Is WS-10A uses in J-20?? Anybody can do photo comparison of the nozzle of J-20 between FWS-10 and AL-31 on the J-20 one??
At first, I don't think it is a WS-10"A". WS-10A is famous here because TG(that's what Chinese fanboys call China, it's the acronym of Chinese "Party's State") means you to know: You know WS-10A because it was showed in Juhai, and it was showed in Juhai because it is designated to power J-10 and is supposed to be exported with J-10 some day later, not because it is the latest achievement China has made so far.
As for the nozzles of J-20, they looks like ejector nozzles but not as the same as WS-10's. The outerwear petals of a WS-10's nozzle are short and wide, but the J-20's are short and thin.
An AL-31F/FN's nozzle is a convergent-divergent nozzle, the petals look like long and thin, they are divided into two sections and articulated together for the purpose of convergence and divergence of the exhaust gas.
Theoretically, you cannot directly use a 3G engine on a 4G bird because the stealth design is against aerodynamic performance. You need higher T/W ratio of engines to increase the thrust without increasing weight.
The engines might be two derivatives of WS-10 with T/W ratio of 8.5-9 or two WS-15s if 117s have been ruled out.
If the engines were WS-15s, I would think the chief designer was too bold and it was too risky. If the engines were AL-31s or WS-10A, the plane would be underpowered, though it would be no problem to use a pair of AL-31s or WS-10As for the maiden flight. But I couldn't explain why the nozzles looked like neither AL-31's nor WS-10A's if the engines were AL-31s or WS-10As.
If you wants photos, you can google the images by using keywords like "WS-10A", "AL-31FN", etc.