Mass flow rate hot primary engine Calculator

✖Mass Flow Rate represents the amount of mass passing through a system per unit of time.ⓘ Mass Flow Rate [m_a]			+10% -10%
✖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 [ṁ_b]			+10% -10%

✖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.ⓘ Mass flow rate hot primary engine [m_c]

⎘ Copy

👎

Formula

✖

Mass flow rate hot primary engine

Formula

m c = m a - ṁ b

Example

43 kg/s = 301 kg/s - 258 kg/s

Calculator

LaTeX

Reset

👍

Download Turbofans Formulas PDF PDF Image

Mass flow rate hot primary engine Solution

STEP 0: Pre-Calculation Summary

Formula Used

Mass Flow Rate Core = Mass Flow Rate-Mass Flow Rate Bypass
m_c = m_a-ṁ_b
This formula uses 3 Variables

Variables Used

Mass Flow Rate Core - (Measured in Kilogram per Second) - 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.
Mass Flow Rate - (Measured in Kilogram per Second) - Mass Flow Rate represents the amount of mass passing through a system per unit of time.
Mass Flow Rate Bypass - (Measured in Kilogram per Second) - Mass Flow Rate Bypass refers to the rate at which air bypasses the core of a turbofan engine and flows through the bypass duct.

STEP 1: Convert Input(s) to Base Unit

Mass Flow Rate: 301 Kilogram per Second --> 301 Kilogram per Second No Conversion Required
Mass Flow Rate Bypass: 258 Kilogram per Second --> 258 Kilogram per Second No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

m_c = m_a-ṁ_b --> 301-258

Evaluating ... ...

m_c = 43

STEP 3: Convert Result to Output's Unit

43 Kilogram per Second --> No Conversion Required

FINAL ANSWER

43 Kilogram per Second <-- Mass Flow Rate Core

(Calculation completed in 00.020 seconds)

You are here -

Home » Physics » Propulsion » Jet Propulsion » Aerospace » Turbofans » Mass flow rate hot primary engine

Credits

Created by Himanshu Sharma

National Institute of Technology, Hamirpur (NITH), Himachal Pradesh

Himanshu Sharma has created this Calculator and 50+ more calculators!

Verified by Kartikay Pandit

National Institute Of Technology (NIT), Hamirpur

Kartikay Pandit has verified this Calculator and 400+ more calculators!

< Turbofans Calculators

Turbofan thrust

Go Turbofan Thrust = Mass Flow Rate Core*(Exit Velocity Core Nozzle-Flight Speed)+Mass Flow Rate Bypass*(Exit Velocity Bypass Nozzle-Flight Speed)

Cooling Effectiveness

Go Cooling Effectiveness = (Temperature of Hot Gas Stream-Temperature of Metal)/(Temperature of Hot Gas Stream-Temperature of Cooling Air)

Total mass flow rate through turbofan engine

Go Mass Flow Rate = Mass Flow Rate Core+Mass Flow Rate Bypass

Bypass Ratio

Go Bypass Ratio = Mass Flow Rate Bypass/Mass Flow Rate Core

Mass flow rate hot primary engine Formula

Mass Flow Rate Core = Mass Flow Rate-Mass Flow Rate Bypass
m_c = m_a-ṁ_b

What is mass flow rate?

In physics and engineering, mass flow rate is the mass of a substance which passes per unit of time. Its unit is kilogram per second in SI units, and slug per second or pound per second in US customary units.

How to Calculate Mass flow rate hot primary engine?

Mass flow rate hot primary engine calculator uses Mass Flow Rate Core = Mass Flow Rate-Mass Flow Rate Bypass to calculate the Mass Flow Rate Core, Mass flow rate hot primary engine is a measure of the rate of mass flowing through the hot primary engine, typically used in engineering and physics applications to calculate the amount of mass being processed or transported. Mass Flow Rate Core is denoted by m_c symbol.

How to calculate Mass flow rate hot primary engine using this online calculator? To use this online calculator for Mass flow rate hot primary engine, enter Mass Flow Rate (m_a) & Mass Flow Rate Bypass (ṁ_b) and hit the calculate button. Here is how the Mass flow rate hot primary engine calculation can be explained with given input values -> 42 = 301-258.

FAQ

What is Mass flow rate hot primary engine?

Mass flow rate hot primary engine is a measure of the rate of mass flowing through the hot primary engine, typically used in engineering and physics applications to calculate the amount of mass being processed or transported and is represented as m_c = m_a-ṁ_b or Mass Flow Rate Core = Mass Flow Rate-Mass Flow Rate Bypass. Mass Flow Rate represents the amount of mass passing through a system per unit of time & Mass Flow Rate Bypass refers to the rate at which air bypasses the core of a turbofan engine and flows through the bypass duct.

How to calculate Mass flow rate hot primary engine?

Mass flow rate hot primary engine is a measure of the rate of mass flowing through the hot primary engine, typically used in engineering and physics applications to calculate the amount of mass being processed or transported is calculated using Mass Flow Rate Core = Mass Flow Rate-Mass Flow Rate Bypass. To calculate Mass flow rate hot primary engine, you need Mass Flow Rate (m_a) & Mass Flow Rate Bypass (ṁ_b). With our tool, you need to enter the respective value for Mass Flow Rate & Mass Flow Rate Bypass and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

How many ways are there to calculate Mass Flow Rate Core?

In this formula, Mass Flow Rate Core uses Mass Flow Rate & Mass Flow Rate Bypass. We can use 1 other way(s) to calculate the same, which is/are as follows -

Mass Flow Rate Core = (Turbofan Thrust-Mass Flow Rate Bypass*(Exit Velocity Bypass Nozzle-Flight Speed))/(Exit Velocity Core Nozzle-Flight Speed)

Home

FREE PDFs

🔍 Search