Because Chinese fighter industry is relatively lacking in experience of conducting a full design cycle for both a modern fighter turbofan engine and an modern high performance fighter airframe, it would have been preferable to conduct most of the prototype validation and pre-series development of any indiginous fighter using something close to its intended engines. This way any fundamental issue arising from engine/airframe aerodynamic incompatibility would have the opportunity to menifest itself early, and could be addressed while the opportunity still exists to make fundamental changes to the airframe before any large upfront investments in production tooling, with reduce impact on production schedule.
So it would certainly not have been ideal to so pace the fighter program as j-20 appear to have been paced, which is the final intended engine have not yet flown, while the fighter it is intended for has already gone through its main development phase, and production tooling is undoubtedly already finalized and possibly already manufactured.
This suggests WS-15 was originally intended to reach flying prototype stage by around 2010, and be flown with the first j-20 prototype. The fact that engine has not yet flown suggests the engine is well behind intended schedule.
Not sure about that -- if a bottleneck for a particular subsystem exists but other subsystems are ready for testing, then I think it would make sense for development to continue with those other subsystems, while also designing the aircraft with specific knowledge that it will eventually have the one delayed subsystem replaced in due time.
That way you get to test your other subsystems and your airframe and also an earlier initial capability, though your aircraft will have substandard performance WRT, compared to intended performance with the intended subsystem.
Better than having to wait until
all subsystems are ready to start testing, which may cause a major delay in all subsystems and domains of the aircraft.
I don't think any disagrees with the idea that WS-15 is delayed,
relative to the other subsystems and the other domains of J-20's development. But whether it reflects problems with WS-15's development, or whether it reflects that the other domains of the aircraft and its subsystems were developed faster, or maybe a mixture of both, is another matter entirely.
While I agree that it would have been "preferable" for J-20 prototypes to have been fielded from the outset with engines similar to WS-15 (or even WS-15 itself), I don't think that was ever a serious expectation. In fact even in the early to mid 2000s when J-20 was still called J-XX by the PLA watching community, it was accepted that J-20 will initially be tested with interim engines and that the first batch may even enter service with interim engines.
The question basically comes down to whether the air force and/or CAC had scheduled WS-15's development knowing that it would not make it in time to equip initial J-20 prototypes. i.e.: were interim engines always part of the plan? That could have significant implications for what kind of trials and testing they are focusing on and which ones they are not, in this stage of development.