Aha, you were right all along; a bit of wikiing reveals this:kalinka wrote:Yes, I'm pretty sure, because you can google the problem and will find more than 100 other studies about same effect. (blown flap, boundary layer control...) What I posted here is just I think the shortest, clearest explanation. You can find studies with 20-30 pages and more diagrams if you wish. The blowing wing concept is all about anti-stalling the wing : sticking the airflow to the surface of the wing all the way to the end. So the rear wing may "stall" in case of high angle,and high speed situation, but here the "stall" means dramatically increased drag+low downforce because the airflow is no longer sticking to the surface of the wing. It's my understanding though.
http://en.wikipedia.org/wiki/Circulation_control_wing
Seems to be a much better explanation of the concept- the blown flaps idea is something of an aviation-specific evolution on this theme.
This still leaves me puzzled as to why there was a line of the aero paint just above the slit (in those photos posted earlier). Does that indicate the airflow detaching from the wing, as Raptor suggested earlier? Surely that can't be the intention; or can it?
As to pup's idea with the pressure valvey doodah at the back; that sounds interesting, but is there any reason to stop blowing air out the CCW slit, at any speed? Would there be any possible drag reduction from stalling the wing at high speeds?(ie tune it so that when CCW airflow is stopped, wing stalls)
I guess that would basically be the same as my previous idea, only working the other way (so the blown slit is making the wing stall later rather than earlier).
Heh, I feel the same. Trying to work it all out from badly written wiki articles and mentally modelling the airflow gives me a headache. Real interesting stuff though.Pup wrote:Physics 101 just never prepared me for stuff such as that.