FormulaDen.com

Physics Chemistry Math Chemical Engineering Civil Electrical Electronics Electronics and Instrumentation Materials Science Mechanical Production Engineering Financial Health

Ideal Thrust given Effective Speed Ratio Formula

GoMomentum Thrust Formula

GoIdeal Thrust of Jet Engine Formula

Fx Copy

LaTeX Copy

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

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

T_ideal - Ideal Thrust?m_a - Mass Flow Rate?V - Flight Speed?α - Effective Speed Ratio?

Ideal Thrust given Effective Speed Ratio Example

With values

With units

Only example

Here is how the Ideal Thrust given Effective Speed Ratio equation looks like with Values.

Here is how the Ideal Thrust given Effective Speed Ratio equation looks like with Units.

Here is how the Ideal Thrust given Effective Speed Ratio equation looks like.

479.6564 = 3.5 \cdot 111 \cdot ((\frac{1}{0.4475}) - 1)

479.6564N = 3.5kg/s \cdot 111m/s \cdot ((\frac{1}{0.4475}) - 1)

479.6564 = 3.5 \cdot 111 \cdot ((\frac{1}{0.4475}) - 1)

Tip: Use pencil ( Pencil

) icon above to edit Input Values and Units.

Calculate

Recalculate

Solution

Copy

Reset

You are here -

Home » Category

Physics » Category

Aerospace » Category

Propulsion » fx Ideal Thrust given Effective Speed Ratio

Ideal Thrust given Effective Speed Ratio Solution

Follow our step by step solution on how to calculate Ideal Thrust given Effective Speed Ratio?

FIRST Step Consider the formula

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

Next Step Substitute values of Variables

∴

T ideal = 3.5kg/s \cdot 111m/s \cdot ((\frac{1}{0.4475}) - 1)

Next Step Prepare to Evaluate

∴

T ideal = 3.5 \cdot 111 \cdot ((\frac{1}{0.4475}) - 1)

Next Step Evaluate

∴

T ideal = 479.656424581006N

LAST Step Rounding Answer

∴

T ideal = 479.6564N

Ideal Thrust given Effective Speed Ratio Formula Elements

Variables

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

Effective Speed Ratio

Effective Speed Ratio is the ratio of aircraft forward speed to the aircraft jet velocity.

Symbol: α

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Effective Speed Ratio

Other Formulas to find Ideal Thrust

Go Momentum Thrust

T ideal = m a \cdot ((1 + f) \cdot V e - V)

Go Ideal Thrust of Jet Engine

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

Go Thrust given aircraft forward speed, velocity of exhaust

T ideal = m a \cdot (V e - 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 Thrust power

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

Go Specific thrust

I sp = V e - V

Go Specific Thrust given Effective Speed Ratio

I sp = V e \cdot (1 - α)

How to Evaluate Ideal Thrust given Effective Speed Ratio?

Ideal Thrust given Effective Speed Ratio evaluator uses Ideal Thrust = Mass Flow Rate*Flight Speed*((1/Effective Speed Ratio)-1) to evaluate the Ideal Thrust, Ideal Thrust given Effective Speed Ratio is a measure of the thrust produced by an aircraft or a jet engine, calculated by considering the mass flow rate, flight speed, and effective speed ratio, providing a crucial parameter for aerodynamic analysis and aircraft design. Ideal Thrust is denoted by T_ideal symbol.

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

FAQs on Ideal Thrust given Effective Speed Ratio

What is the formula to find Ideal Thrust given Effective Speed Ratio?

The formula of Ideal Thrust given Effective Speed Ratio is expressed as Ideal Thrust = Mass Flow Rate*Flight Speed*((1/Effective Speed Ratio)-1). Here is an example- 494.4545 = 3.5*111*((1/0.4475)-1).

How to calculate Ideal Thrust given Effective Speed Ratio?

With Mass Flow Rate (m_a), Flight Speed (V) & Effective Speed Ratio (α) we can find Ideal Thrust given Effective Speed Ratio using the formula - Ideal Thrust = Mass Flow Rate*Flight Speed*((1/Effective Speed Ratio)-1).

What are the other ways to Calculate Ideal Thrust?

Here are the different ways to Calculate Ideal Thrust-

Ideal Thrust=Mass Flow Rate*((1+Fuel Air Ratio)*Exit Velocity-Flight Speed)
Ideal Thrust=Mass Flow Rate*(Exit Velocity-Flight Speed)
Ideal Thrust=Mass Flow Rate*(Exit Velocity-Flight Speed)

Can the Ideal Thrust given Effective Speed Ratio be negative?

No, the Ideal Thrust given Effective Speed Ratio, measured in Force cannot be negative.

Which unit is used to measure Ideal Thrust given Effective Speed Ratio?

Ideal Thrust given Effective Speed Ratio is usually measured using the Newton[N] for Force. Exanewton[N], Meganewton[N], Kilonewton[N] are the few other units in which Ideal Thrust given Effective Speed Ratio can be measured.

Let Others Know

✖

Facebook

Twitter

Copied!

: Value
: Unit

Ideal Thrust given Effective Speed Ratio Formula

​GoMomentum Thrust Formula

​GoIdeal Thrust of Jet Engine Formula

Ideal Thrust given Effective Speed Ratio Example

Ideal Thrust given Effective Speed Ratio Solution

Ideal Thrust given Effective Speed Ratio Formula Elements

Other Formulas to find Ideal Thrust

Other formulas in Thrust Generation category

How to Evaluate Ideal Thrust given Effective Speed Ratio?

FAQs on Ideal Thrust given Effective Speed Ratio

Variable Name

GoMomentum Thrust Formula

GoIdeal Thrust of Jet Engine Formula