You are comparing the performance between a turbojet engine with no bypass air and a turbofan. both engines generate 100 kw of total exhaust power, ; are at rest, and mue22inlet and exit pressures equal ambient pressure. the engine core for both the turbojet and the turbofan passes a mass flow of 20 kg/s. for the turbofan, the total engine power is split equally between the core and the fan. the bypass ratio equals 3. assume the fuel to air ratio, f, is zero. a)for the turbojet engine, what is the exhaust velocity and thrust? b)for the turbofan engine, what is the core exhaust velocity and thrust? c)for the turbofan engine, what is the fan mass flowd)for the turbofan engine, what is the fan exhaust velocity? e)for the turbofan engine, what is the total engine thrust