Mass Flow Rate of Exhaust Gases given Fuel Air Ratio Calculator

✖Mass Flow Rate Turbojet represents the amount of air entering a turbojet engine per unit time.ⓘ Mass Flow Rate Turbojet [m_a]			+10% -10%
✖Fuel Air Ratio signifies the proportion of fuel mixed with air in a combustion system.ⓘ Fuel Air Ratio [f]			+10% -10%

✖Total Mass Flow Rate Turbojet represents the amount of air and fuel exiting a turbojet engine per unit time.ⓘ Mass Flow Rate of Exhaust Gases given Fuel Air Ratio [m_total]

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Mass Flow Rate of Exhaust Gases given Fuel Air Ratio Solution

STEP 0: Pre-Calculation Summary

Formula Used

Total Mass Flow Rate Turbojet = Mass Flow Rate Turbojet*(1+Fuel Air Ratio)
m_total = m_a*(1+f)
This formula uses 3 Variables

Variables Used

Total Mass Flow Rate Turbojet - (Measured in Kilogram per Second) - Total Mass Flow Rate Turbojet represents the amount of air and fuel exiting a turbojet engine per unit time.
Mass Flow Rate Turbojet - (Measured in Kilogram per Second) - Mass Flow Rate Turbojet represents the amount of air entering a turbojet engine per unit time.
Fuel Air Ratio - Fuel Air Ratio signifies the proportion of fuel mixed with air in a combustion system.

STEP 1: Convert Input(s) to Base Unit

Mass Flow Rate Turbojet: 5 Kilogram per Second --> 5 Kilogram per Second No Conversion Required
Fuel Air Ratio: 0.008 --> No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

m_total = m_a*(1+f) --> 5*(1+0.008)

Evaluating ... ...

m_total = 5.04

STEP 3: Convert Result to Output's Unit

5.04 Kilogram per Second --> No Conversion Required

FINAL ANSWER

5.04 Kilogram per Second <-- Total Mass Flow Rate Turbojet

(Calculation completed in 00.004 seconds)

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Credits

Created by Chilvera Bhanu Teja

Institute of Aeronautical Engineering (IARE), Hyderabad

Chilvera Bhanu Teja has created this Calculator and 300+ more calculators!

Verified by Sagar S Kulkarni

Dayananda Sagar College of Engineering (DSCE), Bengaluru

Sagar S Kulkarni has verified this Calculator and 200+ more calculators!

< Turbojets Calculators

Nozzle Exit Area in Turbojet

LaTeX Go Nozzle Exit Area = (Net Thrust of Turbojet-Mass Flow Rate Turbojet*(1+Fuel Air Ratio)*(Exit Velocity-Flight Speed))/(Nozzle Exit Pressure-Ambient Pressure)

Turbojet Gross Thrust

LaTeX Go Gross Thrust of Turbojet = Mass Flow Rate Turbojet*(1+Fuel Air Ratio)*Exit Velocity+(Nozzle Exit Pressure-Ambient Pressure)*Nozzle Exit Area

Mass Flow Rate of Exhaust Gases given Fuel Air Ratio

LaTeX Go Total Mass Flow Rate Turbojet = Mass Flow Rate Turbojet*(1+Fuel Air Ratio)

Mass Flow Rate of Exhaust Gases

LaTeX Go Total Mass Flow Rate Turbojet = Mass Flow Rate Turbojet+Fuel Flow Rate

Mass Flow Rate of Exhaust Gases given Fuel Air Ratio Formula

LaTeX Go

Total Mass Flow Rate Turbojet = Mass Flow Rate Turbojet*(1+Fuel Air Ratio)
m_total = m_a*(1+f)

What is mass flow rate?

Mass flow rate is the mass of a fluid passing per unit time. It is also defined as the rate of movement of fluid through a unit area.

How to Calculate Mass Flow Rate of Exhaust Gases given Fuel Air Ratio?

Mass Flow Rate of Exhaust Gases given Fuel Air Ratio calculator uses Total Mass Flow Rate Turbojet = Mass Flow Rate Turbojet*(1+Fuel Air Ratio) to calculate the Total Mass Flow Rate Turbojet, Mass Flow Rate of Exhaust Gases given Fuel Air Ratio is a measure of the total mass flow rate of exhaust gases in an engine, which is influenced by the mass flow rate of air and the fuel-air ratio, providing valuable insights into engine performance and emissions. Total Mass Flow Rate Turbojet is denoted by m_total symbol.

How to calculate Mass Flow Rate of Exhaust Gases given Fuel Air Ratio using this online calculator? To use this online calculator for Mass Flow Rate of Exhaust Gases given Fuel Air Ratio, enter Mass Flow Rate Turbojet (m_a) & Fuel Air Ratio (f) and hit the calculate button. Here is how the Mass Flow Rate of Exhaust Gases given Fuel Air Ratio calculation can be explained with given input values -> 5.04 = 5*(1+0.008).

FAQ

What is Mass Flow Rate of Exhaust Gases given Fuel Air Ratio?

Mass Flow Rate of Exhaust Gases given Fuel Air Ratio is a measure of the total mass flow rate of exhaust gases in an engine, which is influenced by the mass flow rate of air and the fuel-air ratio, providing valuable insights into engine performance and emissions and is represented as m_total = m_a*(1+f) or Total Mass Flow Rate Turbojet = Mass Flow Rate Turbojet*(1+Fuel Air Ratio). Mass Flow Rate Turbojet represents the amount of air entering a turbojet engine per unit time & Fuel Air Ratio signifies the proportion of fuel mixed with air in a combustion system.

How to calculate Mass Flow Rate of Exhaust Gases given Fuel Air Ratio?

Mass Flow Rate of Exhaust Gases given Fuel Air Ratio is a measure of the total mass flow rate of exhaust gases in an engine, which is influenced by the mass flow rate of air and the fuel-air ratio, providing valuable insights into engine performance and emissions is calculated using Total Mass Flow Rate Turbojet = Mass Flow Rate Turbojet*(1+Fuel Air Ratio). To calculate Mass Flow Rate of Exhaust Gases given Fuel Air Ratio, you need Mass Flow Rate Turbojet (m_a) & Fuel Air Ratio (f). With our tool, you need to enter the respective value for Mass Flow Rate Turbojet & Fuel Air Ratio 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 Total Mass Flow Rate Turbojet?

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

Total Mass Flow Rate Turbojet = Mass Flow Rate Turbojet+Fuel Flow Rate

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