Bypass Mass Flow Rate given Turbofan Thrust evaluator uses Mass Flow Rate Bypass = (Turbofan Thrust-Mass Flow Rate Core*(Exit Velocity Core Nozzle-Flight Speed))/(Exit Velocity Bypass Nozzle-Flight Speed) to evaluate the Mass Flow Rate Bypass, Bypass Mass Flow Rate given Turbofan Thrust is a measure of the mass flow rate of air that bypasses the core engine in a turbofan engine, which is a critical parameter in aircraft engine design and performance. Mass Flow Rate Bypass is denoted by ṁb symbol.
How to evaluate Bypass Mass Flow Rate given Turbofan Thrust using this online evaluator? To use this online evaluator for Bypass Mass Flow Rate given Turbofan Thrust, enter Turbofan Thrust (T), Mass Flow Rate Core (mc), Exit Velocity Core Nozzle (Vj,c), Flight Speed (V) & Exit Velocity Bypass Nozzle (Vj,b) and hit the calculate button.