maglomanic
Junior Member
The point is ability of the DSI to sustain the conditions involving Mach 2.0. DSI in no way hinders a plane reaching Mach 2.0.F-16 - mach 2.0? Maybe when it's flying with no payload. F-16 really struggles reaching that kind of speed. As for JF-17, it will struggle too, because it uses a fixed inlet like F-16 and F-35. If you look at the fighters that can reach extremely high mach speed, they can all fly at really high altitude and use variable inlet. JF-17 does not display any of those traits. I remember reading how the variable inlet on J-10 allows J-10 to maintain thrust level at high supersonic speed. As I mentionned, unless JF-17 wants to get a complex intake like that of J-10, it's not going to touch mach2.0 anytime soon.
I have maintained all along and i will repeat it again. There is not need for JF-17 or even F-16 to go over Mach 2.0 atleast in the theater where PAF operates. People who amuse themselves with such ideas are doing just that.Amusing themselves.
For most cases all you need is a faster rate of acceleration than a max ceiling in terms of speed.
But to justify racially motivated insults based on the nonesense that is posted by teenagers on PDF is not acceptable atleast to me(and i am certainly not pointing or attributing it to you so dont get me wrong). What do you think is the level of thinking of the kids who come up with these kind of ideas? And i am sure you can find individuals on PDF who are more saner than that. For that matter and you pointed it yourself that alot of Chinese boards are filled with CGI's and fabricated stories of PAF pilots flying J-10 and praising it . This doesnt lead me to generalize and insult Nationalties. The right way is to correct them on technality and give sound reasons.But as for this converting JF-17 to J-10 stuff, I think this kind of thought does get mentionned quite a bit on PDF. And yes, I have definitely read stuff about converting JF-17 to use two engines.
And i have to commend you for being patient towards alot of such kids on PDF, infact even i lose it with some of the kids who just argue for the sake of argument.
If you are talking about twin engines then you are trying to convert a beleiver! Please read my post what i think of such suggestion.I am in complete agreement with you hereYou have to think about the cost involved in this development and what extra development would do to the per unit cost of the plane.
In order to enable higher payload it would need better thrust to weight ratio. That would definitely increase the manuverability at lower loads. May as well bump up speed to 1.8 from current 1.6 (not that it matters much for PAF).For what it's worth i think it is already manuverable enough in yaw. A little increase in thrust will help it's pitch charcterstics as well.JF-17's flight performance has pretty much been set after prototype 04-06. I don't see much more improvement in flight performance after the airframe is already finalized. If current generation plane is any indication, improved multirole capability, increased payload and improved avionics seem to be where upgrades are going to.
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