Yes, that is what I said, and the fact is the J-20 has poor wing geometry.
And explain this "poor wing geometry". The sweep angles are consistent. Delta wings provide less drag and improved transonic and supersonic flag. Explain the "poor" aspect of the J-20's wing geometry.
And yes, some credible links would be nice.
Right, and the J-20 has a smooth 'underside'? It doesn't have four large objects, most likely hydraulic mechanisms) hanging from underneath the wings?
That's not part of the centroplane ("the fuselage") I was referring to.
Compare the undersides of the fuselage of the J-20 and T-50.
http://www.chinasignpost.com/wp-content/uploads/2011/01/J-20-underside_CDF_16-Jan-2011.jpg
http://www.worldaffairsboard.com/at...20637d1272853204-pak-fa-news-t50_img_1472.jpg
The former provide better stealth from that aspect.
You will provide a credible scientific source (not a magazine quote or blog quote) explaining 'panel alignment', than you will point out and be very specific where the J-20 has 'panel alignment' and where the pak-fa lacks 'panel alignment' than you will give an explanation as to why it is important, than you will make a quote from your credible chosen source that supports your claim.
Alignment and angling of access panels and door edges with the rest of the aircraft are necessary to avoid much radar return.
F-22 Stealth
A close look at the T-50:
http://www.ausairpower.net/Sukhoi-T-50-PAK-FA-KnAAPO-2BS.jpg
The access panels on the T-50 are not aligned with the sharp edges of the aircraft or with the edges other bays.
You do not see much of this problem on the J-20 and no sign of this problem on the F-22.
Same routine, as above ,but what is most delightful and plainly ignorant on your part is that the F-22 also has these 'gaps around the inlet'. Reading too much of Martians propaganda?
Please, I would like for you to explain yourself out of this one, here are those 'gaps':
Seems like you and Martian know better than the two largest and most experienced aircraft manufacturers in the world, correct?
Never said that the F-22 didn't have this problem. In fact the F-22 also to some degree possess this problem, as with the T-50. However, the YF-23 and F-35 don't.
You can't possibly possess every advantage of every RCS reduction measure and not inherit some disadvantages. It's all about balancing and focusing on the role of the aircraft.
Here is the YF-23 intake:
http://www.aim120.com/image/IMG_0609.jpg
You wanna hear what's propaganda? Read Putin's statement on how the T-50 is "better" than the F-22.
And the four large spheres underneath the J-20's wings don't apply? I forgot, physics don't apply to the J-20. By the way, the F-22 and pak-fa have the same spheres only much , much, much smaller. I wonder why the J-20's sphere are as large.........
The "spheres" on the J-20's wings contribute negligible amounts of frontal RCS, arguably the most important aspect of RCS for stealth aircraft.
Please note that the "spheres" are not spheres, they are specifically designed to be aerodynamic and sleek in design, unlike the bulging IRST.
Don't care, half of the 'stealth' aircraft the US developed didn't have a bubble canopy.
And this "half of the stealth aircraft" never was an air superiority fighter and does not compare to the F-22 in terms of stealth.
Lets keep the conversation realistic and relevant.
Plasma stealth technology was first patented by Arnold Eldridge of General Electric. It was also tested aboard a Russian Su-27IB aircraft.
So yes, the concept is realistic.
Yes, like the Americans thought the Mig-25 was an agile fighter?
The Americans' biggest fear from the MiG-25 was its extremely powerful engine that could allow it to go at extremely high speeds. Speed alone in Cold War dogfights was very important. Agility does not come in the same package of an interceptor.
Just because the Chinese chose a delta design doesn't mean they did it for maneuverability, there are a number of delta aircraft that would get humiliated in a dogfight. And the J-11A reference just proves that the J-11 pilot was an armature or incompetent or both, in Russian aggressor squadrons Mig-23's have achieved Mig-29 kills, despite having inferior avionics and very inferior maneuverability. That same J-11 pilot wound get spanked by the Mig-23.
Delta design, again, does not boost maneuverability to a colossal extent. It is the canards that do. Delta wing configuration mostly reduces drag by removing excess airfoils and greatly boosts transonic and supersonic flight performance.
The J-11A vs J-10A exercise was a drill, not simply a 1 to 1 competition for fun. Pilots selected for these "Red Flag style" drills are not "amateurs". That's what the K-8, L-15, and JL-9 trainers are for. Drills involve professional pilots.
A good reason for the J-20's delta design was an attempt to improve the aircraft's range. While the canards may have been designed for improved maneuverability, they could also have been put in place because the radar and other avionics caused the J-20 to be too heavy in the nose, thus they had no other choice, this is the same problem early Sukhois had, until they managed to correct it.
Delta design = less airfoils = less drag = better fuel efficiency
I said that in the above paragraph.
The center of mass for the aircraft could easily have been solved by extending the delta wing forward (see the Saab Viggen). I also do not see how the nose (when its size is compared to the back) can shift the center of mass of the aircraft forward.
How many American aircraft use canards? What makes you think the designers of the F-22 would ever use canards even if it had no consequences to RCS?
The F-22 designers did in fact consider canards, but the addition to frontal RCS made them change their minds.
One of the Chinese members claimed that the WS-15 program was recently terminated.
And one Chinese member also claimed that Japan was part of China. Seriously dude, you are better than this.