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Mass Flow Rate Bypass refers to the rate at which air bypasses the core of a turbofan engine and flows through the bypass duct. Check FAQs
b=T-mc(Vj,c-V)Vj,b-V
b - Mass Flow Rate Bypass?T - Turbofan Thrust?mc - Mass Flow Rate Core?Vj,c - Exit Velocity Core Nozzle?V - Flight Speed?Vj,b - Exit Velocity Bypass Nozzle?

Bypass Mass Flow Rate given Turbofan Thrust Example

With values
With units
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Here is how the Bypass Mass Flow Rate given Turbofan Thrust equation looks like with Values.

Here is how the Bypass Mass Flow Rate given Turbofan Thrust equation looks like with Units.

Here is how the Bypass Mass Flow Rate given Turbofan Thrust equation looks like.

257.9615Edit=17.8Edit-43Edit(300Edit-198Edit)250Edit-198Edit
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Bypass Mass Flow Rate given Turbofan Thrust Solution

Follow our step by step solution on how to calculate Bypass Mass Flow Rate given Turbofan Thrust?

FIRST Step Consider the formula
b=T-mc(Vj,c-V)Vj,b-V
Next Step Substitute values of Variables
b=17.8kN-43kg/s(300m/s-198m/s)250m/s-198m/s
Next Step Convert Units
b=17800N-43kg/s(300m/s-198m/s)250m/s-198m/s
Next Step Prepare to Evaluate
b=17800-43(300-198)250-198
Next Step Evaluate
b=257.961538461538kg/s
LAST Step Rounding Answer
b=257.9615kg/s

Bypass Mass Flow Rate given Turbofan Thrust Formula Elements

Variables
Mass Flow Rate Bypass
Mass Flow Rate Bypass refers to the rate at which air bypasses the core of a turbofan engine and flows through the bypass duct.
Symbol: b
Measurement: Mass Flow RateUnit: kg/s
Note: Value should be greater than 0.
Turbofan Thrust
Turbofan Thrust is the total thrust produced by jet core efflux and bypass air which has been accelerated by a ducted fan.
Symbol: T
Measurement: ForceUnit: kN
Note: Value should be greater than 0.
Mass Flow Rate Core
Mass Flow Rate Core refers to the rate at which air flows through the core of a turbofan engine, specifically through the combustion chamber and the turbine.
Symbol: mc
Measurement: Mass Flow RateUnit: kg/s
Note: Value should be greater than 0.
Exit Velocity Core Nozzle
Exit Velocity Core Nozzle is the speed at which exhaust gases exit the primary nozzle of a turbofan engine.
Symbol: Vj,c
Measurement: SpeedUnit: m/s
Note: Value should be greater than 0.
Flight Speed
Flight Speed refers to the velocity at which an aircraft travels through the air.
Symbol: V
Measurement: SpeedUnit: m/s
Note: Value should be greater than 0.
Exit Velocity Bypass Nozzle
Exit Velocity Bypass Nozzle is the speed at which exhaust gases exit the secondary nozzle of a turbofan exit.
Symbol: Vj,b
Measurement: SpeedUnit: m/s
Note: Value should be greater than 0.

Other Formulas to find Mass Flow Rate Bypass

​Go Bypass Mass Flow Rate
b=ma-mc

Other formulas in Turbofans category

​Go Bypass Ratio
bpr=bmc
​Go Cooling Effectiveness
ε=Tg-TmTg-Tc
​Go Total mass flow rate through turbofan engine
ma=mc+b
​Go Turbofan thrust
T=mc(Vj,c-V)+b(Vj,b-V)

How to Evaluate Bypass Mass Flow Rate given Turbofan Thrust?

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 b 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.

FAQs on Bypass Mass Flow Rate given Turbofan Thrust

What is the formula to find Bypass Mass Flow Rate given Turbofan Thrust?
The formula of Bypass Mass Flow Rate given Turbofan Thrust is expressed as Mass Flow Rate Bypass = (Turbofan Thrust-Mass Flow Rate Core*(Exit Velocity Core Nozzle-Flight Speed))/(Exit Velocity Bypass Nozzle-Flight Speed). Here is an example- 257.9615 = (17800-43*(300-198))/(250-198).
How to calculate Bypass Mass Flow Rate given Turbofan Thrust?
With Turbofan Thrust (T), Mass Flow Rate Core (mc), Exit Velocity Core Nozzle (Vj,c), Flight Speed (V) & Exit Velocity Bypass Nozzle (Vj,b) we can find Bypass Mass Flow Rate given Turbofan Thrust using the formula - Mass Flow Rate Bypass = (Turbofan Thrust-Mass Flow Rate Core*(Exit Velocity Core Nozzle-Flight Speed))/(Exit Velocity Bypass Nozzle-Flight Speed).
What are the other ways to Calculate Mass Flow Rate Bypass?
Here are the different ways to Calculate Mass Flow Rate Bypass-
  • Mass Flow Rate Bypass=Mass Flow Rate-Mass Flow Rate CoreOpenImg
Can the Bypass Mass Flow Rate given Turbofan Thrust be negative?
No, the Bypass Mass Flow Rate given Turbofan Thrust, measured in Mass Flow Rate cannot be negative.
Which unit is used to measure Bypass Mass Flow Rate given Turbofan Thrust?
Bypass Mass Flow Rate given Turbofan Thrust is usually measured using the Kilogram per Second[kg/s] for Mass Flow Rate. Gram per Second[kg/s], Gram per Hour[kg/s], Milligram per Minute[kg/s] are the few other units in which Bypass Mass Flow Rate given Turbofan Thrust can be measured.
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