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Mass Flow Rate given Ideal Thrust Formula

GoMass Flow given Momentum in Ambient Air Formula

GoMass Flow Rate given Ram Drag and Flight Speed Formula

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Mass Flow Rate represents the amount of mass passing through a system per unit of time. Check FAQs

m a = \frac{T ideal}{V e - V}

m_a - Mass Flow Rate?T_ideal - Ideal Thrust?V_e - Exit Velocity?V - Flight Speed?

Mass Flow Rate given Ideal Thrust Example

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Here is how the Mass Flow Rate given Ideal Thrust equation looks like with Values.

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

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

3.5 = \frac{479.5}{248 - 111}

3.5kg/s = \frac{479.5N}{248m/s - 111m/s}

3.5 = \frac{479.5}{248 - 111}

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Mass Flow Rate given Ideal Thrust Solution

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

FIRST Step Consider the formula

m a = \frac{T ideal}{V e - V}

Next Step Substitute values of Variables

∴

m a = \frac{479.5N}{248m/s - 111m/s}

Next Step Prepare to Evaluate

∴

m a = \frac{479.5}{248 - 111}

LAST Step Evaluate

∴

m a = 3.5kg/s

Mass Flow Rate given Ideal Thrust Formula Elements

Variables

Mass Flow Rate

Mass Flow Rate represents the amount of mass passing through a system per unit of time.

Symbol: m_a

Measurement: Mass Flow RateUnit: kg/s

Note: Value should be greater than 0.

Formulas to find Mass Flow Rate

Ideal Thrust

Ideal Thrust is the thrust produced by an engine when nozzle exit pressure is same as ambient pressure or nozzle is perfectly expanded.

Symbol: T_ideal

Measurement: ForceUnit: N

Note: Value should be greater than 0.

Formulas to find Ideal Thrust

Exit Velocity

Exit Velocity refers to the speed at which gases expand at the exit of nozzle of a engine.

Symbol: V_e

Measurement: SpeedUnit: m/s

Note: Value can be positive or negative.

Formulas to find Exit Velocity

Flight Speed

Flight Speed refers to the velocity at which an aircraft moves through the air.

Symbol: V

Measurement: SpeedUnit: m/s

Note: Value should be greater than 0.

Formulas to find Flight Speed

Other Formulas to find Mass Flow Rate

Go Mass Flow given Momentum in Ambient Air

m a = \frac{M}{V}

Go Mass Flow Rate given Ram Drag and Flight Speed

m a = \frac{D ram}{V}

Other formulas in Thrust Generation category

Go Total Thrust given Efficiency and Enthalpy

T total = m a \cdot ((\sqrt{2 \cdot Δh nozzle \cdot η nozzle}) - V + (\sqrt{η T \cdot η transmission \cdot Δh turbine}))

Go Ideal Thrust given Effective Speed Ratio

T ideal = m a \cdot V \cdot ((\frac{1}{α}) - 1)

Go Thrust power

T P = m a \cdot V \cdot (V e - V)

Go Specific thrust

I sp = V e - V

How to Evaluate Mass Flow Rate given Ideal Thrust?

Mass Flow Rate given Ideal Thrust evaluator uses Mass Flow Rate = Ideal Thrust/(Exit Velocity-Flight Speed) to evaluate the Mass Flow Rate, Mass Flow Rate given Ideal Thrust is a measurement of the rate of mass flow of a fluid, typically in aerospace engineering, calculated by considering the ideal thrust, the exit velocity and flight speed of an aircraft or rocket. Mass Flow Rate is denoted by m_a symbol.

How to evaluate Mass Flow Rate given Ideal Thrust using this online evaluator? To use this online evaluator for Mass Flow Rate given Ideal Thrust, enter Ideal Thrust (T_ideal), Exit Velocity (V_e) & Flight Speed (V) and hit the calculate button.

FAQs on Mass Flow Rate given Ideal Thrust

What is the formula to find Mass Flow Rate given Ideal Thrust?

The formula of Mass Flow Rate given Ideal Thrust is expressed as Mass Flow Rate = Ideal Thrust/(Exit Velocity-Flight Speed). Here is an example- 3.306569 = 479.5/(248-111).

How to calculate Mass Flow Rate given Ideal Thrust?

With Ideal Thrust (T_ideal), Exit Velocity (V_e) & Flight Speed (V) we can find Mass Flow Rate given Ideal Thrust using the formula - Mass Flow Rate = Ideal Thrust/(Exit Velocity-Flight Speed).

What are the other ways to Calculate Mass Flow Rate?

Here are the different ways to Calculate Mass Flow Rate-

Mass Flow Rate=Momentum of Ambient Air/Flight Speed
Mass Flow Rate=Ram Drag/Flight Speed

Can the Mass Flow Rate given Ideal Thrust be negative?

No, the Mass Flow Rate given Ideal Thrust, measured in Mass Flow Rate cannot be negative.

Which unit is used to measure Mass Flow Rate given Ideal Thrust?

Mass Flow Rate given Ideal 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 Mass Flow Rate given Ideal Thrust can be measured.

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Mass Flow Rate given Ideal Thrust Formula

​GoMass Flow given Momentum in Ambient Air Formula

​GoMass Flow Rate given Ram Drag and Flight Speed Formula

Mass Flow Rate given Ideal Thrust Example

Mass Flow Rate given Ideal Thrust Solution

Mass Flow Rate given Ideal Thrust Formula Elements

Other Formulas to find Mass Flow Rate

Other formulas in Thrust Generation category

How to Evaluate Mass Flow Rate given Ideal Thrust?

FAQs on Mass Flow Rate given Ideal Thrust

Variable Name

GoMass Flow given Momentum in Ambient Air Formula

GoMass Flow Rate given Ram Drag and Flight Speed Formula