it is possible that PLAAF may use pakistan F-16 to flew mock dogfight against J-10A.and the article may ,which I suspect F-16A.
The F-16A has a lot less than 13,000 kg of max thrust (according to
), and you said the article talked about an F-16 with 13K kg of max thrust, so the article's F-16 should be the F-16C or F-16D (2 seater).
I read the F-16A is a superior VR dogfighter than the later F-16 jets, but the later F-16 jets are vastly superior BVR dogfighters. Apparently, the later F-16 jets acquired advanced electronics (fly-by-wire, avionics, & sensors), additional structural components, and heavier, but more powerful engines. In other words, the later F-16 jets weigh a lot more than the F-16A, so the later F-16 jets' thrust-to-weight ratio may be slightly inferior (F-16D) or about the same (F-16C) or substantially better (F-16E and F-16IN) than the F-16A jets, but their wing loading is inferior and their center-of-gravity relative to their center-of-lift is inferior. Once again, I don't know how these engines perform at various altitudes, velocities, and angles of attack. I also don't know other detailed features of these engines (response rate, efficiency, reliability, etc).
Anyhow, the F-16A has a max initial turn rate of 26 degrees/second and a max sustained turn rate of 18 degrees/second. (Source:
)
If the above info is true, and if the J-10A does have a max turn rate of 33 degrees/sec (Is this initial or sustained?), then the J-10A is a very agile jet. I read the respective numbers for the Su-27 is 28 degrees/sec and 23 degrees/sec. The Su-35 (or any Su-27 variant with canards) has better low speed agility than the non-canard Su-27 variants, but inferior high speed agility than the non-canard Su-27 variants.
But like I previously said, your source claimed the F-16 has a shorter takeoff distance than the J-10A, but I've seen a video of a standard J-10A making a shorter takeoff than any standard F-16 or F-15 I have seen.