causing th higher pressure underneeth to ‘push’ the wing up).
On a model we rely much more on the effect of the difference in angle between the chord of the aerofoil and the free-stream airflow. The process is simply that the air hits the underside of the wing and this increases the pressure under the wing and gives us lift (as well as deflecting the air downwards and giving us a small amount of newtonian lift). This is known as reaction lift.
Last bit of theory, this should bring most of it together for us.
Because of the reliance on this reaction lift, the aerofoil tends to sit at a high angle of attack – close to the stall. So, to delay the stall and hence allow us to gain more lift, we need to create turbulant airflow over the wing.
Thats it, turbulant airflow over a small-scale wing is prefered. You can test this by building a paper aeroplane and flying it, then taking a pair of scissors and cutting lots of small nicks (~2mm long) all down the leading edges, and flying it again. You’ll notice a marked improvement in it’s glide. It really does work.
Anyway, now we can get back to why Mark2 doesn’t fly so well. Because of the large leading-edge radius, the wing favours laminar flow. This means that when the aircraft settles down into it’s normal flight attitude, it’s close to the stall. Indeed, it does stall and then the nose drops (good ol’ longitudinal stability) and it picks up speed. and the nose starts to rise again. Now, at a faster speed the nose rises and the wings generate their reaction lift. Lots of it. The wings bend up. Suddenly all that lift isn’t holding the glider in the air, and it (all the while accelerating) spirals down to the grond.
There are two ways of thinking to solve this:
1. Delay the stall, strengthen wings
Later stall means longer time flying, but it also measn the glider will have to be accelerating for longer to bring the nose up – this means it’ll be going faster and it’ll more likely than not over-pitch up and stall again – given that the strengthened wings won’t bend up.
2. Promote earlier stall, recover quicker.
This means the wing stalls quickly, and the glider has to accelerate less to bring the nose up to normal flight again. Because we’re not accelerating as much, the wings don’t tend to bend up and we remain nicely airborne. Incidentally, the motion of diving, accelerating, climing slightly, stalling, diving, accelerating (etc…) in effect the apparant porpussing of the glider is known as a ‘Phugoid’ motion.
Deep breaths all, that was a long one
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