F-18E/F's are smaller and lighter than the J-15. The F-18E/F's also happen to have more powerful engine (and thus probably higher thrust-to-weight ratio) than the J-15. This coupled with the lighter weight will definitely mean greater agility (assuming that J-15 doesn't use TVC). Yeah, payload will slow down both planes, but Super Hornet has a higher thrust-to-weight ratio.
If you really think J-15 was intended for air superiority, then you don't know much about aircraft configuration and airframes.
And how maneuverable are those T-10s, after all? Any numbers on the max G-turn? And the J-15 isn't even based on the T-10.
Sure, Flankers may be the "big boys" when it comes to fuel and maybe payload, but definitely not the nimble guys. The fact that it's big already undermines its agility. Guess why the Su-35s need TVC?
Super Hornets are not stealth aircraft, yes, but they have AESAs. If J-15 doesn't induct AESA, it's got a serious deficiency.
About the J-10C, yes, single-engine J-10B's won't have enough power to launch from carriers. That's why CAC took out the term "single" and put in "double" instead.
Can you at least do some basic investigation before posting?
according to wikipedia, if it is basically reliable.
su-33's Thrust/weight is 0.83, max g is 8. Su-27SK's tw ratio is 1.09, no data there about max G. But they are well-known as a type of 9G level jet.su-35 is a 10 G level jet.
Super hornets'Thrust/weight is 0.93, design load factor: 7.6 g
Saturn/Lyulka AL-31F turbofans
Dry thrust: 7,670 kgf (75.22 kN, 16,910 lbf) each
Thrust with afterburner: 12,500 kgf (122.6 kN, 27,560 lbf) each
and your powerful F414-GE-400:
Dry thrust: 14,000 lbf (62.3 kN) each
Thrust with afterburner: 22,000 lbf (97.9 kN) each
When I mentioned T-10 serials planes, I meant flankers. Did I put a K after the T-10? Whether or not J-15 is based on T-10K, it is based on flankers.
No matter how many engines J-10 will have, with chin intakes, it is not a suitable fighter to operate on a carrier. If you want to change all those things, it will be a basically new plane. Seems CAC is busy on J-20s.
One important reason France withdrawed from EF-2000 program was they wanted a fighter suitable to operate on their carriers. EF-2000 has exactly the same type of chin intakes.
Did you mean Su-35 needs TVC is because of engines are not powerful enough? Any evidence? Why F-22 needs TVC?
Since it is possible to introduce new material and new engines and ASEA radars to J-15, I can not see huge disadvantages compared to super bugs.
There is a game called 7-G which is a sim about super bugs.
And TW ratio does not mean acceleration ability, flankers with good aerodynamic shape have low resistance when flying .
Super Hornet is the slowest fighter that America built in the last 30 or 40 years. it cannot even attain a speed of mach 2.
According to wiki,
The United States Marine Corps has avoided the Super Hornet program and their resistance is so high that they would rather fly old Navy F/A-18Cs that have been replaced with Super Hornets.
It is good at changing speed to angle movement, but to gain speed again? That needs some time.