How to Calculate Core Exhaust Velocity given Turbofan Thrust?
Core Exhaust Velocity given Turbofan Thrust calculator uses Exit Velocity Core Nozzle = (Turbofan thrust-Mass Flow Rate Bypass*(Exit Velocity Bypass Nozzle-Flight Speed))/Mass Flow Rate Core+Flight Speed to calculate the Exit Velocity Core Nozzle, Core Exhaust Velocity given Turbofan Thrust formula is defined as velocity of the airflow from turbofan through primary or core nozzle. Exit Velocity Core Nozzle is denoted by Vj,c symbol.
How to calculate Core Exhaust Velocity given Turbofan Thrust using this online calculator? To use this online calculator for Core Exhaust Velocity given Turbofan Thrust, enter Turbofan thrust (T), Mass Flow Rate Bypass (ṁb), Exit Velocity Bypass Nozzle (Vj,b), Flight Speed (V) & Mass Flow Rate Core (mc) and hit the calculate button. Here is how the Core Exhaust Velocity given Turbofan Thrust calculation can be explained with given input values -> 299.9535 = (17800-258*(250-198))/43+198.