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Flow Deflection Angle is defined as the angle by which the flow turns through the expansion wave. Check FAQs
θe=vM2-vM1
θe - Flow Deflection Angle?vM2 - Prandtl Meyer Function at Downstream Mach no.?vM1 - Prandtl Meyer Function at Upstream Mach no.?

Flow Deflection Angle using Prandtl Meyer Function Example

With values
With units
Only example

Here is how the Flow Deflection Angle using Prandtl Meyer Function equation looks like with Values.

Here is how the Flow Deflection Angle using Prandtl Meyer Function equation looks like with Units.

Here is how the Flow Deflection Angle using Prandtl Meyer Function equation looks like.

6Edit=83Edit-77Edit
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Flow Deflection Angle using Prandtl Meyer Function Solution

Follow our step by step solution on how to calculate Flow Deflection Angle using Prandtl Meyer Function?

FIRST Step Consider the formula
θe=vM2-vM1
Next Step Substitute values of Variables
θe=83°-77°
Next Step Convert Units
θe=1.4486rad-1.3439rad
Next Step Prepare to Evaluate
θe=1.4486-1.3439
Next Step Evaluate
θe=0.10471975511964rad
Next Step Convert to Output's Unit
θe=5.99999999999999°
LAST Step Rounding Answer
θe=6°

Flow Deflection Angle using Prandtl Meyer Function Formula Elements

Variables
Flow Deflection Angle
Flow Deflection Angle is defined as the angle by which the flow turns through the expansion wave.
Symbol: θe
Measurement: AngleUnit: °
Note: Value can be positive or negative.
Prandtl Meyer Function at Downstream Mach no.
Prandtl Meyer Function at Downstream Mach no. is the Prandtl Meyer Functional value at downstream of expansion wave.
Symbol: vM2
Measurement: AngleUnit: °
Note: Value can be positive or negative.
Prandtl Meyer Function at Upstream Mach no.
Prandtl Meyer Function at Upstream Mach no. is the Prandtl Meyer Functional value at upstream of expansion wave.
Symbol: vM1
Measurement: AngleUnit: °
Note: Value can be positive or negative.

Other Formulas to find Flow Deflection Angle

​Go Flow Deflection Angle due to Expansion Wave
θe=(γe+1γe-1atan((γe-1)(Me22-1)γe+1)-atan(Me22-1))-(γe+1γe-1atan((γe-1)(Me12-1)γe+1)-atan(Me12-1))

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 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)

How to Evaluate Flow Deflection Angle using Prandtl Meyer Function?

Flow Deflection Angle using Prandtl Meyer Function evaluator uses Flow Deflection Angle = Prandtl Meyer Function at Downstream Mach no.-Prandtl Meyer Function at Upstream Mach no. to evaluate the Flow Deflection Angle, The Flow deflection angle using Prandtl Meyer function formula relates the Mach number to the maximum deflection angle achievable through an isentropic (constant entropy) expansion process. It is obtained as the difference of the Prandtl Meyer function calculated at downstream and upstream Mach number. Flow Deflection Angle is denoted by θe symbol.

How to evaluate Flow Deflection Angle using Prandtl Meyer Function using this online evaluator? To use this online evaluator for Flow Deflection Angle using Prandtl Meyer Function, enter Prandtl Meyer Function at Downstream Mach no. (vM2) & Prandtl Meyer Function at Upstream Mach no. (vM1) and hit the calculate button.

FAQs on Flow Deflection Angle using Prandtl Meyer Function

What is the formula to find Flow Deflection Angle using Prandtl Meyer Function?
The formula of Flow Deflection Angle using Prandtl Meyer Function is expressed as Flow Deflection Angle = Prandtl Meyer Function at Downstream Mach no.-Prandtl Meyer Function at Upstream Mach no.. Here is an example- 343.7747 = 1.44862327915502-1.34390352403538.
How to calculate Flow Deflection Angle using Prandtl Meyer Function?
With Prandtl Meyer Function at Downstream Mach no. (vM2) & Prandtl Meyer Function at Upstream Mach no. (vM1) we can find Flow Deflection Angle using Prandtl Meyer Function using the formula - Flow Deflection Angle = Prandtl Meyer Function at Downstream Mach no.-Prandtl Meyer Function at Upstream Mach no..
What are the other ways to Calculate Flow Deflection Angle?
Here are the different ways to Calculate Flow Deflection Angle-
  • Flow Deflection Angle=(sqrt((Specific Heat Ratio Expansion Wave+1)/(Specific Heat Ratio Expansion Wave-1))*atan(sqrt(((Specific Heat Ratio Expansion Wave-1)*(Mach Number Behind Expansion Fan^2-1))/(Specific Heat Ratio Expansion Wave+1)))-atan(sqrt(Mach Number Behind Expansion Fan^2-1)))-(sqrt((Specific Heat Ratio Expansion Wave+1)/(Specific Heat Ratio Expansion Wave-1))*atan(sqrt(((Specific Heat Ratio Expansion Wave-1)*(Mach Number Ahead of Expansion Fan^2-1))/(Specific Heat Ratio Expansion Wave+1)))-atan(sqrt(Mach Number Ahead of Expansion Fan^2-1)))OpenImg
Can the Flow Deflection Angle using Prandtl Meyer Function be negative?
Yes, the Flow Deflection Angle using Prandtl Meyer Function, measured in Angle can be negative.
Which unit is used to measure Flow Deflection Angle using Prandtl Meyer Function?
Flow Deflection Angle using Prandtl Meyer Function is usually measured using the Degree[°] for Angle. Radian[°], Minute[°], Second[°] are the few other units in which Flow Deflection Angle using Prandtl Meyer Function can be measured.
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