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Velocity after Expansion given Ideal Thrust Formula

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

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

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

Velocity after Expansion given Ideal Thrust Example

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Here is how the Velocity after Expansion given Ideal Thrust equation looks like with Values.

Here is how the Velocity after Expansion given Ideal Thrust equation looks like with Units.

Here is how the Velocity after Expansion given Ideal Thrust equation looks like.

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

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

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

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Velocity after Expansion given Ideal Thrust Solution

Follow our step by step solution on how to calculate Velocity after Expansion given Ideal Thrust?

FIRST Step Consider the formula

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

Next Step Substitute values of Variables

∴

V e = \frac{479.5N}{3.5kg/s} + 111m/s

Next Step Prepare to Evaluate

∴

V e = \frac{479.5}{3.5} + 111

LAST Step Evaluate

∴

V e = 248m/s

Velocity after Expansion given Ideal Thrust Formula Elements

Variables

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

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

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

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 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 Velocity after Expansion given Ideal Thrust?

Velocity after Expansion given Ideal Thrust evaluator uses Exit Velocity = Ideal Thrust/Mass Flow Rate+Flight Speed to evaluate the Exit Velocity, Velocity after Expansion given Ideal Thrust is a measure of the velocity achieved by an object after expansion, calculated by considering the ideal thrust, mass flow rate, and flight speed of the object, providing valuable insights into the object's motion and behavior. Exit Velocity is denoted by V_e symbol.

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

FAQs on Velocity after Expansion given Ideal Thrust

What is the formula to find Velocity after Expansion given Ideal Thrust?

The formula of Velocity after Expansion given Ideal Thrust is expressed as Exit Velocity = Ideal Thrust/Mass Flow Rate+Flight Speed. Here is an example- 240.4286 = 479.5/3.5+111.

How to calculate Velocity after Expansion given Ideal Thrust?

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

Can the Velocity after Expansion given Ideal Thrust be negative?

Yes, the Velocity after Expansion given Ideal Thrust, measured in Speed can be negative.

Which unit is used to measure Velocity after Expansion given Ideal Thrust?

Velocity after Expansion given Ideal Thrust is usually measured using the Meter per Second[m/s] for Speed. Meter per Minute[m/s], Meter per Hour[m/s], Kilometer per Hour[m/s] are the few other units in which Velocity after Expansion given Ideal Thrust can be measured.

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Velocity after Expansion given Ideal Thrust Formula

Velocity after Expansion given Ideal Thrust Example

Velocity after Expansion given Ideal Thrust Solution

Velocity after Expansion given Ideal Thrust Formula Elements

Other formulas in Thrust Generation category

How to Evaluate Velocity after Expansion given Ideal Thrust?

FAQs on Velocity after Expansion given Ideal Thrust

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