So, I think we can all agree that the Mig29 has a number of technologies that greatly improve its sustained turn rate at high angles of attack that together make up the 4th Gen standard such as large automatic leading-edge droop flaps that drop down to allow controlled airflow to pass over at high angles of attack preventing airflow separation and increasing lift in wing camber thus delaying the stall point.
The Mig29 also equipped with one of iconic 4th generation enhancements such as the very large leading edge root extensions (LERX) that extend up the wing root up fuselage to almost the nose of the aircraft. The Mig29s are actually curved and cambered. LERX directs large amounts of airflow over the wing and fuselage at a very highspeed. The vortices generated here will not separate from the wing and fuselage easily and will stay attached to the wing well past the point stall/boundary separation greatly increasing sustained turn rate at high angles of attack without suffering any loss to lift. Mig and Su would be incapable of the supermaneuvrability without it.
The Mig29 is further enhanced being designed with an integral aerodynamic layout, where the fuselage is creates up to 40% of the total lifting force. All 5th generation fighters are designed with this layout as foundation.
The Mig29 is also actually a very decently light fighter weighing in empty at 24,000lbs/10886? With a thrust to weight of 1.09:1 right? Insanely powerful.
So, my question, why does the Xi’an JH-7A not having a single one of these technologies in 4th generation wing and fuselage design with a vastly inferior thrust to weight still able to generate more lift, higher angles of attack and sustain turns at those higher angles of attack for a longer period in a smaller turn radius over the SMT?
Because of weight??
The JH-7A’s is extensively made up of many types of composite materials, I find that it is true. However, the JH-7A empty weight was only reduced by 881lbs and the only noticeable effect was stated to be maximum takeoff weight increased by 10%, and the range increased, nothing more.
The JH-7A weighed 31,086lbs empty made up of composite materials.
The SMT is 26,6204 empty after upgrades.
So why is the SMT quite literally struggling to stay in the air being the much lighter, smaller aircraft and having the superior wing and fuselage design as well as vastly superior thrust to weight over everything that the JH-7 pretends to be?
Why aren’t the F-16 reporters freaking out over such a UFO? while its greatly heavier doing everything the SMT should do but cannot?