That is hilarious. The MIG 1.44 project was never intended to be low radar observable, so it is wrong to compare the J-20 and the 1.44 based upon those 'stealth' features. But then why use the 1.44 ? Why are those comparison points applicable only against the 1.44 but not the J-9 and the J-10 ? Like the 1.44, none of them were designed with 'stealth' in mind.
So if I were to use your ( silly ) method of comparing jets to declare their origins...
- The F-15 Silent Eagle did not came from the F-15.
- The T-38, F-5, and F-20 are not related. The T-38 is dual cockpit. The F-20 is single engine. The F-5 is single cockpit and twin engine. Ergo, the jets are completely discrete from conception. Also, the Iranian Saeqeh cannot be based on the F-5 since the Saeqeh has twin canted vertical stabs and the F-5 has single vertical stab.
- The F-18 Hornet has no design influence on the F-18 Super Hornet.
Walk into the engineering depts of those companies with the above arguments and they would laugh so hard they would bust hernias.
I understand you Chinese hate Indians, so just for fun, I am going to quote professor Ajoy Kumar Kundu...
"Finally, I recommend that aircraft designers have some flying experience, which is most helpful in understanding the flying qualities of aircraft they are trying to design.
I suggest even more: hands-on experience under the supervision of a flight instructor. A driver with a good knowledge of the design features has more appreciation for the automobile."
Probably...None of you even turned a wrench on a car. A bicycle ? Maybe. But something complex like a car ? Doubtful. And here you guys be, talking about military aircrafts as if you have yrs of experience enough to write a book about it.
The phrase 'fit for the purpose' engineering is appropriate here. Basically,
CONCURRENT to design is the research for precedents. See who did what before you and adopt what they did to fit your intention.
Why, despite all the advances in technology, do the airliners from Boeing and Airbus have identical layout, essentially, a cylinder aerodynamically supported by blades ? Not 'almost' identical, but really is identical. Because that design 'fit for the purpose' in more ways than most people realize. What happened to the flyign wing ? Aerodynamically speaking, it is easier to address pitch stability -- passive and active -- than it is in a flying wing design. To transport cargo, human and else, stay with what is known and proven. So just on the aerodynamic front, the flying wing is -- for now -- discarded as a viable candidate for commercial air transport. Then take in other issues like manufacturing resources or familiarity with the current technology base, the design of a cylinder aerodynamically supported by multiple wings makes eminent sense. The design 'fit for the purpose'.
Likewise with the J-20. When Chengdu sought to push Chinese military aviation to the fore, they searched for precedents to 'fit for the purpose'.
Here is how the process works...
The above flow is applicable for anything, but we can stay with aviation for now.
https://en.wikipedia.org/wiki/Chengdu_Aircraft_Industry_Group
If we look at the history of Chengdu's product lines, we can see that the company is at best mediocre in military aviation. Nothing that could be considered 'ground breaking'.
So why in the world would Chengdu start with zero in the J-20's design loops ? Even if you have unlimited money, why would you make your life more and more difficult by
NOT using precedents ? Do the Chinese prefers to do everything the hard way ?
Does it matter that the 737 has two engines and the A380 has four ? No, it does not take away from the obvious fact that both aircrafts shares identical design layout. How much more money would it take if Boeing and Airbus did not use prior designs and exploit previous experience ?
There is a difference between 'aircraft' and 'airplane'.
The dirigible is an 'aircraft' but not an 'airplane'. Do you guys know why ? That was a rhetorical question to make fun of you guys' technical ignorance. We already know the answer: No, you guys do not.
The lift method of the dirigible is lighter than air gas.
The lift method of the airplane is the
PLANE, hence the word 'airplane' or 'aeroplane'. The shapes of this plane is where we have diverse wing shapes, from the straight wings of the glider to the swept wings of the 737 to the delta wing of the Concorde. All wings are planes -- lifting planes.
What is an 'airfoil' or 'aerofoil' ? It is the 2D cross sectional geometric shape of the wing. So even if two wings of the same shape and dimensions have different airfoils, that do not make them different from the fact that both are the same lifting mechanism. Both are planes.
To quote professor Kundu -- and to spite you guys -- again...
"Previous designs have a strong influence on future designs – real-life experience has no substitute and is dependable. It is therefore important that past information be properly synthesized by studying statistical trends and examining all aspects of any influencing parameters in shaping a new aircraft...
Many types of aircraft are in production serving different sector requirements – the civil and military missions differ substantially. It is important to classify aircraft categories in order to identify strong trends existing within each class.
Existing patterns of correlation (through regression analysis) within a class of aircraft indicate what may be expected from a new design."
Note the highlighted.
Chengdu
DID NOT start the J-20 from zero. Can they ? Yes, but it would be the height of foolishness to do so.
For example...As we examine the J-20 wing design...
Of all the wing planforms available, why did Chengdu used the delta instead of rectangular or trapezoidal ? Because the world's best fighter aircrafts uses variations of the delta for its known advantages. That ruled out civil aviation as source for Chengdu's R/D plan, correct ?
How many of the world's best fighters uses tailless delta layout ? Did the SR-71 factored ? Not likely. That leave influences like the HAL Tejas, F-16XL, or Vulcan ( bomber ). And perhaps the MIG 1.44 ?
That the world was surprised by the J-20 allegedly a 'fifth-gen' fighter is definite proof that because of its mediocre history, Chengdu had to insert precedents into those process loops. Even though the J-20 have some differences from the 1.44, such as the reshaping and relocation of the intakes for the purpose of low radar observability, or that the airfoil of the J-20's delta wing is different than that of the 1.44's, there is no denying the overall physical commonalities between the J-20 and the 1.44. Saved a lot of development time and money.
In the West, aspiring aviation engineers are taught to look for precedents as much as possible, even to the point where the idea is printed into textbooks. You are saying Chengdu did not look for precedents in designing the J-20 ? What happened to the idea that 'we stand on the shoulders of giants' in order to innovate, invent, and produce anything ?
You have no problems boasting how copying and reverse engineering made China into the technological powerhouse she is today, from the cellphone to the supercomputer. But when it comes to the J-20...???
The final product that is the J-20 hints at what was inserted into its R/D development process loops: The MIG 1.44.