In taking a quick look at US navy aircraft of WWII and later, comparing the radial piston engined Grumman F8F **** cat with 2250 hp, 7650# empty wt, 455 mph max speed and the later Grumman F9F turbojet with 8500 ft-lbs of thrust, 11,866# empty, and 647 max speed it is interesting that they (the planes) are in about the same sized (L x W) package but you get a lot more performance from the turbine. Course variables exist like shaft losses and blade efficiency and all that but assuming designers gave it their best shot at the time, it's an impressive difference.
Course fuel consumption would be an interesting parameter to look at using 100+ octane AV. gas vs JP-4? (Kerosene) and price per gallon. Guess one could look that up if all that interested.