Same artist did a cartoon of J-20 with two missiles in each side bay but we’ve never seen that in real life. But to answer your question, I think it was a few months.
ps: the artist implies that it is the WS-15 engine
@Deino.
ps: multiple eye witnesses in Chengdu have spotted the plane takeoff and fly around the city. Apparently one of them took a photo of the front of the plane and there has been some changes to the DSI inlets. Unfortunately, I haven’t been able to find the image.
Well? So did I hit or miss on the inlet modification speculation?
Unfortunately, researching what happened with the DSI inlets, it seems as though the inlets saw significant modification during the WS-10 / AL-31 stage. This was apparently because of difficulties in optimizing the inlets for the WS-10 / AL-31.
This implies that either two things are possible:
One: the Chinese had tremendous difficulty optimizing both for the stealthiness of the J-20 and the full flight envelope of the J-20. The F-35, in contrast, doesn't need its DSI inlet to exceed Mach 1.6, whereas the J-20 is expected to fly at least to Mach 1.8 and perhaps to Mach 2.4. This implies that without substantial inlet modification (and I'm not saying it'll happen, in fact, I'd find it unlikely), the J-20 cannot extract the full potential of the WS-15.
Two: the J-20 inlets were originally designed for the WS-15, and were then back-engineered to support the Al-31 and WS-10. That's where all the trouble came from; if the WS-15 (and this is likely) required more airflow than the Al-31 and WS-10, the Al-31 and WS-10 would then see excess airflow from a fixed (in the sense that there are no moving parts in the DSI) inlet.
I'd prefer the second scenario to be true, but it's questionable as to how effective reducing the DSI bump might be in fulfilling the WS-15's capability. The bump's job is to get boundary layer air to flow away from the inlet. A large bump implies greater effectiveness in doing so. Shrinking the bump to increase airflow would reduce the effectiveness of the DSI at lower speeds.