Static Viscosity at Transition Point Calculator

✖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 Density [ρ_e]			+10% -10%
✖Static velocity is the velocity of fluid at a point in the fluid, or velocity in the continuous flow.ⓘ Static Velocity [u_e]			+10% -10%
✖Location transition point is the location where the transition of laminar to turbulent occurs nd used to find the Reynolds number there.ⓘ Location Transition Point [xt]			+10% -10%
✖Transition Reynolds number is 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.ⓘ Transition Reynolds Number [Ret]			+10% -10%

✖Static viscosity, is the viscosity of continuous flow, viscosity measures the ratio of the viscous force to the inertial force on the fluid.ⓘ Static Viscosity at Transition Point [μe]

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Formula

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Static Viscosity at Transition Point

Formula

`"μe" = ("ρ"_{"e"}*"u"_{"e"}*"xt")/"Ret"`

Example

`"41.52192P"=("98.3kg/m³"*"8.8m/s"*"12m")/"2500"`

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Static Viscosity at Transition Point Solution

STEP 0: Pre-Calculation Summary

Formula Used

Static Viscosity = (Static Density*Static Velocity*Location Transition Point)/Transition Reynolds Number
μe = (ρ_e*u_e*xt)/Ret
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.
Location Transition Point - (Measured in Meter) - Location transition point is the location where the transition of laminar to turbulent occurs nd used to find the Reynolds number there.
Transition Reynolds Number - Transition Reynolds number is 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.

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
Location Transition Point: 12 Meter --> 12 Meter No Conversion Required
Transition Reynolds Number: 2500 --> No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

μe = (ρ_e*u_e*xt)/Ret --> (98.3*8.8*12)/2500

Evaluating ... ...

μe = 4.152192

STEP 3: Convert Result to Output's Unit

4.152192 Pascal Second -->41.52192 Poise (Check conversion here)

FINAL ANSWER

41.52192 Poise <-- Static Viscosity

(Calculation completed in 00.004 seconds)

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Created by Sanjay Krishna

Amrita School of Engineering (ASE), Vallikavu

Sanjay Krishna has created this Calculator and 300+ more calculators!

Verified by Maiarutselvan V

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 at Transition Point Formula

Static Viscosity = (Static Density*Static Velocity*Location Transition Point)/Transition Reynolds Number
μe = (ρ_e*u_e*xt)/Ret

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 at Transition Point?

Static Viscosity at Transition Point calculator uses Static Viscosity = (Static Density*Static Velocity*Location Transition Point)/Transition Reynolds Number to calculate the Static Viscosity, The Static viscosity at transition point formula is defined as the interrelation between static density, static velocity, viscosity, and location of the transition point. Static Viscosity is denoted by μe symbol.

How to calculate Static Viscosity at Transition Point using this online calculator? To use this online calculator for Static Viscosity at Transition Point, enter Static Density (ρ_e), Static Velocity (u_e), Location Transition Point (xt) & Transition Reynolds Number (Ret) and hit the calculate button. Here is how the Static Viscosity at Transition Point calculation can be explained with given input values -> 415.2192 = (98.3*8.8*12)/2500.

FAQ

What is Static Viscosity at Transition Point?

The Static viscosity at transition point formula is defined as the interrelation between static density, static velocity, viscosity, and location of the transition point and is represented as μe = (ρ_e*u_e*xt)/Ret or Static Viscosity = (Static Density*Static Velocity*Location Transition Point)/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, Location transition point is the location where the transition of laminar to turbulent occurs nd used to find the Reynolds number there & Transition Reynolds number is 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.

How to calculate Static Viscosity at Transition Point?

The Static viscosity at transition point formula is defined as the interrelation between static density, static velocity, viscosity, and location of the transition point is calculated using Static Viscosity = (Static Density*Static Velocity*Location Transition Point)/Transition Reynolds Number. To calculate Static Viscosity at Transition Point, you need Static Density (ρ_e), Static Velocity (u_e), Location Transition Point (xt) & Transition Reynolds Number (Ret). With our tool, you need to enter the respective value for Static Density, Static Velocity, Location Transition Point & 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, Location Transition Point & 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*Boundary-layer momentum thickness for transition)/Reynolds Number

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