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 = (ρe*ue*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 = (ρe*ue*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 00.004 seconds)

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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 = (ρe*ue*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 e), Static Velocity (ue), 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 = (ρe*ue*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 e), Static Velocity (ue), 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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