Deino
INT'L MOD
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I actually believe (from my limited knowledge of aerodynamics) that the J-10 is superior aerodynamically to the J-31. I say this because of some variables like:
1. Superior wing loading
2. Delta canard design
Care to explain since when a delta canard design is per se an aerodynamically superior design? Neither the F-22, the Su-57 or Su-27-series are delta canards and aerodynamically quite superior design to many other types including delta canard designs?