Something like this is what I had in mind.
They could make a slit in the wing between the pylons (would be more effective and predictable than slits in the pylon).bhallg2k wrote:It seems to me that you'd just need to make the inboard slits smaller than the outboard ones, small enough so that the vented flow doesn't overlap.
If these slits blow vertical to the wing surface you can detach the flow from it. At least that's what all the F-Ducts of the olden days did and it worked for them.bhallg2k wrote:I'm not so sure about that, actually. It's the flow over the trailing edge of the main plane that must be stalled in order to achieve the desired effect, and don't think a single 15cm vent between the pylons could do the trick. It might help maybe perhaps kinda.
It is not strictly turbulent air you have to introduce you have to create a high pressure to overcome the Coanda effect and use a flow direction perpendicular to the main flow so that the two flows don't mix (granted, the boundary layer is turbulent).bhallg2k wrote:Old F-ducts worked with slits because they were placed just under the trailing edge of the main plane and extended pretty much from end plate to end plate, and that's simply not allowed anymore. A 15cm slit under the wing, between the pylons would have no stalling effect on the trailing edge of the main plane, because its output would be laminar by the time it reached the target.
Maybe a sit on the back of the wing could help, but I don't know that it's necessary because the duct slits already directly apply turbulent air flow to the desired area.
I could be wrong, though, and it wouldn't be the first time.