You realise MKI is Very poor design. Russian is the master of su-27, their su-35 final design is without canard. So you trust the Indian more or Russian more?Su-30 MKI has both canards and TVC.
You realise MKI is Very poor design. Russian is the master of su-27, their su-35 final design is without canard. So you trust the Indian more or Russian more?Su-30 MKI has both canards and TVC.
Don't you realise all your mention is prototype only? Of cos I am aware of these pLanes. Do you reLise why they did not make it to final design? The su-35 is a classic example. Do you know the finalize design is without canard? I don't want to say more.. Facts is there.
You realise MKI is Very poor design. Russian is the master of su-27, their su-35 final design is without canard. So you trust the Indian more or Russian more?
I don't think Russian will remove something useful. Common sense tells you. No need explanation. If you talk abt cost, thrust vector is more high maintenance, not canard shall be removed.Yes I did realize they were all testbeds/prototypes. I do not know why they didn't go into production -- possibly they were only meant to be testbeds perhaps?
Well when I said "russian built flankers" I meant Su-30MKI, which definitely are in production. The Su-35 claim on the other hand is irrelevant.
Unless you can prove that the russians removed the canards due to conflicts with tvc you're not saying anything.
Besides, J-20 will feature TVC too... so I suppose we should all expect CAC to remove the canards on the planes featuring W-15.
I dont think j-20 will feature thrust vector. There is no mention of it until I see one then I will believe?G
As for su-35 and MkI I don't see any different requirement. Both are design as the same role. Multi role air superiority. Different countries and different requirement is an assumption, right?
Look my point is that your claim, that canards make tvc redundant/tvc makes canards redundant, because no production aircraft has that configuration, is flawed because the Su-30MKI fulfills what you outlined. Any further claims about its effectiveness vs Su-35BM is irrelevant from the premises you've given for your overall conclusion.
Can I say canard is on su-30MKI is flaw? The canard is there probably by demand of IAF that it will give them the physical psychological of completed with everything. We are talking about India which has the least design experience of china, Russia and UK who don't opt for these combo. If you want to add in France and Sweden....
If su-35BM never happen. Probably I will accept yr example of su-30MKI. But with the su-35BM, plus it's from the more experience Russian. I am convinced Russian do not see any merit of canard on their su-35 already install with thrust vector, no matter what countries requirement.
No, there's nothing to suggest the russians did not retain canards on the Su-35BM because they "did not see any merit". You may as well be arguing that they liked the look without canards better >_>
Originally the Su-35 project did not contemplate the adoption of canards, however during the development of the aircraft at the beginning of the 1990s, the radar was installed then in development N-011M "Bars" in a prototype of the T-10 / Su-27. At the beginning it was noticed that the extreme weight of N-011M Bars affected the center of gravity of the aircraft, the radar was much heavier than the N-001 radar of the original Su-27. This compelled the designers of the aircraft to adopt some system that supported the frontal surface of the aircraft. The solution of canards appeared to reequilibrate the center of gravity of the aircraft. It was noticed in the flight of tests of the Su-35 that canards had improved the stability of the aircraft, improved the sustentation capacity, in closed maneuvers with very great angles of attack. This change made as much "success" that was adopted in other variants of the Su-27. The down side was that it increased the aerodinamico drag in supersonic regimen and even more increased the wing area of the aircraft, which resulted in an increase of the RCS of the aircraft.
Aiming at to reduce the RCS of the aircraft, the designers of the T-10 had opted to remove canards from the aircraft. But to make this was possible it would be necessary to reduce the weight of the embarked radar, with the purpose of re-equilibrating the center of gravity of aircraft without the use of canards. This was possible with the new radar that was in development and that will have substantially inferior weight to the N-011M, having had similar weight to the original N-001 of the Su-27. This minituarization of components and use of in the manufacture of the parts of lighter materials, allowed the center of gravity of the aircraft came back to be as the original Su-27, making possible withdrawal of canards of the aircraft.