SLC wrote:
My explanation is pretty clear, as far as I'm concerned. Did you see the crappy MS Paint job I did a couple of pages ago? I simply don't see how I can describe it any clearer than that.
Ok, let me put it this way. Why does the two element wing work differently from a similarly sized single element wing? If it was just a single element, would the effect of stall be the same? I am assuming not, but maybe I'm wrong there. So, if I'm right, what is the effect of splitting the foil, which allows the drag imposed by the wake (is this form drag?) to be minimal in stall? I think my understanding is that the angle of attack of the top element is actually much smaller than its angle to the free stream because of the deflection caused by the main element. That is what simoncm is getting at in his drawings (although I agree there are some odd directions to their resolved vectors).
From the laymans perspective it appears as if the top element has an exceptionally steep AoA and hence the idea of it stalling is a bit like replacing it with a brick, nay, lintel. Do you see the line of argument? To summarise, yes the induced drag is high due to the angle to the free stream, but as the speed (and apparent AoA) is also high, stalling may induce a large parasitic drag, but, by some mechanism, it doesn't.
(I need a glossary!
)
[EDIT]: Did a bit more reading and I wanted to ask if the effect is connected to the low aspect ratio of the wing? [/EDIT]
SLC wrote:
My phd was on vortex merging and breakdown between two flat plates, and no, you may not read it - the research was paid for by my current employer and as a result it is confidential.
Shame. Does that mean you didn't publish? I suppose it doesn't matter so much if you were going straight into industry anyway. Was it numerical or experimental (or analytical???)? If it was numerical, can you say what sort of model you used?