I've been wondering what route they will go down, will they go down the LOAN nozzle with 3D TVC route or pure flat 2D TVC route.
SAC patents suggests the latter or some form of the latter.
I've heard that flat nozzles may have a higher RCS from the rear than an axisymmetric one but is better more IR signature suppression.
Yup to both. The 90 degree angles that the rectangular nozzle forms aren't doing it favours too.
Another thing I've noticed is that current J-20 and likewise J-35 do not use ceramics to coat the interior walls like the F-35 to decrease IR signature
The J-20 does. It's the white paint on the interior walls. Not sure about the J-35 since we lack clear imagery of service birds.
WS-10C equipped J-20s have a non serrated circular ring inside the serrated nozzles
Well, it's RCS effects are minimal enough for the PLA to be happy with 300+ birds. I wouldn't be too concerned.
IMO it seems that WS-15 will solve the problem for J-20 but the prototype we had good pictures of the engines still don't seem to have the ceramic coatings hopefully they do come equipped on production J-20As that we may see any day now same goes for production J-35s with WS-19.
From what I've heard, the WS-15's axisymmetric nozzle option wouldn't need a ceramic coat on the interior walls. The material/integrated cooling (I forgot) straight up suppresses IR signature without the need of a coat.