Didn't the article say that the Su-57 and F-35 didn't have leading edge treatment while the J-20 did?
No, what it said more specifically was: "the trailing edge treatment on the canard and main wing of J-20 in the form of edge serration will be simulated because they are very easily to identify visually"
I.e.: only the trailing edge of the canard and main wing is represented because of the structurally visible serrations, and is represented in the form of structural edge serrations on the trailing edges only. Not on the edges of the entire aircraft, and not as RAM treatments.
F-35 and Su-57 as aircraft do not have serrated trailing edges that are structurally present, so they were not factored in.
So if you're asking whether J-20 in that simulation had any sort of RAM treatment advantage, I do not think so.