Pressure Ratio across Expansion Fan Formula

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Pressure Ratio Across Expansion Fan is the ratio of downstream and upstream pressure across expansion fan. Check FAQs
Pe,r=(1+0.5(γe-1)Me121+0.5(γe-1)Me22)γeγe-1
Pe,r - Pressure Ratio Across Expansion Fan?γe - Specific Heat Ratio Expansion Wave?Me1 - Mach Number Ahead of Expansion Fan?Me2 - Mach Number Behind Expansion Fan?

Pressure Ratio across Expansion Fan Example

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Here is how the Pressure Ratio across Expansion Fan equation looks like with Values.

Here is how the Pressure Ratio across Expansion Fan equation looks like with Units.

Here is how the Pressure Ratio across Expansion Fan equation looks like.

0.3403Edit=(1+0.5(1.41Edit-1)5Edit21+0.5(1.41Edit-1)6Edit2)1.41Edit1.41Edit-1
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Pressure Ratio across Expansion Fan Solution

Follow our step by step solution on how to calculate Pressure Ratio across Expansion Fan?

FIRST Step Consider the formula
Pe,r=(1+0.5(γe-1)Me121+0.5(γe-1)Me22)γeγe-1
Next Step Substitute values of Variables
Pe,r=(1+0.5(1.41-1)521+0.5(1.41-1)62)1.411.41-1
Next Step Prepare to Evaluate
Pe,r=(1+0.5(1.41-1)521+0.5(1.41-1)62)1.411.41-1
Next Step Evaluate
Pe,r=0.340265841483963
LAST Step Rounding Answer
Pe,r=0.3403

Pressure Ratio across Expansion Fan Formula Elements

Variables
Pressure Ratio Across Expansion Fan
Pressure Ratio Across Expansion Fan is the ratio of downstream and upstream pressure across expansion fan.
Symbol: Pe,r
Measurement: NAUnit: Unitless
Note: Value can be positive or negative.
Specific Heat Ratio Expansion Wave
The Specific Heat Ratio Expansion Wave is the ratio of the heat capacity at constant pressure to heat capacity at constant volume.
Symbol: γe
Measurement: NAUnit: Unitless
Note: Value should be greater than 1.
Mach Number Ahead of Expansion Fan
Mach Number Ahead of Expansion Fan is the Mach number of the upstream flow.
Symbol: Me1
Measurement: NAUnit: Unitless
Note: Value should be greater than 0.
Mach Number Behind Expansion Fan
Mach Number Behind Expansion Fan is the Mach number of downstream flow across the expansion fan.
Symbol: Me2
Measurement: NAUnit: Unitless
Note: Value should be greater than 0.

Other formulas in Expansion Waves category

​Go Temperature Ratio across Expansion Fan
Te,r=1+0.5(γe-1)Me121+0.5(γe-1)Me22
​Go Pressure behind Expansion Fan
P2=P1(1+0.5(γe-1)Me121+0.5(γe-1)Me22)γeγe-1
​Go Temperature behind Expansion Fan
T2=T1(1+0.5(γe-1)Me121+0.5(γe-1)Me22)
​Go Forward Mach Angle of Expansion Fan
μ1=arsin(1Me1)

How to Evaluate Pressure Ratio across Expansion Fan?

Pressure Ratio across Expansion Fan evaluator uses Pressure Ratio Across Expansion Fan = ((1+0.5*(Specific Heat Ratio Expansion Wave-1)*Mach Number Ahead of Expansion Fan^2)/(1+0.5*(Specific Heat Ratio Expansion Wave-1)*Mach Number Behind Expansion Fan^2))^((Specific Heat Ratio Expansion Wave)/(Specific Heat Ratio Expansion Wave-1)) to evaluate the Pressure Ratio Across Expansion Fan, The Pressure Ratio across Expansion Fan is a measure of the change in pressure experienced by a fluid as it passes through the fan. Expansion fans are regions in a fluid flow where the flow velocity decreases, and pressure increases due to an expansion in the flow area. Pressure Ratio Across Expansion Fan is denoted by Pe,r symbol.

How to evaluate Pressure Ratio across Expansion Fan using this online evaluator? To use this online evaluator for Pressure Ratio across Expansion Fan, enter Specific Heat Ratio Expansion Wave e), Mach Number Ahead of Expansion Fan (Me1) & Mach Number Behind Expansion Fan (Me2) and hit the calculate button.

FAQs on Pressure Ratio across Expansion Fan

What is the formula to find Pressure Ratio across Expansion Fan?
The formula of Pressure Ratio across Expansion Fan is expressed as Pressure Ratio Across Expansion Fan = ((1+0.5*(Specific Heat Ratio Expansion Wave-1)*Mach Number Ahead of Expansion Fan^2)/(1+0.5*(Specific Heat Ratio Expansion Wave-1)*Mach Number Behind Expansion Fan^2))^((Specific Heat Ratio Expansion Wave)/(Specific Heat Ratio Expansion Wave-1)). Here is an example- 0.335105 = ((1+0.5*(1.41-1)*5^2)/(1+0.5*(1.41-1)*6^2))^((1.41)/(1.41-1)).
How to calculate Pressure Ratio across Expansion Fan?
With Specific Heat Ratio Expansion Wave e), Mach Number Ahead of Expansion Fan (Me1) & Mach Number Behind Expansion Fan (Me2) we can find Pressure Ratio across Expansion Fan using the formula - Pressure Ratio Across Expansion Fan = ((1+0.5*(Specific Heat Ratio Expansion Wave-1)*Mach Number Ahead of Expansion Fan^2)/(1+0.5*(Specific Heat Ratio Expansion Wave-1)*Mach Number Behind Expansion Fan^2))^((Specific Heat Ratio Expansion Wave)/(Specific Heat Ratio Expansion Wave-1)).
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