I'll gladly oblige, Deino!
According to this drawing from the same person who first indicated we might see a J-10 with TVC and J-20s with sawtoothed nozzles, yes. There are supposedly two J-20s testing the WS-10 with sawtoothed nozzles, and another one testing TVC.
Interesting... though in that case I do find it notable that photos of both the TVC J-10 and WS-10 powered J-20 have since emerged, while the TVC J-20 has remained conspicuously absent. Which could mean the author of the cartoon misidentified the serrated WS-10 for the TVC variant on that one occasion and it doesn't in fact exist, or publishing a drawing pushes the limits of what he can release - which in turn would fit the pattern I'm postulating. It's ok to show the nozzle per se, but acknowledging its connection to the J-20 is considered sensitive and can at best be done indirectly.
It's not like the LOAN design used on the F-16 was exactly identical to what ended up being employed on the F135.
The F-16 nozzle lacks the RCS treatments round the airframe interface (but that's an airframe rather than engine-driven difference) and has a divergent section of conventional length (again related to the host aircraft, as VTOL was not required). Available imagery of the test nozzle makes it hard to be certain, but it *appears* as though it may have one petal less (14) than the production version on the F-35 (15). That could be engine related, as the F135 is significantly larger in diameter than the F100 - whether the same applies to the WS-10 and WS-15 is not such a clear-cut case though.
It's a question of specific thrust: in the former case, you have two engines with virtually identical bypass ratio (though somewhat mitigated by a 600-700K increase in turbine inlet temperature) where the final application delivers more than 1.8 times the thrust of the early-model F100. In the latter pairing the thrust ratio is more like 1.5 while the WS-15 may well *halve* the BPR (though the TIT increase will probably turn out to be less steep). In any case we know they are close enough to fit the same basic aircraft whereas I doubt a F100 can sensibly fit in a F-35 no matter the extent of the modifications.
And anyway, the hypothesis does not absolutely require the J-10 TVC-nozzle and the WS-15 nozzle to have exactly the same petal count - so long as the numbers differ from both the AL-31F and "stealthified" WS-10, it remains compatible with gongke's comments. I'm not sure we can take his statement as meaning the nozzle people have seen (without realizing that it is related to the WS-15) is absolutely identical to the final WS-15 design, rather than just the same in basic concept. I'm sure people have referred to the LOAN test nozzle and the final one on the F-35 in a similar way.
In fact, can't gongke's petal counts be interpreted to mean the TVC J-20 doesn't exist (at least not unless we accept the engine really is a WS-15 already)? The nozzle on the J-10 test bed almost certainly has fewer petals than he attributes to the WS-10 variant in the J-20.