Chilvera Bhanu Teja
Institute of Aeronautical Engineering (IARE), Hyderabad
Chilvera Bhanu Teja has created this Calculator and 200+ more calculators!
Sagar S Kulkarni
Dayananda Sagar College of Engineering (DSCE), Bengaluru
Sagar S Kulkarni has verified this Calculator and 200+ more calculators!

11 Other formulas that you can solve using the same Inputs

Total thrust if efficiency and enthalpy is known
Total thrust=Air flow rate*((sqrt(2*Enthalpy drop in nozzle*Efficiency of nozzle))-Aircraft forward speed+(sqrt(Efficiency of turbine*Transmission efficiency of propeller*Enthalpy drop in turbine))) GO
Propulsive power
Propulsive power=1/2*((Air flow rate+Fuel flow rate)*Jet velocity of aircraft^2-(Air flow rate*Aircraft forward speed^2)) GO
Thermal efficiency of jet engines if effective speed ratio is known
Thermal efficiency=Jet velocity of aircraft^2*(1-Effective speed ratio^2)/(2*Fuel air ratio*Calorific value of fuel) GO
Thrust power
Thrust power=Air flow rate*Aircraft forward speed*(Jet velocity of aircraft-Aircraft forward speed) GO
Thrust if effective speed ratio is known
Thrust=Air flow rate*Aircraft forward speed*((1/Effective speed ratio)-1) GO
Thrust if aircraft forward speed, velocity of exhaust is known
Thrust=Air flow rate*(Jet velocity of aircraft-Aircraft forward speed) GO
Thrust specific fuel consumption
Thrust-Specific Fuel Consumption=(3600*Fuel air ratio)/Specific thrust GO
Power required to produce an exhaust jet velocity
Power required=1/2*Air flow rate*Jet velocity of aircraft^2 GO
Kinetic energy of air at inlet
Kinetic Energy=1/2*Air flow rate*Aircraft forward speed^2 GO
Gross thrust
Gross thrust=Air flow rate*Jet velocity of aircraft GO
Inlet drag
Inlet drag=Air flow rate*Aircraft forward speed GO

4 Other formulas that calculate the same Output

Mass flowrate given mass flux
Mass Flow Rate=Mass flux*Number of tubes*Distance between two consequent tubes*Height GO
Mass Flow Rate in a Steady Flow
Mass Flow Rate=Cross sectional area*Fluid Velocity/Specific Volume GO
Mass flow rate of a stream in the turbine (expanders)
Mass Flow Rate=Work done rate/Change in enthalpy GO
Mass flow rate of exhaust gases
Mass Flow Rate=Air flow rate+Fuel flow rate GO

Mass flow rate of exhaust gases if fuel air ratio is known Formula

Mass Flow Rate=Air flow rate*(1+Fuel air ratio)
m=m<sub>a</sub>*(1+f)
More formulas
Speed of Sound GO
Mach Number GO
Mach Angle GO
Stagnation Temperature GO
Heat capacity ratio GO
Internal Energy of a perfect gas at given temperature GO
Enthalpy of ideal gas at given temperature GO
Shaft work in compressible flow machines GO
Shaft work in compressible flow machines neglecting inlet and exit velocities GO
Stagnation Velocity of Sound GO
Stagnation Velocity of Sound if specific heat at constant pressure is known GO
Stagnation Velocity of Sound if stagnation enthalpy is known GO
Pressure ratio GO
Mass flow rate of exhaust gases GO

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 if fuel air ratio is known?

Mass flow rate of exhaust gases if fuel air ratio is known calculator uses Mass Flow Rate=Air flow rate*(1+Fuel air ratio) to calculate the Mass Flow Rate, The Mass flow rate of exhaust gases if fuel air ratio is known formula is defined as the product of mass flow rate of air and term unity added to fuel air ratio. Mass Flow Rate and is denoted by m symbol.

How to calculate Mass flow rate of exhaust gases if fuel air ratio is known using this online calculator? To use this online calculator for Mass flow rate of exhaust gases if fuel air ratio is known, enter Air flow rate (ma) and Fuel air ratio (f) and hit the calculate button. Here is how the Mass flow rate of exhaust gases if fuel air ratio is known calculation can be explained with given input values -> 6.6 = 3*(1+1.2).

FAQ

What is Mass flow rate of exhaust gases if fuel air ratio is known?
The Mass flow rate of exhaust gases if fuel air ratio is known formula is defined as the product of mass flow rate of air and term unity added to fuel air ratio and is represented as m=ma*(1+f) or Mass Flow Rate=Air flow rate*(1+Fuel air ratio). Air flow rate is the mass flow rate of air and Fuel air ratio is the ratio of mass flow rate of fuel to the mass flow rate of air.
How to calculate Mass flow rate of exhaust gases if fuel air ratio is known?
The Mass flow rate of exhaust gases if fuel air ratio is known formula is defined as the product of mass flow rate of air and term unity added to fuel air ratio is calculated using Mass Flow Rate=Air flow rate*(1+Fuel air ratio). To calculate Mass flow rate of exhaust gases if fuel air ratio is known, you need Air flow rate (ma) and Fuel air ratio (f). With our tool, you need to enter the respective value for Air flow rate and 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 Mass Flow Rate?
In this formula, Mass Flow Rate uses Air flow rate and Fuel air ratio. We can use 4 other way(s) to calculate the same, which is/are as follows -
  • Mass Flow Rate=Cross sectional area*Fluid Velocity/Specific Volume
  • Mass Flow Rate=Work done rate/Change in enthalpy
  • Mass Flow Rate=Air flow rate+Fuel flow rate
  • Mass Flow Rate=Mass flux*Number of tubes*Distance between two consequent tubes*Height
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