Eddy Viscosity Calculation Solution

STEP 0: Pre-Calculation Summary
Formula Used
Eddy Viscosity = (Transition Thermal Conductivity*Transient Prandtl Number)/Molar Specific Heat Capacity at Constant Pressure
μT = (kT*PrT)/Cp molar
This formula uses 4 Variables
Variables Used
Eddy Viscosity - (Measured in Pascal Second) - The Eddy Viscosity is a measure of the turbulent momentum transfer in a fluid, influencing the flow characteristics around surfaces in hypersonic conditions.
Transition Thermal Conductivity - (Measured in Watt per Meter per K) - The Transition Thermal Conductivity is the measure of heat transfer through a material during the transition phase in hypersonic flow over a flat plate.
Transient Prandtl Number - The Transient Prandtl Number is a dimensionless quantity that characterizes the relationship between thermal and momentum diffusivity in transient heat transfer during hypersonic flow.
Molar Specific Heat Capacity at Constant Pressure - (Measured in Joule Per Kelvin Per Mole) - The Molar Specific Heat Capacity at Constant Pressure is the amount of heat required to raise the temperature of one mole of a substance at constant pressure.
STEP 1: Convert Input(s) to Base Unit
Transition Thermal Conductivity: 112 Watt per Meter per K --> 112 Watt per Meter per K No Conversion Required
Transient Prandtl Number: 2.4 --> No Conversion Required
Molar Specific Heat Capacity at Constant Pressure: 122 Joule Per Kelvin Per Mole --> 122 Joule Per Kelvin Per Mole No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
μT = (kT*PrT)/Cp molar --> (112*2.4)/122
Evaluating ... ...
μT = 2.20327868852459
STEP 3: Convert Result to Output's Unit
2.20327868852459 Pascal Second -->22.0327868852459 Poise (Check conversion ​here)
FINAL ANSWER
22.0327868852459 22.03279 Poise <-- Eddy Viscosity
(Calculation completed in 00.004 seconds)

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Hypersonic Transition Calculators

Static Velocity at Transition Point
​ LaTeX ​ Go Static Velocity = (Transition Reynolds Number*Static Viscosity)/(Static Density*Location Transition Point)
Static Density at Transition Point
​ LaTeX ​ Go Static Density = (Transition Reynolds Number*Static Viscosity)/(Static Velocity*Location Transition Point)
Location of Transition Point
​ LaTeX ​ Go Location Transition Point = (Transition Reynolds Number*Static Viscosity)/(Static Velocity*Static Density)
Transition Reynolds Number
​ LaTeX ​ Go Transition Reynolds Number = (Static Density*Static Velocity*Location Transition Point)/Static Viscosity

Eddy Viscosity Calculation Formula

​LaTeX ​Go
Eddy Viscosity = (Transition Thermal Conductivity*Transient Prandtl Number)/Molar Specific Heat Capacity at Constant Pressure
μT = (kT*PrT)/Cp molar

What is Prandtl Number?

The Prandtl Number is a dimensionless number approximating the ratio of momentum diffusivity to thermal diffusivity. The Prandtl Number is often used in heat transfer and free and forced convection calculations. It depends on the fluid properties.

How to Calculate Eddy Viscosity Calculation?

Eddy Viscosity Calculation calculator uses Eddy Viscosity = (Transition Thermal Conductivity*Transient Prandtl Number)/Molar Specific Heat Capacity at Constant Pressure to calculate the Eddy Viscosity, Eddy Viscosity Calculation formula is defined as a measure of the turbulent flow's ability to transfer momentum, which is essential in understanding the behavior of fluids in various engineering applications, particularly in the context of flat plate viscous flow. Eddy Viscosity is denoted by μT symbol.

How to calculate Eddy Viscosity Calculation using this online calculator? To use this online calculator for Eddy Viscosity Calculation, enter Transition Thermal Conductivity (kT), Transient Prandtl Number (PrT) & Molar Specific Heat Capacity at Constant Pressure (Cp molar) and hit the calculate button. Here is how the Eddy Viscosity Calculation calculation can be explained with given input values -> 220.3279 = (112*2.4)/122.

FAQ

What is Eddy Viscosity Calculation?
Eddy Viscosity Calculation formula is defined as a measure of the turbulent flow's ability to transfer momentum, which is essential in understanding the behavior of fluids in various engineering applications, particularly in the context of flat plate viscous flow and is represented as μT = (kT*PrT)/Cp molar or Eddy Viscosity = (Transition Thermal Conductivity*Transient Prandtl Number)/Molar Specific Heat Capacity at Constant Pressure. The Transition Thermal Conductivity is the measure of heat transfer through a material during the transition phase in hypersonic flow over a flat plate, The Transient Prandtl Number is a dimensionless quantity that characterizes the relationship between thermal and momentum diffusivity in transient heat transfer during hypersonic flow & The Molar Specific Heat Capacity at Constant Pressure is the amount of heat required to raise the temperature of one mole of a substance at constant pressure.
How to calculate Eddy Viscosity Calculation?
Eddy Viscosity Calculation formula is defined as a measure of the turbulent flow's ability to transfer momentum, which is essential in understanding the behavior of fluids in various engineering applications, particularly in the context of flat plate viscous flow is calculated using Eddy Viscosity = (Transition Thermal Conductivity*Transient Prandtl Number)/Molar Specific Heat Capacity at Constant Pressure. To calculate Eddy Viscosity Calculation, you need Transition Thermal Conductivity (kT), Transient Prandtl Number (PrT) & Molar Specific Heat Capacity at Constant Pressure (Cp molar). With our tool, you need to enter the respective value for Transition Thermal Conductivity, Transient Prandtl Number & Molar Specific Heat Capacity at Constant Pressure and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
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