Thermal Conductivity of Transition Flow Solution

STEP 0: Pre-Calculation Summary
Formula Used
Transition Thermal Conductivity = (Eddy Viscosity*Specific Heat Capacity)/Transient Prandtl Number
kT = (μT*c)/PrT
This formula uses 4 Variables
Variables Used
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.
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.
Specific Heat Capacity - (Measured in Joule per Kilogram per K) - The Specific Heat Capacity is the amount of heat energy required to raise the temperature of a unit mass of a substance by one degree Celsius.
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.
STEP 1: Convert Input(s) to Base Unit
Eddy Viscosity: 22.03279 Poise --> 2.203279 Pascal Second (Check conversion ​here)
Specific Heat Capacity: 0.122 Kilojoule per Kilogram per K --> 122 Joule per Kilogram per K (Check conversion ​here)
Transient Prandtl Number: 2.4 --> No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
kT = (μT*c)/PrT --> (2.203279*122)/2.4
Evaluating ... ...
kT = 112.000015833333
STEP 3: Convert Result to Output's Unit
112.000015833333 Watt per Meter per K --> No Conversion Required
FINAL ANSWER
112.000015833333 112 Watt per Meter per K <-- Transition Thermal Conductivity
(Calculation completed in 00.004 seconds)

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Amrita School of Engineering (ASE), Vallikavu
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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

Thermal Conductivity of Transition Flow Formula

​LaTeX ​Go
Transition Thermal Conductivity = (Eddy Viscosity*Specific Heat Capacity)/Transient Prandtl Number
kT = (μT*c)/PrT

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 Thermal Conductivity of Transition Flow?

Thermal Conductivity of Transition Flow calculator uses Transition Thermal Conductivity = (Eddy Viscosity*Specific Heat Capacity)/Transient Prandtl Number to calculate the Transition Thermal Conductivity, Thermal Conductivity of Transition Flow formula is defined as a measure of the ability of a fluid to conduct heat in a transitional flow regime, where the flow is neither fully laminar nor fully turbulent, and is commonly used in the context of flat plate viscous flow. Transition Thermal Conductivity is denoted by kT symbol.

How to calculate Thermal Conductivity of Transition Flow using this online calculator? To use this online calculator for Thermal Conductivity of Transition Flow, enter Eddy Viscosity T), Specific Heat Capacity (c) & Transient Prandtl Number (PrT) and hit the calculate button. Here is how the Thermal Conductivity of Transition Flow calculation can be explained with given input values -> 1120 = (2.203279*122)/2.4.

FAQ

What is Thermal Conductivity of Transition Flow?
Thermal Conductivity of Transition Flow formula is defined as a measure of the ability of a fluid to conduct heat in a transitional flow regime, where the flow is neither fully laminar nor fully turbulent, and is commonly used in the context of flat plate viscous flow and is represented as kT = (μT*c)/PrT or Transition Thermal Conductivity = (Eddy Viscosity*Specific Heat Capacity)/Transient Prandtl Number. The Eddy Viscosity is a measure of the turbulent momentum transfer in a fluid, influencing the flow characteristics around surfaces in hypersonic conditions, The Specific Heat Capacity is the amount of heat energy required to raise the temperature of a unit mass of a substance by one degree Celsius & The Transient Prandtl Number is a dimensionless quantity that characterizes the relationship between thermal and momentum diffusivity in transient heat transfer during hypersonic flow.
How to calculate Thermal Conductivity of Transition Flow?
Thermal Conductivity of Transition Flow formula is defined as a measure of the ability of a fluid to conduct heat in a transitional flow regime, where the flow is neither fully laminar nor fully turbulent, and is commonly used in the context of flat plate viscous flow is calculated using Transition Thermal Conductivity = (Eddy Viscosity*Specific Heat Capacity)/Transient Prandtl Number. To calculate Thermal Conductivity of Transition Flow, you need Eddy Viscosity T), Specific Heat Capacity (c) & Transient Prandtl Number (PrT). With our tool, you need to enter the respective value for Eddy Viscosity, Specific Heat Capacity & Transient Prandtl Number 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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