Almost all the pictures below are fan art and the warrior whose CHICOM is invisible only draws "should be".
By the end of the 1990s, the Western Intelligence Agency identified several Chinese 5th generation combat programs as codename J - XX or XXJ. Chinese air force officials confirmed the existence of such a plan, they presume that the plan will be used during 2017-2019. However, Robert Gates argues that by 2020, the "advanced stealth combatants" in the United States may be twenty times that of China. By the end of 2010, two prototypes of Chengdudu - 20 have been constructed and tested at high speed. The J-20 made its first flight on January 11, 2011. On December 26, 2015, a new J - 20 with a serial number 2101 jumped out of the Chengdu airline factory. It is considered to be the beginning of Low Speed Initial Production (LRIP) aircraft. 2101 made the first flight on January 18, 2016
J - XX / J - 20 is a large fighter of almost the same size as F - 111. This first aircraft has a large dihedral wing wing delta configuration and all moving vertical / horizontal tail wings have a pair of outward / backward slopes, having the same size and outwardly inclined ventral fins / strips I will. If it is moving like a tail and any production version remains, it will provide some very advanced capabilities regarding controllability and operability. No doubt, this configuration is designed to provide excellent sustained supersonic cruise performance with proper engine type and excellent maneuverability in transonic and supersonic mechanisms.
The planar alignment of the J-XX / J-20 shows the exact angular alignment between the canard and the delta front and the exact cross (starboard to port, port to port) angle between the canard and the triangle trailing edge Alignment is shown. The leading edge scan is about 43 °, which clearly is used for efficient supersonic flight. The People's Liberation Army does not reveal the type of engine. Some people claim that Russians offer 117S series engines with super cruising function, but depending on the overall efficiency of aircraft aerodynamics, these are the ones to maximize the performance of this advanced aircraft It may be insufficient.