J-20 influenced by the F-35? you guys mut be kidding right?
Just because China got some papers from the JSF does not mean the actual plane was “infuenced” by that data.
I’m sure neither the 144 has something to do with it.
Way too many differences, both the F-35 and 144 are completely different from the J-20.
I like this plane in some aspects, on some others I dislike, so is nice to discuss about it, but saying the J20 was “influenced” from something else is the same arrogant assumption, without any kind of fundament or solid fact, that typically comes from some idiots that believe only few have the word’s technologic monopoly.
This program is completelly indigenous.
The Su-15 is truly a very fast aircraft, and can keep a very high speed a a decent range, I believe that they would not have trouble intercepting the 52.
For these kind of interceptions the “macro” view is quite important, since is not a dogfight, everything is important, the aspect of the target, the entrance speed, the heigh
They probably will do a dive, then a very accelerated climb before reaching the target, then a turning (or probably the whole manouvre while doing a slight turn – pilots should be “blind” doing this, but the ground control should help them a lot), and then a dive over the target coming from back..repeat the process.
The Su-15 IMO is the best interceptor ever created,is even faster than the F-104, and as a whole much better than the Mig-25.

I think we can see in this picture that both, the LEVCON and the slat have different incidence.
Probably the LEVCON is acting as a canard rather than another slat, would be interesting to read a comprehensive analysis of its aerodynamics, since among the 5th gen planes, IMO, the PAKFA is the most advanced on that field.
I’m, not sure yet..hopefully we will read something more detailed about it.
Regarding the engine incident, people is taking it too lightly…it was a very serious incident.
And why they should be desperate?
The program has political support, if LM had the possibility to show the F-35 one year after it first flight they would do it.
Same for the F-22, a program that was under heavy attack…any good public show had helped.
Or do you believe that uncountable TV shows, pictures etc..is not the same thing that showing the product in a public show?
The difference is..trust.
Times changes, we are not in the cold war anymore, now is matter to show the product and search for customers.
And to keep the program alive.
So if russians trust in their plane, they will show it.
They had the option of showing many pictures, telling many tales, and recording many TV shows.
But they trust in their plane.
BTW, the J-20 media exposure has been impressively extensive for a communist country..then again, times change.
Another aspect, its active interference for coming missile is really amazing, here I am seeking more information about it.
What is your source for this?
I’m still amazed how the Candid is that thirsty of fuel…probably lack of room for fuel?
The Il-96 could be a nice alternative, but we don’t know what kind of restructuration would need to handle the antenna
The Il-96 seems to be way too big for this task as well.
Empty weights
Il-76-70-80TM
E-3-70TM
And the Il-96 with a whooping 120TM…no thanks, way too much trouble for an AWACS 🙂
It’s actually almost the same size (diameter & thickness) as the E-3 radome,
JSR is probably right guessing the new antenna is much bigger, because it seems that the new plane will carry 3 AESA/PESA antennas while the E-3 is just a rotating one.
Things get worse if the antennas are AESA with all the cooling issues.
The An-70 probably can’t handle the antenna and the subsystems needed for 3 arrays.
And probably no other russian aicraft would.
Why is this aircraft consuming so much fuel? are it engines that thirsty? because I don’t believe aerodynamics is the main reason.
Since the Il-96 is larger overall and has a bigger fuselage
The Il-96 won’t do the job, don’t confuse doctrines, because Russia is not NATO
NATO docrine is to bully small nations on preemtive strikes, that’s why all their planes need fancy airports and a lot of support.
Russian planes need to survive a nuclear war
T-50-2 LEVCONS and slats leading edges seems to be painted with something..RAM?
No sign for diffrencial LEVCON driving yet, at least to me.
These doors gaps seems to be intended and not accidental, these gaps will be there in the production plane IMO, probably will be filled with plastic, rubber..or something…but IMO these gaps are not bad manufacturing finishing…are meant to be there…and I’m thinking a couple of reasons why they are there.
Tell me – what does a radar blocker look like? What does a fan and stator row look like? What are the main differences?
Would be awesome if they manage to integrate blockers in the engine itself, but I think it would be inpractical too, the blocker will be an independient device, I think is already confirmed
If the enemy has managed to push deep enough through your defences to hit AWACS bases,
In a nuclear conflict there will be no big airfields left.
Soviet and now, Russian doctrine is heavily based on the capability to withstand a nuclear first strike, so I think the Il-76 is still the best option.
I don’t like to make childish commentaries, but this aircraft truly rocks…that picture is awesome.
Until now I’m thinking LEVCONS are slaved with the slats, things changes a lot if they can be differentially moved, now there are three possibilites
1-The levcons control is independient with the slats
2-The slats and Levcons can be differentially moved
3-Both
I don’t recall that slats can be differentially driven in another airplane or fighter, please let me know if so.
Now the BIG question remains
Are the Pakfa Levcons act as canards or are just big slats?, both are quite different.
Regarding the exhausts, I think since the program has started with a 3D TVC, IMO is very likely the production T-50 is MEANT to get a 3D TVC, because all the program, all the requirements and all the airframe was designed and tested with this kind of device, so the rounded 3D TVC is here to stay.
If indians want their exhausts ala Raptor…well, is their problem, go and pay for that garbage…
But I think russians are not that dumb.
That makes me wonder if an S-duct would actually help pressure recovery at supersonic speeds?
This should be OK for supercruiser, at determined velocities, but not good to achieve higher speeds, this could be the definitive answer why the 22 is limited below M2, because despite the S-duct could help at, let’s say M1.5, at higher speeds the pressure keeps constant or is increased, while intakes flow velocity decreases or stay the same.
Care to explain why DSI would prevent supercruising?
Well, everything depends on the shape of the DSI, I must elaborate this, CARET system should be much better suitable for a supersonic-supercruiser plane, because it can adapt much better in the different transicion stages, from M1 to M2, CARET should be better for different supersonic manouvres, heights, etc, while DSI is a ‘fixed’ CARET, and adapted at ceirtan margins only.
Can you design a DSI for M2? yes sure, but this DSI wont work well at, for example, M1.2, neither maneuvering at M2.
The point is that there are more things for the supercruiser requirement than just doing M1.5 on dry power
BTW, why the J-20 color is that dark grey? is there other chinese plane painted with that color?
Maybe are testing RAM coatings already?, would not be surprising if the J-20 is ahead the T-50 in its testing schedule, still not impressive performance shown though, also that canards demand is suspecting.
The T-50 is the 5th gen plane that looks more ‘sportish’, the J-20 looks too mean, and the F-22 too formal.
Also its rear part has it charm haha.
since they admitted CARET is the future, which Boeing adopted as a layout for NGF’s inlet, leaving them few options but to design sth F-22 alike with additional foreplane.
I believe they went with the DSI because supercruiser is not a requirement, and the whole aerodynamic configuration would be OK for supersonic dashing, but nor for supercruiser.
I told them that air-intake F-22 aplied is curved so toughly that banned F-22 from speed beyond M2
Ok, ok, this is interesting, and escaped from my mind, are you talking about the speed flow loses?, meaning that the curved intake decreases the input flow velocity?
Now thinking about it, is highly likely, because yes, the s-duct is very curved turning the speed into pressure, decreasing the flow velocity that goes over the compressor.
What is going on with the Berkut? any news about it?, with all the attention over the T-50, the berkut has been forgotten, and while the PAKFA is a way more practical solutiion, the S-37 is still a promissing design.
Yeah, we should respect this kind of serious work. These simulated evaluations are way better than just look photos and talk:D
As far i have read the simulation is done with the conventional optic-aspect procedure.
This is why when you increase the GHz in the test, the plane becomes more ‘stealthy’
This is not true in a real test