Ratio of Stagnation and Static Temperature Formula

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The Stagnation to Static Temperature ratio depends upon the Mach number and ratio of specific heats. Check FAQs
Tr=1+(γ-12)M2
Tr - Stagnation to Static Temperature?γ - Specific Heat Ratio?M - Mach Number?

Ratio of Stagnation and Static Temperature Example

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Here is how the Ratio of Stagnation and Static Temperature equation looks like with Values.

Here is how the Ratio of Stagnation and Static Temperature equation looks like with Units.

Here is how the Ratio of Stagnation and Static Temperature equation looks like.

1.8Edit=1+(1.4Edit-12)2Edit2
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Ratio of Stagnation and Static Temperature Solution

Follow our step by step solution on how to calculate Ratio of Stagnation and Static Temperature?

FIRST Step Consider the formula
Tr=1+(γ-12)M2
Next Step Substitute values of Variables
Tr=1+(1.4-12)22
Next Step Prepare to Evaluate
Tr=1+(1.4-12)22
LAST Step Evaluate
Tr=1.8

Ratio of Stagnation and Static Temperature Formula Elements

Variables
Stagnation to Static Temperature
The Stagnation to Static Temperature ratio depends upon the Mach number and ratio of specific heats.
Symbol: Tr
Measurement: NAUnit: Unitless
Note: Value should be greater than 0.
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.
Mach Number
Mach Number is a dimensionless quantity representing the ratio of flow velocity past a boundary to the local speed of sound.
Symbol: M
Measurement: NAUnit: Unitless
Note: Value should be greater than 0.

Other formulas in Governing Equations and Sound Wave category

​Go Speed of Sound
a=γ[R-Dry-Air]Ts
​Go Mach Number
M=Vba
​Go Mach Angle
μ=asin(1M)
​Go Mayer's Formula
R=Cp-Cv

How to Evaluate Ratio of Stagnation and Static Temperature?

Ratio of Stagnation and Static Temperature evaluator uses Stagnation to Static Temperature = 1+((Specific Heat Ratio-1)/2)*Mach Number^2 to evaluate the Stagnation to Static Temperature, The Ratio of Stagnation and Static temperature, this equation demonstrates how the ratio of stagnation temperature to static temperature varies with the Mach number of the flow. It indicates the temperature rise due to compression or temperature drop due to expansion associated with changes in flow velocity and Mach number in a compressible flow. Stagnation to Static Temperature is denoted by Tr symbol.

How to evaluate Ratio of Stagnation and Static Temperature using this online evaluator? To use this online evaluator for Ratio of Stagnation and Static Temperature, enter Specific Heat Ratio (γ) & Mach Number (M) and hit the calculate button.

FAQs on Ratio of Stagnation and Static Temperature

What is the formula to find Ratio of Stagnation and Static Temperature?
The formula of Ratio of Stagnation and Static Temperature is expressed as Stagnation to Static Temperature = 1+((Specific Heat Ratio-1)/2)*Mach Number^2. Here is an example- 1.82 = 1+((1.4-1)/2)*2^2.
How to calculate Ratio of Stagnation and Static Temperature?
With Specific Heat Ratio (γ) & Mach Number (M) we can find Ratio of Stagnation and Static Temperature using the formula - Stagnation to Static Temperature = 1+((Specific Heat Ratio-1)/2)*Mach Number^2.
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