I think we now have a full picture of how the J-20's vortex generation system works. From the looks of it the vortex generators work in stages, with each stage progressing at a greater AoA. The first stage is the vortices formed by the LERXes. The second is the vortices formed from the LERXes in conjunction with those formed by the dogtooth created from the leading edge slats dropping. The third is the first two strengthened by the camber of the LERXes in conjunction with the canard downwash. The last is all prior three plus vortical flow formed over the centerline fuselage from the fore body camber over the inlets. The first three work together to form an ever expanding low pressure zone over the wings that gradually encompasses their whole area, while the last one forms a lower pressure area that encompasses the whole top side of the plane including the centerline fuselage and, from the looks of it at least, the canards.
and here I want to bring forward the (SDF post of the day), of the many excellent posts today, today has been a day like SDF of the past, outstanding thinking and good manners, beautiful pictures and videos, but here my friend latenlazy, (I love this name man, takes a big man to wear it) through the "scientific method of observation" has taken those beautiful pictures of vortices lift and dissected the brilliant aerodynamics of the J-20, proving that a thoughtful man provided with photographic evidence, is able to see and accurately formulate an accurate thesis providing insight and analysis of these very complex aerodynamics!
Good job Man! and thank you for taking the time to explain it, believe it or not, our own Engineer, took the time to patiently walk me though this beautiful airplane long ago, and the light bulb came on? and here brother, you've brought forth a thoughted and insightful look at this amazing airframe... I hope everyone will take the time to read his analysis,,,,, its worth stopping and letting him spell it out!