Quickie
Colonel
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
Yes, we've learned a lot in the short modern aviation era, but we're nowhere near the point where no model wind tunnel testing is required, or designing an advanced aircraft is just a matter of feeding your requirement into the computer without the need for much prototype testing, or any designer, especially those with the pumped-up ego, can just say I knew of and has completely analyzed an aircraft's aerodynamics anytime a new advanced aircraft comes into the scene. Two aircrafts may share the same basic designs, for example F-15 and the Flanker, but they're also very different aerodynamically in the details.
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
Yeah, more like they wouldn't have so much problem if they knew of the aerodynamics design contradiction during the early design stage, or maybe their predicted compromises turn out much worse than they've predicted. This is another proof that no designer can claim that he completely understands an aircraft aerodynamics because we've done aerodynamic studies of every possible shapes, control surfaces, aircraft configurations, and their every possible variations thereof.
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