Yeah, I thought I had heard there were two, but I only see one flying, thanks paint gun. Yes challenge every body has to sell their airplanes in a market based economy, but that makes it all the more fun for us. Quickie, what Mig is saying is that all of our airplanes are compromises and yes engineers and test pilots tweak here and tweak there, but the Mig is right. We have all tried most of the configurations with computer modeling, and it is very accurate on the best programs at the top levels, you can bend tweak stretch any kind of control surface or even wings that warp and change shape, the boys in 1903 came up with that. It is funny to look back on the JXX thread about 05 an read that the J-20 would not be a rear mounted delta and would not have canards.
curious question, why is J-20 test flight so close to urban center? unless it's is part of public relation program.
They can't possibly have covered every possible aircraft configurations already. If they've everything figured out, they wouldn't have so much problem with the F-35 and the prototype testings would not take a decade or so .
Computer simulations only aid in the design of a new aircraft. The more tedious work are in the wind-tunnel testing and years of prototype flight testing. Out of the so many possibilities, there're only so many configurations that would be budgeted to go through with the design and prototype testing phases, with the successfull ones going on to production and service.
Aerodynamic designs are more than the sum of its parts.The americans have studied all these configurations thoughrouly, when they studied canting, wing position, all moving agaist conventional tail, they studied different angles sizes, positions etc etc.....
Second the US and Europe share technology and have a long tradition of aeronuatic design, this is supported by the fact NATO has common programs Eurofighter, Gripen, X-31, F-35 etc, etc...and NATO has very large military budget, add to that research done in third countries.
F-35 had aerodynamic concep with canards, canted V tails, SR-71 had inward canted canted tails, F-117 had inward canted v tails in the haveblue prototype and outward canted v tails on the production model.
So in few words if F-35 has no canards but tailplanes, is single engined and not twin engined or has conventional vertical and not all moving tail, it does not mean lockheed does not understand J-20 aerodynamics, it simply means F-35 has different design parameters to J-20
F-35 has troubles not because of aerodynamics but because of design contradictions, like F-111, it has compromised in a way some features are not well suited to different missions