FormulaDen.com
Physics
Chemistry
Math
Chemical Engineering
Civil
Electrical
Electronics
Electronics and Instrumentation
Materials Science
Mechanical
Production Engineering
Financial
Health
You are here
-
Home
»
Physics
»
Aerospace
»
Propulsion
Mass Flow Rate Bypass in Jet Propulsion Formulas
Mass Flow Rate Bypass refers to the rate at which air bypasses the core of a turbofan engine and flows through the bypass duct. And is denoted by ṁ
b
. Mass Flow Rate Bypass is usually measured using the Kilogram per Second for Mass Flow Rate. Note that the value of Mass Flow Rate Bypass is always positive.
Formulas to find Mass Flow Rate Bypass in Jet Propulsion
f
x
Bypass Mass Flow Rate
Go
f
x
Bypass Mass Flow Rate given Turbofan Thrust
Go
Jet Propulsion formulas that make use of Mass Flow Rate Bypass
f
x
Bypass Ratio
Go
f
x
Total mass flow rate through turbofan engine
Go
f
x
Turbofan thrust
Go
f
x
Core Exhaust Velocity given Turbofan Thrust
Go
f
x
Bypass Exhaust Velocity given Turbofan Thrust
Go
f
x
Mass flow rate hot primary engine
Go
f
x
Primary Mass flow Rate in Turbofan Engine
Go
List of variables in Jet Propulsion formulas
f
x
Mass Flow Rate
Go
f
x
Mass Flow Rate Core
Go
f
x
Turbofan Thrust
Go
f
x
Exit Velocity Core Nozzle
Go
f
x
Flight Speed
Go
f
x
Exit Velocity Bypass Nozzle
Go
FAQ
What is the 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. Mass Flow Rate Bypass is usually measured using the Kilogram per Second for Mass Flow Rate. Note that the value of Mass Flow Rate Bypass is always positive.
Can the Mass Flow Rate Bypass be negative?
No, the Mass Flow Rate Bypass, measured in Mass Flow Rate cannot be negative.
What unit is used to measure Mass Flow Rate Bypass?
Mass Flow Rate Bypass 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 Mass Flow Rate Bypass can be measured.
Let Others Know
✖
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!