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) - Static viscosity, is the viscosity of continuous flow, viscosity measures the ratio of the viscous force to the inertial force on the fluid.
Static Density - (Measured in Kilogram per Cubic Meter) - Static density, is the density of the fluid when its not moving, or the density of fluid if we are moving relative to the fluid.
Static Velocity - (Measured in Meter per Second) - Static velocity is the velocity of fluid at a point in the fluid, or velocity in the continuous flow.
Boundary-layer momentum thickness for transition - (Measured in Meter) - Boundary-layer momentum thickness for transition is defined in relation to the momentum flow rate within the boundary layer.
Reynolds Number - The Reynolds number is the ratio of inertial forces to viscous forces within a fluid which is subjected to relative internal movement due to different fluid velocities.
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: 0.1 Meter --> 0.1 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*0.1)/6000
Evaluating ... ...
μe = 0.0144173333333333
STEP 3: Convert Result to Output's Unit
0.0144173333333333 Pascal Second -->0.144173333333333 Poise (Check conversion here)
FINAL ANSWER
0.144173333333333 0.144173 Poise <-- Static Viscosity
(Calculation completed in 00.004 seconds)

Credits

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

Boundary-Layer Momentum Thickness using Reynolds Number at Transition Point
Go Boundary-layer momentum thickness for transition = (Reynolds Number*Static Viscosity)/(Static Velocity*Static Density)
Static Density Equation using Boundary-Layer Momentum Thickness
Go Static Density = (Reynolds Number*Static Viscosity)/(Static Velocity*Boundary-layer momentum thickness for transition)
Static Velocity using Boundary-Layer Momentum Thickness
Go Static Velocity = (Reynolds Number*Static Viscosity)/(Static Density*Boundary-layer momentum thickness for transition)
Static Viscosity Equation using Boundary-Layer Momentum Thickness
Go Static Viscosity = (Static Density*Static Velocity*Boundary-layer momentum thickness for transition)/Reynolds Number
Reynolds Number Equation using Boundary-Layer Momentum Thickness
Go Reynolds Number = (Static Density*Static Velocity*Boundary-layer momentum thickness for transition)/Static Viscosity
Static Velocity at Transition Point
Go Static Velocity = (Transition Reynolds Number*Static Viscosity)/(Static Density*Location Transition Point)
Static Density at Transition Point
Go Static Density = (Transition Reynolds Number*Static Viscosity)/(Static Velocity*Location Transition Point)
Location of Transition Point
Go Location Transition Point = (Transition Reynolds Number*Static Viscosity)/(Static Velocity*Static Density)
Static Viscosity at Transition Point
Go Static Viscosity = (Static Density*Static Velocity*Location Transition Point)/Transition Reynolds Number
Transition Reynolds Number
Go Transition Reynolds Number = (Static Density*Static Velocity*Location Transition Point)/Static Viscosity
Specific Heat at Constant Pressure for Transient Flow
Go Molar Specific Heat Capacity at Constant Pressure = (Transient Prandtl Number*Transition Thermal Conductivity)/Eddy Viscosity
Prandtl Number of Transition Flow
Go Transient Prandtl Number = (Eddy Viscosity*Molar Specific Heat Capacity at Constant Pressure)/Transition Thermal Conductivity
Eddy Viscosity Calculation
Go Eddy Viscosity = (Transition Thermal Conductivity*Transient Prandtl Number)/Molar Specific Heat Capacity at Constant Pressure
Thermal Conductivity of Transition Flow
Go Transition Thermal Conductivity = (Eddy Viscosity*Specific Heat Capacity)/Transient Prandtl Number
Local Mach Number using Reynolds Number Equation at Transition Region
Go Local Mach Number = Boundary-layer Momentum Reynolds number/100
Reynolds Number Equation using Local Mach Number
Go Boundary-layer Momentum Reynolds number = 100*Local Mach Number

Static Viscosity Equation using Boundary-Layer Momentum Thickness Formula

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, The Static viscosity equation using boundary-layer momentum thickness formula is defined as the interrelation between static density, static velocity, viscosity, and boundary-layer momentum thickness. 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*0.1)/6000.

FAQ

What is Static Viscosity Equation using Boundary-Layer Momentum Thickness?
The Static viscosity equation using boundary-layer momentum thickness formula is defined as the interrelation between static density, static velocity, viscosity, and boundary-layer momentum thickness and is represented as μe = (ρe*ue*θt)/Re or Static Viscosity = (Static Density*Static Velocity*Boundary-layer momentum thickness for transition)/Reynolds Number. Static density, is the density of the fluid when its not moving, or the density of fluid if we are moving relative to the fluid, Static velocity is the velocity of fluid at a point in the fluid, or velocity in the continuous flow, Boundary-layer momentum thickness for transition is defined in relation to the momentum flow rate within the boundary layer & The Reynolds number is the ratio of inertial forces to viscous forces within a fluid which is subjected to relative internal movement due to different fluid velocities.
How to calculate Static Viscosity Equation using Boundary-Layer Momentum Thickness?
The Static viscosity equation using boundary-layer momentum thickness formula is defined as the interrelation between static density, static velocity, viscosity, and boundary-layer momentum thickness 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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