Pressure behind Expansion Fan Formula

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Pressure Behind Expansion Fan is the pressure in the downstream direction of the expansion fan. Check FAQs
P2=P1(1+0.5(γe-1)Me121+0.5(γe-1)Me22)γeγe-1
P2 - Pressure Behind Expansion Fan?P1 - Pressure Ahead of Expansion Fan?γe - Specific Heat Ratio Expansion Wave?Me1 - Mach Number Ahead of Expansion Fan?Me2 - Mach Number Behind Expansion Fan?

Pressure behind Expansion Fan Example

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With units
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Here is how the Pressure behind Expansion Fan equation looks like with Values.

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

Here is how the Pressure behind Expansion Fan equation looks like.

13.6106Edit=40Edit(1+0.5(1.41Edit-1)5Edit21+0.5(1.41Edit-1)6Edit2)1.41Edit1.41Edit-1
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Pressure behind Expansion Fan Solution

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

FIRST Step Consider the formula
P2=P1(1+0.5(γe-1)Me121+0.5(γe-1)Me22)γeγe-1
Next Step Substitute values of Variables
P2=40Pa(1+0.5(1.41-1)521+0.5(1.41-1)62)1.411.41-1
Next Step Prepare to Evaluate
P2=40(1+0.5(1.41-1)521+0.5(1.41-1)62)1.411.41-1
Next Step Evaluate
P2=13.6106336593585Pa
LAST Step Rounding Answer
P2=13.6106Pa

Pressure behind Expansion Fan Formula Elements

Variables
Pressure Behind Expansion Fan
Pressure Behind Expansion Fan is the pressure in the downstream direction of the expansion fan.
Symbol: P2
Measurement: PressureUnit: Pa
Note: Value can be positive or negative.
Pressure Ahead of Expansion Fan
Pressure Ahead of Expansion Fan is the pressure in the upstream direction of the expansion fan.
Symbol: P1
Measurement: PressureUnit: Pa
Note: Value should be greater than 0.
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 Pressure Ratio across Expansion Fan
Pe,r=(1+0.5(γe-1)Me121+0.5(γe-1)Me22)γeγe-1
​Go Temperature Ratio across Expansion Fan
Te,r=1+0.5(γe-1)Me121+0.5(γe-1)Me22
​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 behind Expansion Fan?

Pressure behind Expansion Fan evaluator uses Pressure Behind Expansion Fan = Pressure Ahead of 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 Behind Expansion Fan, The Pressure behind Expansion Fan formula is defined as the product of upstream static pressure ahead of expansion fan to the ratio of static to stagnation pressure ratio downstream to upstream across the expansion fan. Pressure Behind Expansion Fan is denoted by P2 symbol.

How to evaluate Pressure behind Expansion Fan using this online evaluator? To use this online evaluator for Pressure behind Expansion Fan, enter Pressure Ahead of Expansion Fan (P1), 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 behind Expansion Fan

What is the formula to find Pressure behind Expansion Fan?
The formula of Pressure behind Expansion Fan is expressed as Pressure Behind Expansion Fan = Pressure Ahead of 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- 13.4042 = 40*((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 behind Expansion Fan?
With Pressure Ahead of Expansion Fan (P1), Specific Heat Ratio Expansion Wave e), Mach Number Ahead of Expansion Fan (Me1) & Mach Number Behind Expansion Fan (Me2) we can find Pressure behind Expansion Fan using the formula - Pressure Behind Expansion Fan = Pressure Ahead of 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)).
Can the Pressure behind Expansion Fan be negative?
Yes, the Pressure behind Expansion Fan, measured in Pressure can be negative.
Which unit is used to measure Pressure behind Expansion Fan?
Pressure behind Expansion Fan is usually measured using the Pascal[Pa] for Pressure. Kilopascal[Pa], Bar[Pa], Pound Per Square Inch[Pa] are the few other units in which Pressure behind Expansion Fan can be measured.
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