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Reversible Nozzle Jet Velocity Formula

GoIdeal Exhaust Velocity given Enthalpy Drop Formula

GoJet velocity given temperature drop Formula

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Ideal Exit Velocity is the velocity at the exit of nozzle, it does not includes losses due to external factors. Check FAQs

C ideal = \sqrt{2 \cdot C p \cdot T \cdot (1 - {(P r)}^{\frac{γ - 1}{γ}})}

C_ideal - Ideal Exit Velocity?C_p - Specific Heat at Constant Pressure?T - Nozzle Temperature?P_r - Pressure Ratio?γ - Specific Heat Ratio?

Reversible Nozzle Jet Velocity Example

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Here is how the Reversible Nozzle Jet Velocity equation looks like with Values.

Here is how the Reversible Nozzle Jet Velocity equation looks like with Units.

Here is how the Reversible Nozzle Jet Velocity equation looks like.

199.1646 = \sqrt{2 \cdot 1248 \cdot 244 \cdot (1 - {(0.79)}^{\frac{1.4 - 1}{1.4}})}

199.1646m/s = \sqrt{2 \cdot 1248J/(kg*K) \cdot 244K \cdot (1 - {(0.79)}^{\frac{1.4 - 1}{1.4}})}

199.1646 = \sqrt{2 \cdot 1248 \cdot 244 \cdot (1 - {(0.79)}^{\frac{1.4 - 1}{1.4}})}

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Reversible Nozzle Jet Velocity Solution

Follow our step by step solution on how to calculate Reversible Nozzle Jet Velocity?

FIRST Step Consider the formula

C ideal = \sqrt{2 \cdot C p \cdot T \cdot (1 - {(P r)}^{\frac{γ - 1}{γ}})}

Next Step Substitute values of Variables

∴

C ideal = \sqrt{2 \cdot 1248J/(kg*K) \cdot 244K \cdot (1 - {(0.79)}^{\frac{1.4 - 1}{1.4}})}

Next Step Prepare to Evaluate

∴

C ideal = \sqrt{2 \cdot 1248 \cdot 244 \cdot (1 - {(0.79)}^{\frac{1.4 - 1}{1.4}})}

Next Step Evaluate

∴

C ideal = 199.164639851496m/s

LAST Step Rounding Answer

∴

C ideal = 199.1646m/s

Reversible Nozzle Jet Velocity Formula Elements

Variables

Functions

Ideal Exit Velocity

Ideal Exit Velocity is the velocity at the exit of nozzle, it does not includes losses due to external factors.

Symbol: C_ideal

Measurement: SpeedUnit: m/s

Note: Value should be greater than 0.

Formulas to find Ideal Exit Velocity

Specific Heat at Constant Pressure

Specific heat at constant pressure is the energy required to raise the temperature of the unit mass of a substance by one degree as the pressure is maintained constant.

Symbol: C_p

Measurement: Specific Heat CapacityUnit: J/(kg*K)

Note: Value should be greater than 0.

Formulas to find Specific Heat at Constant Pressure

Nozzle Temperature

Nozzle Temperature is the temperature of gases expanding the nozzle.

Symbol: T

Measurement: TemperatureUnit: K

Note: Value should be greater than 0.

Formulas to find Nozzle Temperature

Pressure Ratio

Pressure Ratio for the reversible nozzle is the ratio of the ambient pressure to the inlet pressure.

Symbol: P_r

Measurement: NAUnit: Unitless

Note: Value should be between 0 to 1.

Formulas to find Pressure Ratio

Specific Heat Ratio

The Specific Heat Ratio is the ratio of the heat capacity at constant pressure to heat capacity at constant volume of the flowing fluid for non-viscous and compressible flow.

Symbol: γ

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Specific Heat Ratio

sqrt

A square root function is a function that takes a non-negative number as an input and returns the square root of the given input number.

Syntax: sqrt(Number)

Other Formulas to find Ideal Exit Velocity

Go Ideal Exhaust Velocity given Enthalpy Drop

C ideal = \sqrt{2 \cdot Δh nozzle}

Go Jet velocity given temperature drop

C ideal = \sqrt{2 \cdot C p \cdot ΔT}

Other formulas in Nozzle category

Go Kinetic Energy of Exhaust Gases

KE = \frac{1}{2} \cdot m i \cdot (1 + f) \cdot {C ideal}^{2}

Go Velocity Coefficient given Nozzle Efficiency

C v = \sqrt{η nozlze}

Go Discharge Coefficient given Mass Flow

C D = \frac{m a}{m i}

Go Discharge Coefficient given Flow Area

C D = \frac{A act}{A throat}

How to Evaluate Reversible Nozzle Jet Velocity?

Reversible Nozzle Jet Velocity evaluator uses Ideal Exit Velocity = sqrt(2*Specific Heat at Constant Pressure*Nozzle Temperature*(1-(Pressure Ratio)^((Specific Heat Ratio-1)/(Specific Heat Ratio)))) to evaluate the Ideal Exit Velocity, The Reversible Nozzle Jet Velocity formula calculates the jet velocity for a reversible nozzle if the specific heat, temperature, pressure ratio, and specific heat ratio for an engine is given. Ideal Exit Velocity is denoted by C_ideal symbol.

How to evaluate Reversible Nozzle Jet Velocity using this online evaluator? To use this online evaluator for Reversible Nozzle Jet Velocity, enter Specific Heat at Constant Pressure (C_p), Nozzle Temperature (T), Pressure Ratio (P_r) & Specific Heat Ratio (γ) and hit the calculate button.

FAQs on Reversible Nozzle Jet Velocity

What is the formula to find Reversible Nozzle Jet Velocity?

The formula of Reversible Nozzle Jet Velocity is expressed as Ideal Exit Velocity = sqrt(2*Specific Heat at Constant Pressure*Nozzle Temperature*(1-(Pressure Ratio)^((Specific Heat Ratio-1)/(Specific Heat Ratio)))). Here is an example- 197.5254 = sqrt(2*1248*244*(1-(0.79)^((1.4-1)/(1.4)))).

How to calculate Reversible Nozzle Jet Velocity?

With Specific Heat at Constant Pressure (C_p), Nozzle Temperature (T), Pressure Ratio (P_r) & Specific Heat Ratio (γ) we can find Reversible Nozzle Jet Velocity using the formula - Ideal Exit Velocity = sqrt(2*Specific Heat at Constant Pressure*Nozzle Temperature*(1-(Pressure Ratio)^((Specific Heat Ratio-1)/(Specific Heat Ratio)))). This formula also uses Square Root (sqrt) function(s).

What are the other ways to Calculate Ideal Exit Velocity?

Here are the different ways to Calculate Ideal Exit Velocity-

Ideal Exit Velocity=sqrt(2*Enthalpy Drop in Nozzle)
Ideal Exit Velocity=sqrt(2*Specific Heat at Constant Pressure*Temperature Drop)

Can the Reversible Nozzle Jet Velocity be negative?

No, the Reversible Nozzle Jet Velocity, measured in Speed cannot be negative.

Which unit is used to measure Reversible Nozzle Jet Velocity?

Reversible Nozzle Jet Velocity 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 Reversible Nozzle Jet Velocity can be measured.

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: Unit

Reversible Nozzle Jet Velocity Formula

​GoIdeal Exhaust Velocity given Enthalpy Drop Formula

​GoJet velocity given temperature drop Formula

Reversible Nozzle Jet Velocity Example

Reversible Nozzle Jet Velocity Solution

Reversible Nozzle Jet Velocity Formula Elements

Other Formulas to find Ideal Exit Velocity

Other formulas in Nozzle category

How to Evaluate Reversible Nozzle Jet Velocity?

FAQs on Reversible Nozzle Jet Velocity

Variable Name

GoIdeal Exhaust Velocity given Enthalpy Drop Formula

GoJet velocity given temperature drop Formula