Wall Temperature using Reference Temperature Calculator

✖The Static Temperature is the temperature of a fluid measured at rest, providing essential information about the thermal state in hypersonic flow scenarios.ⓘ Static Temperature [T_e]			+10% -10%
✖The Reference temperature is a specific temperature used as a baseline for analyzing thermodynamic properties in hypersonic flow scenarios, particularly for viscous flow over flat plates.ⓘ Reference temperature [T_ref]			+10% -10%
✖The Mach Number is a dimensionless quantity representing the ratio of the speed of an object to the speed of sound in the surrounding medium.ⓘ Mach Number [M]			+10% -10%

✖The Wall Temperature is the temperature at the surface of a wall in a hypersonic flow, influencing heat transfer and fluid dynamics in viscous flow cases.ⓘ Wall Temperature using Reference Temperature [Tw]

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Wall Temperature using Reference Temperature Solution

STEP 0: Pre-Calculation Summary

Formula Used

Wall Temperature = Static Temperature*((Reference temperature/Static Temperature-(1+0.032*Mach Number^2))/0.58+1)
Tw = T_e*((T_ref/T_e-(1+0.032*M^2))/0.58+1)
This formula uses 4 Variables

Variables Used

Wall Temperature - (Measured in Kelvin) - The Wall Temperature is the temperature at the surface of a wall in a hypersonic flow, influencing heat transfer and fluid dynamics in viscous flow cases.
Static Temperature - (Measured in Kelvin) - The Static Temperature is the temperature of a fluid measured at rest, providing essential information about the thermal state in hypersonic flow scenarios.
Reference temperature - (Measured in Kelvin) - The Reference temperature is a specific temperature used as a baseline for analyzing thermodynamic properties in hypersonic flow scenarios, particularly for viscous flow over flat plates.
Mach Number - (Measured in Meter per Second) - The Mach Number is a dimensionless quantity representing the ratio of the speed of an object to the speed of sound in the surrounding medium.

STEP 1: Convert Input(s) to Base Unit

Static Temperature: 350 Kelvin --> 350 Kelvin No Conversion Required
Reference temperature: 200.5 Kelvin --> 200.5 Kelvin No Conversion Required
Mach Number: 2 Meter per Second --> 2 Meter per Second No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

Tw = T_e*((T_ref/T_e-(1+0.032*M^2))/0.58+1) --> 350*((200.5/350-(1+0.032*2^2))/0.58+1)

Evaluating ... ...

Tw = 14.9999999999999

STEP 3: Convert Result to Output's Unit

14.9999999999999 Kelvin --> No Conversion Required

FINAL ANSWER

14.9999999999999 ≈ 15 Kelvin <-- Wall Temperature

(Calculation completed in 00.004 seconds)

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Created by Sanjay Krishna

Amrita School of Engineering (ASE), Vallikavu

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Verified by Maiarutselvan V

PSG College of Technology (PSGCT), Coimbatore

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Wall Temperature using Reference Temperature Formula

LaTeX Go

Wall Temperature = Static Temperature*((Reference temperature/Static Temperature-(1+0.032*Mach Number^2))/0.58+1)
Tw = T_e*((T_ref/T_e-(1+0.032*M^2))/0.58+1)

What is Reference Temperature?

The heat transfer coefficient or film coefficient, or film effectiveness, in thermodynamics and in mechanics is the proportionality constant between the heat flux and the thermodynamic driving force for the flow of heat.

How to Calculate Wall Temperature using Reference Temperature?

Wall Temperature using Reference Temperature calculator uses Wall Temperature = Static Temperature*((Reference temperature/Static Temperature-(1+0.032*Mach Number^2))/0.58+1) to calculate the Wall Temperature, Wall Temperature using Reference Temperature formula is defined as a method to estimate the temperature at the wall of a flat plate in a viscous flow case, which is essential in understanding the heat transfer and fluid dynamics in various engineering applications. Wall Temperature is denoted by Tw symbol.

How to calculate Wall Temperature using Reference Temperature using this online calculator? To use this online calculator for Wall Temperature using Reference Temperature, enter Static Temperature (T_e), Reference temperature (T_ref) & Mach Number (M) and hit the calculate button. Here is how the Wall Temperature using Reference Temperature calculation can be explained with given input values -> 15 = 350*((200.5/350-(1+0.032*2^2))/0.58+1).

FAQ

What is Wall Temperature using Reference Temperature?

Wall Temperature using Reference Temperature formula is defined as a method to estimate the temperature at the wall of a flat plate in a viscous flow case, which is essential in understanding the heat transfer and fluid dynamics in various engineering applications and is represented as Tw = T_e*((T_ref/T_e-(1+0.032*M^2))/0.58+1) or Wall Temperature = Static Temperature*((Reference temperature/Static Temperature-(1+0.032*Mach Number^2))/0.58+1). The Static Temperature is the temperature of a fluid measured at rest, providing essential information about the thermal state in hypersonic flow scenarios, The Reference temperature is a specific temperature used as a baseline for analyzing thermodynamic properties in hypersonic flow scenarios, particularly for viscous flow over flat plates & The Mach Number is a dimensionless quantity representing the ratio of the speed of an object to the speed of sound in the surrounding medium.

How to calculate Wall Temperature using Reference Temperature?

Wall Temperature using Reference Temperature formula is defined as a method to estimate the temperature at the wall of a flat plate in a viscous flow case, which is essential in understanding the heat transfer and fluid dynamics in various engineering applications is calculated using Wall Temperature = Static Temperature*((Reference temperature/Static Temperature-(1+0.032*Mach Number^2))/0.58+1). To calculate Wall Temperature using Reference Temperature, you need Static Temperature (T_e), Reference temperature (T_ref) & Mach Number (M). With our tool, you need to enter the respective value for Static Temperature, Reference temperature & Mach 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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