View attachment 358634
Could
@Asok be the white knight once more?
Actually my point is people advocating for the use of the Chinese engines would not be so unwise to put every thing they have got on the line. And even they were, they certainly would not have chosen the bet on the J-20 with which the secret could not kept for long. There is no needs in this, it is not the end of the World for the PLAAF even the Russian engines are still used for J-20.
The problem of we fanboys is that we know so little or none in the field of aeronautical engineering and we don't have inside sources of knowledge to based our judgements. In any field, there are certain common things that if we were professionals, we would completely rule them out, while outsiders are clueless about them.
So if we found someone who have a track record of non B.S. knowledge, luck for us. I would go to him directly.
"刀口" or Daokou is such a person. He is obviously a long time military fan and has accumulated certain amount of technical knowledge, although still may be superficial.
What clued me in that J-20 CANNOT have used non-WS-15 engine for testing for the last 5 years is that only it could allow J-20 to test Supersonic Cruise and Supersonic Maneuvers. This is the two of the four 4S. Superior Supersonic Cruise and Supersonic Maneuvers are two of the main reasons that F-22 is hard to defeat even in close range combat.
If PLAAF can't test Supersonic Cruise and Supersonic Maneuvers, there is no way they will accept them into the production or even pre-production phase. Supersonic Maneuvers test the structure strength and flight control systems to the Max. J-20 has 8 differential control surfaces, Canards, and TVC nozzles. A very complex, sophisticated and advanced control system is required. They probably take the longest time to develop and most dangerous, since it is software control, you can't determine the outcome by pure logical deduction or visual inspection. It must be thoroughly tested in ALL combinations of scenarios and situations.
I am a software engineer. I know "ALL combinations" means. It means a
humongous number of scenarios. Every time, you had made a change. You have to test All the combinations again.
For example, if you have Speed (stall, post-install, low subsonic speed, high subsonic speed, supersonic speed, maximum speed), Attitude (Sea level, low attitude, medium attitude, high attitude, maximum attitude), Weight (empty weight, combat weight, maximum weight), you would need to test various combinations of these (17) factors.
"Combinatorial explosion is a fundamental problem in computing. It is the problem that the number of
combinations that one has to examine grows
exponentially"
So testing the flight control of J-20 is a huge task, and you can't even begin to test it, much less test it thoroughly, if you don't have the engines to enable J-20 to do sustained Supersonic Maneuvers.
This is one major reason Yang Wei, China's foremost Flight Control Expert, is the Chief Designer of J-20. Only he could understand how to fully test the Flight Control and Structural Integrity of J-20 to the Max. The Complexity of the Flight Control System has came to dominate the complexity of the 5th generation plane. Movable Canards and TVC nozzles have seriously complicated the flight control. This is reason why only in the 1980's was the Engineers able to used them successfully, because before that time, there was no computers powerful enough to control them.
Software, massive amount of code, is the Genie and Devil lurking in modern airplanes.
To test the Flight Control System means to find out the extreme limits of the Structural Integrity and Aerodynamics configurations and how the system will response to it.
This is very ticklish. It means you want to push the plane and pilot to the limit without falling down from the sky. Many planes were lost when they cross this boundary.
So when I was reminded by "刀口" or Daokou, who likely was informed by a professional engineer or insider about this problem, this settle the Engine issue for me.
There is no way could J-20 use a different engines (because they can't do Supersonic Cruise and Supersonic Maneuvers) other that WS-15 for testing. While the superficial similarity of the engine petals could be explain away as engineering choices, like all cars have 4 wheels and one steering wheel, but no cars have one wheel and 4 steering wheels.
There is no reason why WS-10, AL-31 and WS-15's petals MUST be totally different, and CANNOT be similar.
None could I see.
Those people who are stuck in this thinking must supply the reasons as evidences as to WHY they can not be similar, not merely keep pointing J-20's petals are similar to WS-10 or AL-31.
They can be similar, got it? Unless you could come up with strong reasons, why they can not.
The explanation that J-20 used an early model of WS-15 with petals superficially similar to WS-10 and AL-31 is the most plausible explanation to me.
No one has come up with a reason that COMPLETELY-EXCLUDE this possibility.
People have demanded that we come up with evidences or reason for being Pro-WS-15, I now demand reasons, why J-20 COULD-NOT-HAVE-POSSIBLY used WS-15 already.
The excuse that it is possible J-20 have used WS-15, but not probable is seriously lame.