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The Static Viscosity is a measure of a fluid's resistance to flow and deformation under shear stress, particularly relevant in hypersonic transition scenarios. Check FAQs
μe=ρeueθtRe
μe - Static Viscosity?ρe - Static Density?ue - Static Velocity?θt - Boundary-Layer Momentum Thickness for Transition?Re - Reynolds Number?

Static Viscosity Equation using Boundary-Layer Momentum Thickness Example

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With units
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Here is how the Static Viscosity Equation using Boundary-Layer Momentum Thickness equation looks like with Values.

Here is how the Static Viscosity Equation using Boundary-Layer Momentum Thickness equation looks like with Units.

Here is how the Static Viscosity Equation using Boundary-Layer Momentum Thickness equation looks like.

11.2Edit=98.3Edit8.8Edit7.7684Edit6000Edit
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Static Viscosity Equation using Boundary-Layer Momentum Thickness Solution

Follow our step by step solution on how to calculate Static Viscosity Equation using Boundary-Layer Momentum Thickness?

FIRST Step Consider the formula
μe=ρeueθtRe
Next Step Substitute values of Variables
μe=98.3kg/m³8.8m/s7.7684m6000
Next Step Prepare to Evaluate
μe=98.38.87.76846000
Next Step Evaluate
μe=1.12000001534667Pa*s
Next Step Convert to Output's Unit
μe=11.2000001534667P
LAST Step Rounding Answer
μe=11.2P

Static Viscosity Equation using Boundary-Layer Momentum Thickness Formula Elements

Variables
Static Viscosity
The Static Viscosity is a measure of a fluid's resistance to flow and deformation under shear stress, particularly relevant in hypersonic transition scenarios.
Symbol: μe
Measurement: Dynamic ViscosityUnit: P
Note: Value should be greater than 0.
Static Density
The Static Density is the mass per unit volume of a fluid at rest, crucial for understanding fluid behavior in hypersonic flow conditions.
Symbol: ρe
Measurement: DensityUnit: kg/m³
Note: Value should be greater than 0.
Static Velocity
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.
Symbol: ue
Measurement: SpeedUnit: m/s
Note: Value should be greater than 0.
Boundary-Layer Momentum Thickness for Transition
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.
Symbol: θt
Measurement: LengthUnit: m
Note: Value should be greater than 0.
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.
Symbol: Re
Measurement: NAUnit: Unitless
Note: Value should be greater than 0.

Other Formulas to find Static Viscosity

​Go Static Viscosity at Transition Point
μe=ρeuextRet

Other formulas in Hypersonic Transition category

​Go Transition Reynolds Number
Ret=ρeuextμe
​Go Static Density at Transition Point
ρe=Retμeuext
​Go Static Velocity at Transition Point
ue=Retμeρext
​Go Location of Transition Point
xt=Retμeueρe

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

Static Viscosity Equation using Boundary-Layer Momentum Thickness evaluator uses Static Viscosity = (Static Density*Static Velocity*Boundary-Layer Momentum Thickness for Transition)/Reynolds Number to evaluate 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 evaluate Static Viscosity Equation using Boundary-Layer Momentum Thickness using this online evaluator? To use this online evaluator 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.

FAQs on Static Viscosity Equation using Boundary-Layer Momentum Thickness

What is the formula to find Static Viscosity Equation using Boundary-Layer Momentum Thickness?
The formula of Static Viscosity Equation using Boundary-Layer Momentum Thickness is expressed as Static Viscosity = (Static Density*Static Velocity*Boundary-Layer Momentum Thickness for Transition)/Reynolds Number. Here is an example- 1.441733 = (98.3*8.8*7.768427)/6000.
How to calculate Static Viscosity Equation using Boundary-Layer Momentum Thickness?
With Static Density e), Static Velocity (ue), Boundary-Layer Momentum Thickness for Transition (θt) & Reynolds Number (Re) we can find Static Viscosity Equation using Boundary-Layer Momentum Thickness using the formula - Static Viscosity = (Static Density*Static Velocity*Boundary-Layer Momentum Thickness for Transition)/Reynolds Number.
What are the other ways to Calculate Static Viscosity?
Here are the different ways to Calculate Static Viscosity-
  • Static Viscosity=(Static Density*Static Velocity*Location Transition Point)/Transition Reynolds NumberOpenImg
Can the Static Viscosity Equation using Boundary-Layer Momentum Thickness be negative?
No, the Static Viscosity Equation using Boundary-Layer Momentum Thickness, measured in Dynamic Viscosity cannot be negative.
Which unit is used to measure Static Viscosity Equation using Boundary-Layer Momentum Thickness?
Static Viscosity Equation using Boundary-Layer Momentum Thickness is usually measured using the Poise[P] for Dynamic Viscosity. Pascal Second[P], Newton Second per Square Meter[P], Millinewton Second per Square Meter[P] are the few other units in which Static Viscosity Equation using Boundary-Layer Momentum Thickness can be measured.
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