If you knew even the most basic things about modern air combat, you would realize that firstly, the moves in that Raptor demo is worse than useless in a real dogfight (the American pilot's gleeful comments about just switching to guns and drilling away when they were talking about Indian MKIs pulling similar TVC tricks spring to mind throughout that demo), and that secondly, the Raptor was not demonstrating the agility of it's airframe with that routine - it was demonstrating the amazing TWR of it's engines.
Based on Dr Song's paper which suggested the use of TVC on the J20, it would seem that CAC at least is leaning towards the second reason, especially since they are still on best of terms with Russia and would be able to import TVC equipped Russian engines at a whim.
Post stall maneuvers require the aircraft to have good controllability and stability. After the plane enters the post stall region, however, the decrease in stability and control efficiency of conventional rudder surfaces become irrecoverable. One must carefully design an aircraft to enable sustained controllability at high AOA. Although it is possible to solve the problem of post-stall controllability through the use of thrust vectoring nozzles, the aerodynamic configuration itself must provide enough pitch down control capability to guarantee the aircraft to safely recover from post-stall AOA should the thrust vectoring mechanism malfunction. As a result, it is vitally important to study unconventional aerodynamic control mechanisms for high AOA flights.
back issue of air international ,USAF conducted mock dogfight between F-22 and F-15C,during the mock air combat, USAF discover aside from F-22 TVC allow the aircraft greater manuevility over F-15C,other tactical advantage was F-22's supercruise.
In one instant,One F-15's pilot simple unable get simulated gun killed against F-22 flying sypercruise.send a radio urging the F-22 hold steady so he can get a "gun kill"!!!!
Look what you write is pure fantasy, to start let us see the
compare the wing loading of F-22 and Eurofighter what do you find?
yes you find that F-22 has higher wing loading, despite it has a huge wing actually has worse wing loading than Eurofighter.
I know in your fantasies you expect J-20 to be as light as Eurofighter but
how much does F-16 and F-35 weight at empty weight?
answer is simple F-16 weighs 9 tonnes, F-35 weighs 13 tonnes.
I know you think J-20 has similar numbers to Eurofighter, but not J-20 is at least 5.5 meters bigger than Eurofighter and at least it weighs 9 tonnes more at empty weight.
compare the Thrust to weight ratio of F-22 and Eurofighter what do you find?
well you find that F-22 is in the class of F-15, that actually Eurofighter has higher thrust to weight ratio.
So then why F-22 having the numbers of F-15 is much better than F-15 in maneouvrability, do you want to know the answer?
TVC nozzles and internal weapons bays, yes that is the answer, internal weapons bay that reduce drag and TVC nozzles increase turn rates.
I know you are thinking your self how come an Eurofighter can match a F-22 in agility, give it fight and in dogfights beat it.
the answer lies in two factors,
Eurofighter has in a very low wing loading configuration a wing loading of 330 kilograms square meters, while F-22 something in the range of 400kg over square meters.
Eurofighter supercruises, so in a light configuration has relatively low drag even carrying external stores and weapons.
So why J-20 can not compare to Eurofighter?
The answer lies in two factors thrust to weight ratio and cross section.
F-22 is heavier than F-15 at empty weight F-15 weighs 13 tonnes while F-22 19 tonnes.
F-35 weighs 13 tonnes F-16 9 tonnes
all stealth aircraft are heavier than the generation before due to larger cross sections.
Why? first they use S ducts this increases weight, second internal weapons bays increase volume and weight.
now, stealth shaping always increases drag yes i know you think J-20 is more aerodynamic than Eurofighter, but not Eurofighter has a bullet shaped forebody like Su-27 or any missile or ICBM.
However Eurofighter and Su-27 have a disadvantage external weapons increase drag too, So J-11 or Eurofighter increase drag a lot fully loaded.
That is the reason Su-30MKI has thrust vectoring
So answer to your statement does J-20 need TVC nozzles? answer yes it does.
Because the need to carry large weapons bays, add S ducts increases weight on J-20, plus its large faceted cross section increase drag.
So to answer you why Eurofighter can compete with F-22 in agility, the answer is at expense of weapons carriage, a light loaded Eurofighter can compete with F-22 in agility but only in a very light configuration otherwise it will not be able to compete.
However F-22 is not inferior to Eurofighter but that is thanks to TVC nozzles without it the F-22 is not better than F-16 or F-15, but with helmet mounted sights more or less both are even in dogfights.
As in all your previous post, you're wrong on so many counts with all your pseudo aerodynamics theory.
If T/W ratio and TVC is all the matters, why don't they put a more powerful engine and TVC on the F-15? It should then be able to beat all the whole range of modern fighters like the Typhoon, Rafale, Gripen in maneouvrebility and turn rates.
I don't like the way you simply accuse the people here of being in a fantasy, believing in myth and other such accusations - I think there're forum rules forbidding this sort of thing.
One benefit obtainable from a control-canard is avoidance of pitch-up. An all-moving canard capable of a significant nose-down deflection will protect against pitch-up. Control canards have poor stealth characteristics, because they present large moving surfaces forward of the wing.Why the fudge would you deflect your canards unless the enemy can already see you?
If China has no 117 equivalent the Su-35 can provide an engine for J-11B and J-20