The supercruise claim in the article is just a recycled belief that comes from a simplistic laymen understanding of how supercruise is achieved. It’s not a claim built on any actual understanding of physics. The truth is you can’t tell anything about whether a design can cruise at supersonic speeds with just its dry thrust by looking only at how powerful the engines are or looking at the T:W ratio.
In an atmosphere all objects hit their top speed when the force propelling them forward matches the force of air resistance pushing them back, so that their acceleration nets to zero (if this sounds familiar to some people that’s what terminal velocity is).*** Thrust tells you how much force you have to push an object forward, *but* it doesn’t tell you how much air resistance that object will need to overcome. The force of air resistance goes up as the speed of the object increases, but *how* much it goes up by depends on the density of the air, a drag coefficient which is defined by the *specific* shape of the object, and the frontal area of the object along the face it is traveling forward in.
If you have two objects of the same volume but they’re shaped differently (and maybe have different surface treatments), some combination of different frontal area and different drag coefficients means that one can have a lower air resistance curve than the other at the same speed, and can thus hit a higher top speed with the same amount of thrust (I’ll leave air density and altitude out of this explanation, but if you jut think about it a bit how they factor in is pretty straightforward). There’s an additional complication once you hit the transonic and supersonic regime because the drag coefficient changes, but the same principles hold. What this means for our particularly discussion here is that if a combination of the J-20’s drag coefficient in the supersonic regime and frontal area keeps the overall force of air resistance lower than the total amount of dry thrust its engines can generate, it can supecruise (or, if we define supercruise more narrowly being able to effectively engage in cruise flight in the supersonic regime, it can go supersonic without afterburners).
Seeing as the drag coefficient can’t be eyeballed, no one can know with any claim to honest fact whether the J-20 with interim engines can supercruise unless someone sticks a J-20 model into a wind tunnel or a CFD simulation and tells us that to be the case with very detailed aerodynamic analysis. What we *can* say is that even if it can supercruise, or at lesser reach supersonic speeds, with its interim engines it can probably supercruise better with more powerful engines, and whatever its performance in that envelope of flight is right now it would almost undoubtedly be better with better engines. In addition, we do know that at least the original design study of the J-20 said its basic design would allow supercruise with weaker engines, and we now have at least some circumstantial evidence from the stories about these traininf exercises that the J-20 can indeed hit supersonic speeds with just its dry thrust, and perhap employ effective supersonic maneuvers for combat powered under dry thrust.
The other stuff in the article you shared about “setbacks” because the intended engines aren’t ready is just (I would go as far as to say shameless, disingenuous, and morally self indulgent) spin over basic information that’s already been known about for years (except the claim referencing back to the SCMP piece about the WS-15 exploding during testing in 2015, which we’re all still a bit dubious about since we don’t have ways of substantiating the claim), hence the dismissive response of many members in this forum.
***There’s an additional factor that can limit top speed with objects powered by jet engines, where the speed of the airstream going into the engine inlet matches the speed of the airstream the engine can push out, since if the speed of the airstream going in is as fast as the speed of the airstream going out then no more work (and thus thrust) can be extracted from the airstream, but we can ignore that when discussing most jet fighters that are designed to go supersonic.