Dynamic Viscosity around Wall Solution

STEP 0: Pre-Calculation Summary
Formula Used
Dynamic Viscosity = Static Viscosity*(Wall Temperature/Static Temperature)^(Constant n)
μviscosity = μe*(Tw/Tstatic)^(n)
This formula uses 5 Variables
Variables Used
Dynamic Viscosity - (Measured in Pascal Second) - The Dynamic Viscosity is the measure of a fluid's resistance to shear stress, affecting the boundary layer's behavior in hypersonic flow conditions.
Static Viscosity - (Measured in Pascal Second) - The Static Viscosity is a measure of a fluid's resistance to flow, describing its thickness and stickiness in the hypersonic boundary layer.
Wall Temperature - (Measured in Kelvin) - The Wall Temperature is the temperature at the surface of the wall in a hypersonic flow, which affects the flow's thermal and velocity boundary layers.
Static Temperature - (Measured in Kelvin) - The Static Temperature is the temperature of the air at a point in the boundary layer, unaffected by the heat generated by friction.
Constant n - The Constant n is a dimensionless parameter that characterizes the temperature and velocity profiles in the hypersonic boundary layer flow.
STEP 1: Convert Input(s) to Base Unit
Static Viscosity: 11.2 Poise --> 1.12 Pascal Second (Check conversion ​here)
Wall Temperature: 15 Kelvin --> 15 Kelvin No Conversion Required
Static Temperature: 350 Kelvin --> 350 Kelvin No Conversion Required
Constant n: 0.001 --> No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
μviscosity = μe*(Tw/Tstatic)^(n) --> 1.12*(15/350)^(0.001)
Evaluating ... ...
μviscosity = 1.11647768145009
STEP 3: Convert Result to Output's Unit
1.11647768145009 Pascal Second -->11.1647768145009 Poise (Check conversion ​here)
FINAL ANSWER
11.1647768145009 11.16478 Poise <-- Dynamic Viscosity
(Calculation completed in 00.004 seconds)

Credits

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Created by Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
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PSG College of Technology (PSGCT), Coimbatore
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Hypersonic Flow Parameters Calculators

Static Velocity Equation using Skin Friction Coefficient
​ LaTeX ​ Go Static Velocity = sqrt((2*Shear Stress)/(Local Skin-Friction Coefficient*Static Density))
Static Density Equation using Skin Friction Coefficient
​ LaTeX ​ Go Static Density = (2*Shear Stress)/(Local Skin-Friction Coefficient*Static Velocity^2)
Local Skin-Friction Coefficient
​ LaTeX ​ Go Local Skin-Friction Coefficient = (2*Shear Stress)/(Static Density*Static Velocity^2)
Local Shear Stress at Wall
​ LaTeX ​ Go Shear Stress = 0.5*Local Skin-Friction Coefficient*Static Density*Static Velocity^2

Dynamic Viscosity around Wall Formula

​LaTeX ​Go
Dynamic Viscosity = Static Viscosity*(Wall Temperature/Static Temperature)^(Constant n)
μviscosity = μe*(Tw/Tstatic)^(n)

What is viscosity?

Viscosity is a measure of a fluid's resistance to flow. It describes the internal friction of a moving fluid.

How to Calculate Dynamic Viscosity around Wall?

Dynamic Viscosity around Wall calculator uses Dynamic Viscosity = Static Viscosity*(Wall Temperature/Static Temperature)^(Constant n) to calculate the Dynamic Viscosity, Dynamic Viscosity around Wall formula is defined as a measure of the resistance to flow of a fluid in the boundary layer of a hypersonic flow, which is a critical parameter in understanding the behavior of fluids at high speeds. Dynamic Viscosity is denoted by μviscosity symbol.

How to calculate Dynamic Viscosity around Wall using this online calculator? To use this online calculator for Dynamic Viscosity around Wall, enter Static Viscosity e), Wall Temperature (Tw), Static Temperature (Tstatic) & Constant n (n) and hit the calculate button. Here is how the Dynamic Viscosity around Wall calculation can be explained with given input values -> 111.6478 = 1.12*(15/350)^(0.001).

FAQ

What is Dynamic Viscosity around Wall?
Dynamic Viscosity around Wall formula is defined as a measure of the resistance to flow of a fluid in the boundary layer of a hypersonic flow, which is a critical parameter in understanding the behavior of fluids at high speeds and is represented as μviscosity = μe*(Tw/Tstatic)^(n) or Dynamic Viscosity = Static Viscosity*(Wall Temperature/Static Temperature)^(Constant n). The Static Viscosity is a measure of a fluid's resistance to flow, describing its thickness and stickiness in the hypersonic boundary layer, The Wall Temperature is the temperature at the surface of the wall in a hypersonic flow, which affects the flow's thermal and velocity boundary layers, The Static Temperature is the temperature of the air at a point in the boundary layer, unaffected by the heat generated by friction & The Constant n is a dimensionless parameter that characterizes the temperature and velocity profiles in the hypersonic boundary layer flow.
How to calculate Dynamic Viscosity around Wall?
Dynamic Viscosity around Wall formula is defined as a measure of the resistance to flow of a fluid in the boundary layer of a hypersonic flow, which is a critical parameter in understanding the behavior of fluids at high speeds is calculated using Dynamic Viscosity = Static Viscosity*(Wall Temperature/Static Temperature)^(Constant n). To calculate Dynamic Viscosity around Wall, you need Static Viscosity e), Wall Temperature (Tw), Static Temperature (Tstatic) & Constant n (n). With our tool, you need to enter the respective value for Static Viscosity, Wall Temperature, Static Temperature & Constant n 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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