Dear
@messiach and just as a pretext to this post, I would like to note that I don't want to offend you in any way, I admire your knowledge, I'm more than glad you are back but during the last few weeks, I have some serious issues and this post is a prime-example!
Please explain, where you see a "higher aspect ratio - for lift and maintained endurance" on the wings or any of these details that allegedly "have been optimised to reduce drag which induces an apparent change in wing clearance" and even more changes on the "mid fuselage is smaller as rootlets expanded ... posterior fuselage looks a bit smaller in a diff"! Please show it by comparison with other suitable images of regular Block 2 JF-17s or at least mark it on an image so that we can check for our-self.
In fact - and I'm quite sure several other members here too - see NOTHING, I see no major new wing with wider span, a different and especially not higher aspect ratio or greater ground-clearance, I see no major changes on the fuselage, which would allow a conclusion towards a different engine, higher mass-flow or whatever. Please don't interpret this as ignorance or arrogance or bias, maybe it is a lack of technical understanding, lack of eye-sight or whatever or indeed your knowledge, but PLEASE explain it since at least I truly want to see and believe it, most of all since such major changes at least IMO make no sense. A new wing, a different, redesigned fuselage, a taller gear and so on are no minor changes like an added RWR ow MAWS and as noted I neither see any visible changes nor a reason for such a major redesign, since it would require additional time consuming tests and certification.
Again, please don't take this post as an offence or critic, but only as a desperate request for more information and proof since I want to lean, otherwise any such claim will still remain as mysterious and unbelievable for some here like claims the PAF will get J-15, J-16 and J-20.
Kind regards,
Deino
@Akh1112