Which engine is better, Pratt & Whitney's F 100 or GE's F10?

what can I say? Each has its own advantages. F 100 engine is the first military engine with a thrust-to-weight ratio of 8 in the world. There are many problems in the reliability, durability and maintainability of the F 100-PW- 100 engine in use, which once put American frontline fighters in danger of grounding. In the "Fighter Engine Wars" in which the engines of General Electric Company F 1 10 are equipped with F15 and F- 16, they are at a disadvantage at first, but after improvement, these two engines have their own advantages. F 100 is worthy of the pioneering work of the third generation engine in terms of technology, materials and thrust-to-weight ratio. In terms of diameter and weight, F 100 engine is obviously superior to its backup engine F 1 10 series, but its reliability is slightly poor. Judging from the engines used by the US Air Force F 15, the US military still attaches importance to F65438. After all, the windward area is much smaller, and the thrust per unit windward area is much larger, which is ideal whether it is vigorous, accelerated or the top speed. F- 15 used in the United States and F- 100 used in South Korea. Similarly, F 1 10 is also an excellent fighter engine, but the larger bypass ratio brings a larger windward area. Although the fuel consumption is reduced, it is also very reliable and has a long service life. However, according to the bypass ratio of the second stage of the US military INPTET, the bypass ratio of the air force engine is only 0.2~0.3, while the bypass ratio of the naval engine does reach 650. The engine bypass ratio of F 1 10 is closer to the naval engine than the air force. F 15 belongs to the fighter plane of the United States Air Force, so it is clear at a glance that F 100 was chosen. So Pakistan also chose F 100.