He did.
".......Even a cursory examination of the available photographs reveals major surface disruptions that would appear very bright to a modern high frequency radar. Access panels, cavities, and vents are visible which could not be eliminated or controlled without significant design changes."
"The sizing of some of these features matters. With even an imprecise measure of the size of some of these features it is clear that they were intended to mask the aircraft from lower frequency radars, and from a narrow range of aspect angles."
What he meant isn't just about how smooth it is, but the sizing of these features. It has to do with radar frequency irradiation of these features.
There are also many other major disruption on surface even from frontal angle that we can see from the comparison shot below.
A large frontal reflecting surface at the inlet, the bump along the edge of canard gap,
change of alignment angle along the gap, round LERX (Leading edge root extensions), gaps on the leading edge slats, and uneven surface along the body (see the alignment line).
I would assume those little spikes (I counted 5) that sticks out around the nose will be removed from the production line model. If not, those are major disruption too.
The examples in his writing was a loose screw on the Have Blue. If he were talking about smoothed out surface structures on the plane though he's really picking his cherries. The fact that there are structural bumps and uneven surfaces that are smoothed out along the is a normal characteristic we see in all stealth fighters (yes, that F-22 has these "defects" as well, including a less than perfect alignment line). The point is that the shape and size of these surface features, as well as its material composition and coating, are designed to limit radar return, and it's the overall effect of the airframe that counts and not its individual parts. Quellish's post argued that the J-20 had too many small protruding surface features that made it detectable with higher band radars, but it really doesn't have that many more surface features than the F-22 does, and like the F-22 those features are shaped.
In the J-20s case we don't know if the frontal reflectors along the inlet are heavily treated with Ram like the F-22s inlet, or if they're made with dielectric materials, or if they fact generate the same or lesser radar return because they block radar from entering the inlet (Also note that these features also exist in the F-35). We don't know if those LERXes are shaped in a way that still works with the shape of the airplane (it's the net outcome and not the parts after all), if they're made from radar transparent material, or if they're treated with RAM. We don't even know if or how many design revisions the J-20 will go through. However, in so far you haven't indicated anything that hurts radar return on the J-20 that doesn't exist on the F-22 in some way or form.
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