Engine thrust is determined by two elements: mass flow (ie how much air is going through the engine) and exhaust velocity (ie how hot the air is).Why the JSF engine is so extremely noisy compared to the other aircrafts is truly puzzleing. Perhaps someone may shed some light to this?
The F135 for the JSF has been designed to have increased mass flow compared to the F100 in the F-16. This is because the JSF in its F-35B version will be a VTOL aircraft. While the F135 engine exhaust will only provide about half of the F-35Bs vertical attitude lift thurst (and operate at under half overall power) it is very important that this thurst be of high mass, low velocity. Hot air is the worst thing you can pump in a VTOL configuration. This is why the Pegasus on the Harrier wouldn't look out of place hanging on a 767 because of its huge fans compared to the much narrower F-16 F100 (both engine's producing roughly the same thrust).
So does this mean the JSF will be louder? Considering the F135 has a lot more thrust than the F100 it shouldn't. Becuase exhaust velocity is a major cause of noise.