and here with your last photo, we can very clearly see that the stronger more highly energized vortex is created by the LERX, not the canards. Now the canards should also be creating vortices, but they are far less energetic that the leading edge extenstion.
The picture immediately above it, pictures a very strong vortices off the inlet lip!
Canard vortices probably kick in fully only at high AOA. The Eurofighter AMK re-design shows that long-coupled + lerx + delta does work.
@Bltizo
Still going through previous responses, but let me mention again the J-20 isn't described as an air superiority aircraft, but rather as a heavyweight stealth fighter, which can "seize and maintain" air superiority, although I'll point out that air superiority and air superiority aircraft are two separate things.
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Let's point out the evidence first.
-J-20 has failed to show exceptional maneuverability in videos shown; best is a roughly 22-30 degree ITR turn at around 5000m of altitude, which is STR, and under afterburners as well.
-There's design docs from the original J-20 aerodynamic formula design that indicate why the LERX-Canard-LERX-Delta format was chosen, and it states that supermaneuverability was a goal.
-There's a document that says that the J-20 is a "heavy" stealth fighter, which is little more than a discussion of its weight class, but also that the J-20 is, in the order listed, aimed to seize air superiority, maintain air superiority, intercept enemy aircraft, then escort strike / bombers.
-The J-20 has WVR missile bays.
-But the J-20 also lacks a gun.
-The J-20 has weapons bays roughly comparable to the F-35, but it can't fit in current Chinese anti-ship and anti-radiation missiles, much less the PL-21/PL-XX that's designed for interception.
-Claims by PLAAF pilots have said that while the J-20 has decent (not bad, good, etc) performance subsonically, it has excellent performance supersonically.
-Claims by PLAAF pilots have said that the J-20 apparently beat Chinese domestically produced fighters in speed testing, implying that it has a higher top speed than any other Chinese aircraft in production.
This is essentially the direct evidence. More indirect evidence goes to the changing nature of modern warfare.
-The F-35, for instance, is not designed to out-dogfight an F-16 or match the F-22 in agility. It is designed for excellent ITR, but its STR is known to be questionable.
-Modern WVR missiles make it extremely difficult for dogfighting to be anything other than attritional warfare, given super-agile IR seekers that can reach 20km of range.
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The biggest difference in our perspectives is that I'm trying to guess at what modern stealth vs stealth warfare is going to look like in the future, i.e, I'm working more from the indirect evidence given.
Your point is that the design docs claim that the J-20 is designed to be supermaneuverable, when, first, supermaneuverability refers specifically to maneuvers in the post-stall range (i.e, ITR), and second, high maneuverability in a traditional dogfight setting is of questionable benefit in modern warfare when WVR missiles are making the WVR sphere suicide. From this perspective, we can reread what the evidence is showing us.
-The J-20 is designed for supermaneuverability. But that's an ITR factor (and 22-30 degree ITR has been demonstrated at altitude), and ITR is less relevant in dogfighting than STR.
-The J-20 is described as good, i.e, not outstanding as the F-22 or Su-57 might be, in terms of subsonic maneuverability.
-The J-20 has failed to show exceptional subsonic maneuverability during airshows and so on.
-The J-20 is described as having outstanding supersonic maneuverability and very high top-speeds.
Going from this, we can suspect that dogfighting is addressed, but not a priority on the J-20.
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But then again, we get back to repeating ourselves. You want the J-20 to be outstanding as a dogfighter. I don't care whether the J-20 is an outstanding dogfighter as long as it's a reasonable threat to the F-22 (in numbers) and capable of getting strong K
vs the F-35.