anyone on this site has a makerbot or some sort of 3d printer? since there is so much debate on the canard, why not just print a 3d model of it and test it in a lab. that way we all know whos right. none of us a experts here, we all can find some sort of evidences supporting our beliefs. But at the end of day, no one is right because no one can physically prove it.
If it were intended as a serious stealth design, why would they stick canards on the thing if they didn't think they could make it stealthy?
at high speeds, aft-tail reduce drag, J-31, F-22 and F-35 use aft tails because of drag during supersonic trimming, add more drag you add more deflection.
Aft tails are easier to hide behind the wing thus reducing RCS.
Shenyang went for aft-tail because in RCS and drag, the design reduces RCS and drag.
Shenyang`s J-31 design will hide better the aft-tail from enemy radars than J-20 its canard specially with the dihedral they have and large size.
Pretty much canards by increasing drag and being less effective at supersonic speeds they requiere larger deflections.
Add a long couple canard, you reduce drag, thus deflection, but you also reduce lift at high AoA.
Eurofighter`s canards are radar reflectors that give it away easily on radar
Dude... are we really doing this again? Just stop posting please.
A flying scale model proves nothing of the sort, and distant coupled active canards for primary pitch control will increase your RCS from the frontal aspect. The only true measure of RCS is the Radar return from your full scale prototype, anything else is conjecture. Its quite doubtfull that any one who doesn't need to know has any idea of the J-20s RCS outside of Chengdu and the PLAAF, and the Swedish model bears a mild resemblance to the planform of the YF-23, with the addition of the canards. I will say that the model flys fairly well, without the usual jerking and jinking of a small scale radio controlled models. This model would however make quicker pitch transitions due to the center of lift being located further forward near the center of gravity, and does demonstrate the principle of mass centralization, which does lend itself to relaxed pitch stability.
Stop here little bro, you've brought up some decent points so just leave it here, I saw Vader Stomping around on the Plan carrier thread. This new design by Chengdu is just keeping up their family tradition.
Shenyang went for aft-tail because in RCS and drag, the design reduces RCS and drag.
This is a load of rubbish. Size has nothing to do with the purpose of an aircraft. As an example, the Su-27 is larger than MiG-29 but the former isn't a striker. The use of long coupled canard does not make an aircraft a bomber, as J-10 uses long couple canard and is an air superiority fighter. Western analysis typically have no idea what they are talking about.look, canards are trimming devices, at supercruise, which is the ideal speed of a 5th generation aircraft, the aft-tail has no disadvantage over canards in fact the aft-tail reduces drag.
On designs like B-70 ot T-4, you have a long coupled canard, as a trimming device too but remember these are bombers and long couple canards are usually set on bombers, that is the reason some western analysis claim J-20 is a striker included the US air force magazine, compare J-20 to J-31 and you see a big size difference more in line with a striker.
Shenyang is incompetent, so their design philosophy is to base their design on somebody's else design. It is not an example of a superior design.Shenyang J-31 uses aft-tail and here i put you a chinese example to show you, that in China there are different design philosophies.
So you can not say i am bias.
J-31 in the other hand is smaller, has an aft-tail, with no dihedral, hidden frontally by the wing, in line with the F-22.
J-20's relax stability combined with use of long couple canard means minimum deflection can result in large moment. The vortex produced by LERX reinforces the vortex from the canard, which increases lift at high alpha.here you have the myth that the flight control system will lock the canard deflection at supercruise, when in reality at supersonics speeds the deflections will automatically increase to be fair that deflection also increases on aft tail designs, so canard always will requiere more deflection and thus RCS will increase.
J-20 has relatively long couple canard trying to reduce deflection but this reduces lift at high Alpha.
Shenyang went for traditional configuration because the company is not competent enough to make a design with sophisticated aerodynamics. This hardly constitutes as a proof that traditional configuration is more superior. Furthermore, 310 is just a private venture and not China's 4th generation air superiority fighter. That title belongs to J-20, as it is that Chengdu won the contract.Stealth design requieres the wing and tail to be coplanar, J-31 uses that rule, J-20 breaks it, Shengyang went for a more traditional approach for that reason, why? because chengdu fell into contradictions, the canard should be coplanar for stealth, but above wing level for added lift.
Shenyang on J-31 used a more conventional but more effective way of reducing RCS than Chengdu`s J-20
Song's paper says nothing of the sort. In fact, the paper contradicts what you've said by saying J-20 configuration has good supersonic drag and excellent stealth characteristics.Song`s paper even says that, the need to be coplanar is a stealth requierement
The design team made a future fighter proposal based on the points raised by this article. The proposal employs lift-body LERX canard configuration. It is unstable in both the lateral and yaw directions. The proposal employs small aspect ratio wings with medium back sweep angle, relatively large dihedral canards, all moving vertical stabilizers far smaller than those on conventional fighter aircraft, and S-shaped belly intakes. According to our assessment, the proposed aircraft will have excellent supersonic drag characteristics, high AOA lift characteristics, high AOA stability and controllability, and excellent stealth characteristics.