Reference Viscosity Given Reference Temperature Calculator

✖Emissivity is the ability of an object to emit infrared energy. Emissivity can have a value from 0 (shiny mirror) to 1.0 (blackbody). Most organic or oxidized surfaces have emissivity close to 0.95.ⓘ Emissivity [ε]			+10% -10%
✖Freestream Density is the mass per unit volume of air far upstream of an aerodynamic body at a given altitude.ⓘ Freestream Density [ρ_∞]			+10% -10%
✖Reference Temperature is the Temperature at which the values of the physical properties of a fluid are chosen in dimensionless equations for the heat transfer, and resistance.ⓘ Reference Temperature [T_ref]			+10% -10%
✖Radius of Nose is any of the line segments from its center to its perimeter, and in more modern usage, it is also their length.ⓘ Radius of Nose [r_nose]			+10% -10%

✖The Dynamic Viscosity of a fluid is the measure of its resistance to flow when an external force is applied.ⓘ Reference Viscosity Given Reference Temperature [μ_viscosity]

⎘ Copy

👎

Formula

LaTeX

Reset

👍

Download Computational Fluid Dynamic Solutions Formulas PDF PDF Image

Reference Viscosity Given Reference Temperature Solution

STEP 0: Pre-Calculation Summary

Formula Used

Dynamic Viscosity = Emissivity^2*Freestream Density*sqrt(Reference Temperature)*Radius of Nose
μ_viscosity = ε^2*ρ_∞*sqrt(T_ref)*r_nose
This formula uses 1 Functions, 5 Variables

Functions Used

sqrt - A square root function is a function that takes a non-negative number as an input and returns the square root of the given input number., sqrt(Number)

Variables Used

Dynamic Viscosity - (Measured in Pascal Second) - The Dynamic Viscosity of a fluid is the measure of its resistance to flow when an external force is applied.
Emissivity - Emissivity is the ability of an object to emit infrared energy. Emissivity can have a value from 0 (shiny mirror) to 1.0 (blackbody). Most organic or oxidized surfaces have emissivity close to 0.95.
Freestream Density - (Measured in Kilogram per Cubic Meter) - Freestream Density is the mass per unit volume of air far upstream of an aerodynamic body at a given altitude.
Reference Temperature - (Measured in Kelvin) - Reference Temperature is the Temperature at which the values of the physical properties of a fluid are chosen in dimensionless equations for the heat transfer, and resistance.
Radius of Nose - (Measured in Meter) - Radius of Nose is any of the line segments from its center to its perimeter, and in more modern usage, it is also their length.

STEP 1: Convert Input(s) to Base Unit

Emissivity: 0.948 --> No Conversion Required
Freestream Density: 1.17 Kilogram per Cubic Meter --> 1.17 Kilogram per Cubic Meter No Conversion Required
Reference Temperature: 4652 Kelvin --> 4652 Kelvin No Conversion Required
Radius of Nose: 0.49 Meter --> 0.49 Meter No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

μ_viscosity = ε^2*ρ_∞*sqrt(T_ref)*r_nose --> 0.948^2*1.17*sqrt(4652)*0.49

Evaluating ... ...

μ_viscosity = 35.1413522672742

STEP 3: Convert Result to Output's Unit

35.1413522672742 Pascal Second -->351.413522672742 Poise (Check conversion here)

FINAL ANSWER

351.413522672742 ≈ 351.4135 Poise <-- Dynamic Viscosity

(Calculation completed in 00.004 seconds)

You are here -

Home » Engineering » Mechanical » Fluid Mechanics » Hypersonic Flow » Computational Fluid Dynamic Solutions » Reference Viscosity Given Reference Temperature

Credits

Created by Rahul

Dayanada Sagar college of Engineering (DSCE), banglore

Rahul has created this Calculator and 50+ more calculators!

Verified by Anshika Arya

National Institute Of Technology (NIT), Hamirpur

Anshika Arya has verified this Calculator and 2500+ more calculators!

< Computational Fluid Dynamic Solutions Calculators

Emissivity

LaTeX Go Emissivity = sqrt(Dynamic Viscosity/(Freestream Density*Freestream Velocity*Radius of Nose))

Freestream Velocity

LaTeX Go Freestream Velocity = Dynamic Viscosity/(Emissivity^2*Freestream Density*Radius of Nose)

Freestream Density

LaTeX Go Freestream Density = Dynamic Viscosity/(Emissivity^2*Freestream Velocity*Radius of Nose)

Reference Viscosity

LaTeX Go Dynamic Viscosity = Emissivity^2*Freestream Density*Freestream Velocity*Radius of Nose

Reference Viscosity Given Reference Temperature Formula

LaTeX Go

Dynamic Viscosity = Emissivity^2*Freestream Density*sqrt(Reference Temperature)*Radius of Nose
μ_viscosity = ε^2*ρ_∞*sqrt(T_ref)*r_nose

What is emissivity?

Emissivity is the measure of an object's ability to emit infrared energy. Emitted energy indicates the temperature of the object. Emissivity can have a value from 0.

How to Calculate Reference Viscosity Given Reference Temperature?

Reference Viscosity Given Reference Temperature calculator uses Dynamic Viscosity = Emissivity^2*Freestream Density*sqrt(Reference Temperature)*Radius of Nose to calculate the Dynamic Viscosity, The Reference Viscosity Given Reference Temperature formula is defined as the product of the square of emissivity, freestream density, the square root of the reference temperature, and the radius of the nose. Dynamic Viscosity is denoted by μ_viscosity symbol.

How to calculate Reference Viscosity Given Reference Temperature using this online calculator? To use this online calculator for Reference Viscosity Given Reference Temperature, enter Emissivity (ε), Freestream Density (ρ_∞), Reference Temperature (T_ref) & Radius of Nose (r_nose) and hit the calculate button. Here is how the Reference Viscosity Given Reference Temperature calculation can be explained with given input values -> 3528.978 = 0.948^2*1.17*sqrt(4652)*0.49.

FAQ

What is Reference Viscosity Given Reference Temperature?

The Reference Viscosity Given Reference Temperature formula is defined as the product of the square of emissivity, freestream density, the square root of the reference temperature, and the radius of the nose and is represented as μ_viscosity = ε^2*ρ_∞*sqrt(T_ref)*r_nose or Dynamic Viscosity = Emissivity^2*Freestream Density*sqrt(Reference Temperature)*Radius of Nose. Emissivity is the ability of an object to emit infrared energy. Emissivity can have a value from 0 (shiny mirror) to 1.0 (blackbody). Most organic or oxidized surfaces have emissivity close to 0.95, Freestream Density is the mass per unit volume of air far upstream of an aerodynamic body at a given altitude, Reference Temperature is the Temperature at which the values of the physical properties of a fluid are chosen in dimensionless equations for the heat transfer, and resistance & Radius of Nose is any of the line segments from its center to its perimeter, and in more modern usage, it is also their length.

How to calculate Reference Viscosity Given Reference Temperature?

The Reference Viscosity Given Reference Temperature formula is defined as the product of the square of emissivity, freestream density, the square root of the reference temperature, and the radius of the nose is calculated using Dynamic Viscosity = Emissivity^2*Freestream Density*sqrt(Reference Temperature)*Radius of Nose. To calculate Reference Viscosity Given Reference Temperature, you need Emissivity (ε), Freestream Density (ρ_∞), Reference Temperature (T_ref) & Radius of Nose (r_nose). With our tool, you need to enter the respective value for Emissivity, Freestream Density, Reference Temperature & Radius of Nose and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

How many ways are there to calculate Dynamic Viscosity?

In this formula, Dynamic Viscosity uses Emissivity, Freestream Density, Reference Temperature & Radius of Nose. We can use 1 other way(s) to calculate the same, which is/are as follows -

Dynamic Viscosity = Emissivity^2*Freestream Density*Freestream Velocity*Radius of Nose

Home

FREE PDFs

🔍 Search