Static Viscosity Equation using Boundary-Layer Momentum Thickness Calculator

✖The Static Density is the mass per unit volume of a fluid at rest, crucial for understanding fluid behavior in hypersonic flow conditions.ⓘ Static Density [ρ_e]			+10% -10%
✖The Static Velocity is the velocity of a fluid at a specific point in a flow field, measured relative to the surrounding fluid at rest.ⓘ Static Velocity [u_e]			+10% -10%
✖The Boundary-Layer Momentum Thickness for Transition is a measure of the thickness of the boundary layer where viscous effects influence flow behavior during hypersonic transition.ⓘ Boundary-Layer Momentum Thickness for Transition [θt]			+10% -10%
✖The Reynolds Number is a dimensionless quantity that helps predict flow patterns in different fluid flow situations, particularly in hypersonic transitions over flat plates.ⓘ Reynolds Number [Re]			+10% -10%

✖The Static Viscosity is a measure of a fluid's resistance to flow and deformation under shear stress, particularly relevant in hypersonic transition scenarios.ⓘ Static Viscosity Equation using Boundary-Layer Momentum Thickness [μe]

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Static Viscosity Equation using Boundary-Layer Momentum Thickness Solution

STEP 0: Pre-Calculation Summary

Formula Used

Static Viscosity = (Static Density*Static Velocity*Boundary-Layer Momentum Thickness for Transition)/Reynolds Number
μe = (ρ_e*u_e*θt)/Re
This formula uses 5 Variables

Variables Used

Static Viscosity - (Measured in Pascal Second) - The Static Viscosity is a measure of a fluid's resistance to flow and deformation under shear stress, particularly relevant in hypersonic transition scenarios.
Static Density - (Measured in Kilogram per Cubic Meter) - The Static Density is the mass per unit volume of a fluid at rest, crucial for understanding fluid behavior in hypersonic flow conditions.
Static Velocity - (Measured in Meter per Second) - The Static Velocity is the velocity of a fluid at a specific point in a flow field, measured relative to the surrounding fluid at rest.
Boundary-Layer Momentum Thickness for Transition - (Measured in Meter) - The Boundary-Layer Momentum Thickness for Transition is a measure of the thickness of the boundary layer where viscous effects influence flow behavior during hypersonic transition.
Reynolds Number - The Reynolds Number is a dimensionless quantity that helps predict flow patterns in different fluid flow situations, particularly in hypersonic transitions over flat plates.

STEP 1: Convert Input(s) to Base Unit

Static Density: 98.3 Kilogram per Cubic Meter --> 98.3 Kilogram per Cubic Meter No Conversion Required
Static Velocity: 8.8 Meter per Second --> 8.8 Meter per Second No Conversion Required
Boundary-Layer Momentum Thickness for Transition: 7.768427 Meter --> 7.768427 Meter No Conversion Required
Reynolds Number: 6000 --> No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

μe = (ρ_e*u_e*θt)/Re --> (98.3*8.8*7.768427)/6000

Evaluating ... ...

μe = 1.12000001534667

STEP 3: Convert Result to Output's Unit

1.12000001534667 Pascal Second -->11.2000001534667 Poise (Check conversion here)

FINAL ANSWER

11.2000001534667 ≈ 11.2 Poise <-- Static Viscosity

(Calculation completed in 00.154 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

Static Viscosity Equation using Boundary-Layer Momentum Thickness Formula

LaTeX Go

Static Viscosity = (Static Density*Static Velocity*Boundary-Layer Momentum Thickness for Transition)/Reynolds Number
μe = (ρ_e*u_e*θt)/Re

What is Transition Reynolds Number?

Transitional or transient flow is the phase of flow that occurs between laminar and turbulent flow and corresponds to Reynolds numbers that land between 2300 and 4000. In this type of flow, there is a mixture of laminar and turbulent flows present.

How to Calculate Static Viscosity Equation using Boundary-Layer Momentum Thickness?

Static Viscosity Equation using Boundary-Layer Momentum Thickness calculator uses Static Viscosity = (Static Density*Static Velocity*Boundary-Layer Momentum Thickness for Transition)/Reynolds Number to calculate the Static Viscosity, Static Viscosity Equation using Boundary-Layer Momentum Thickness formula is defined as a measure of the dynamic viscosity of a fluid in a boundary layer, which is a critical parameter in understanding the behavior of fluids in various engineering applications, particularly in the context of flat plate viscous flow. Static Viscosity is denoted by μe symbol.

How to calculate Static Viscosity Equation using Boundary-Layer Momentum Thickness using this online calculator? To use this online calculator for Static Viscosity Equation using Boundary-Layer Momentum Thickness, enter Static Density (ρ_e), Static Velocity (u_e), Boundary-Layer Momentum Thickness for Transition (θt) & Reynolds Number (Re) and hit the calculate button. Here is how the Static Viscosity Equation using Boundary-Layer Momentum Thickness calculation can be explained with given input values -> 1.441733 = (98.3*8.8*7.768427)/6000.

FAQ

What is Static Viscosity Equation using Boundary-Layer Momentum Thickness?

Static Viscosity Equation using Boundary-Layer Momentum Thickness formula is defined as a measure of the dynamic viscosity of a fluid in a boundary layer, which is a critical parameter in understanding the behavior of fluids in various engineering applications, particularly in the context of flat plate viscous flow and is represented as μe = (ρ_e*u_e*θt)/Re or Static Viscosity = (Static Density*Static Velocity*Boundary-Layer Momentum Thickness for Transition)/Reynolds Number. The Static Density is the mass per unit volume of a fluid at rest, crucial for understanding fluid behavior in hypersonic flow conditions, The Static Velocity is the velocity of a fluid at a specific point in a flow field, measured relative to the surrounding fluid at rest, The Boundary-Layer Momentum Thickness for Transition is a measure of the thickness of the boundary layer where viscous effects influence flow behavior during hypersonic transition & The Reynolds Number is a dimensionless quantity that helps predict flow patterns in different fluid flow situations, particularly in hypersonic transitions over flat plates.

How to calculate Static Viscosity Equation using Boundary-Layer Momentum Thickness?

Static Viscosity Equation using Boundary-Layer Momentum Thickness formula is defined as a measure of the dynamic viscosity of a fluid in a boundary layer, which is a critical parameter in understanding the behavior of fluids in various engineering applications, particularly in the context of flat plate viscous flow is calculated using Static Viscosity = (Static Density*Static Velocity*Boundary-Layer Momentum Thickness for Transition)/Reynolds Number. To calculate Static Viscosity Equation using Boundary-Layer Momentum Thickness, you need Static Density (ρ_e), Static Velocity (u_e), Boundary-Layer Momentum Thickness for Transition (θt) & Reynolds Number (Re). With our tool, you need to enter the respective value for Static Density, Static Velocity, Boundary-Layer Momentum Thickness for Transition & Reynolds Number 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 Static Viscosity?

In this formula, Static Viscosity uses Static Density, Static Velocity, Boundary-Layer Momentum Thickness for Transition & Reynolds Number. We can use 1 other way(s) to calculate the same, which is/are as follows -

Static Viscosity = (Static Density*Static Velocity*Location Transition Point)/Transition Reynolds Number

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