Static Viscosity at Transition Point 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 Location Transition Point is the specific position on a flat plate where the flow transitions from laminar to hypersonic, affecting the behavior of viscous flow.ⓘ Location Transition Point [xt]			+10% -10%
✖The Transition Reynolds Number is a dimensionless quantity that characterizes the transition from laminar to turbulent flow over a flat plate in hypersonic conditions.ⓘ Transition Reynolds Number [Ret]			+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 at Transition Point [μe]

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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) - 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.
Location Transition Point - (Measured in Meter) - The Location Transition Point is the specific position on a flat plate where the flow transitions from laminar to hypersonic, affecting the behavior of viscous flow.
Transition Reynolds Number - The Transition Reynolds Number is a dimensionless quantity that characterizes the transition from laminar to turbulent flow over a flat plate in hypersonic conditions.

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: 3.236845 Meter --> 3.236845 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*3.236845)/2500

Evaluating ... ...

μe = 1.12000015952

STEP 3: Convert Result to Output's Unit

1.12000015952 Pascal Second -->11.2000015952 Poise (Check conversion here)

FINAL ANSWER

11.2000015952 ≈ 11.2 Poise <-- Static Viscosity

(Calculation completed in 00.007 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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< 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 at Transition Point Formula

LaTeX Go

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, Static Viscosity at Transition Point formula is defined as a measure of the dynamic viscosity of a fluid at the point where laminar flow transitions to turbulent flow, characterizing the fluid's resistance to shear stress in a flat plate for viscous flow case. 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*3.236845)/2500.

FAQ

What is Static Viscosity at Transition Point?

Static Viscosity at Transition Point formula is defined as a measure of the dynamic viscosity of a fluid at the point where laminar flow transitions to turbulent flow, characterizing the fluid's resistance to shear stress in a flat plate for viscous flow case and is represented as μe = (ρ_e*u_e*xt)/Ret or Static Viscosity = (Static Density*Static Velocity*Location Transition Point)/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 Location Transition Point is the specific position on a flat plate where the flow transitions from laminar to hypersonic, affecting the behavior of viscous flow & The Transition Reynolds Number is a dimensionless quantity that characterizes the transition from laminar to turbulent flow over a flat plate in hypersonic conditions.

How to calculate Static Viscosity at Transition Point?

Static Viscosity at Transition Point formula is defined as a measure of the dynamic viscosity of a fluid at the point where laminar flow transitions to turbulent flow, characterizing the fluid's resistance to shear stress in a flat plate for viscous flow case 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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