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Static Viscosity Relation using Temperature of Wall Formula

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The Static Viscosity is a measure of a fluid's resistance to flow, describing its thickness and stickiness in the hypersonic boundary layer. Check FAQs

μ e = \frac{μ viscosity}{{(\frac{Tw}{T static})}^{n}}

μ_e - Static Viscosity?μ_viscosity - Dynamic Viscosity?Tw - Wall Temperature?T_static - Static Temperature?n - Constant n?

Static Viscosity Relation using Temperature of Wall Example

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Here is how the Static Viscosity Relation using Temperature of Wall equation looks like with Values.

Here is how the Static Viscosity Relation using Temperature of Wall equation looks like with Units.

Here is how the Static Viscosity Relation using Temperature of Wall equation looks like.

10.2322 = \frac{10.2}{{(\frac{15}{350})}^{0.001}}

10.2322P = \frac{10.2P}{{(\frac{15K}{350K})}^{0.001}}

10.2322 = \frac{10.2}{{(\frac{15}{350})}^{0.001}}

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Static Viscosity Relation using Temperature of Wall Solution

Follow our step by step solution on how to calculate Static Viscosity Relation using Temperature of Wall?

FIRST Step Consider the formula

μ e = \frac{μ viscosity}{{(\frac{Tw}{T static})}^{n}}

Next Step Substitute values of Variables

∴

μ e = \frac{10.2P}{{(\frac{15K}{350K})}^{0.001}}

Next Step Convert Units

∴

μ e = \frac{1.02Pa*s}{{(\frac{15K}{350K})}^{0.001}}

Next Step Prepare to Evaluate

∴

μ e = \frac{1.02}{{(\frac{15}{350})}^{0.001}}

Next Step Evaluate

∴

μ e = 1.02321794602848Pa*s

Next Step Convert to Output's Unit

∴

μ e = 10.2321794602848P

LAST Step Rounding Answer

∴

μ e = 10.2322P

Static Viscosity Relation using Temperature of Wall Formula Elements

Variables

Static Viscosity

The Static Viscosity is a measure of a fluid's resistance to flow, describing its thickness and stickiness in the hypersonic boundary layer.

Symbol: μ_e

Measurement: Dynamic ViscosityUnit: P

Note: Value should be greater than 0.

Formulas to find Static Viscosity

Dynamic Viscosity

The Dynamic Viscosity is the measure of a fluid's resistance to shear stress, affecting the boundary layer's behavior in hypersonic flow conditions.

Symbol: μ_viscosity

Measurement: Dynamic ViscosityUnit: P

Note: Value should be greater than 0.

Formulas to find Dynamic Viscosity

Wall Temperature

The Wall Temperature is the temperature at the surface of the wall in a hypersonic flow, which affects the flow's thermal and velocity boundary layers.

Symbol: Tw

Measurement: TemperatureUnit: K

Note: Value can be positive or negative.

Formulas to find Wall Temperature

Static Temperature

The Static Temperature is the temperature of the air at a point in the boundary layer, unaffected by the heat generated by friction.

Symbol: T_static

Measurement: TemperatureUnit: K

Note: Value should be greater than 0.

Formulas to find Static Temperature

Constant n

The Constant n is a dimensionless parameter that characterizes the temperature and velocity profiles in the hypersonic boundary layer flow.

Symbol: n

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Constant n

Other formulas in Hypersonic Flow Parameters category

Go Local Skin-Friction Coefficient

C f = \frac{2 \cdot 𝜏}{ρ e \cdot {u e}^{2}}

Go Local Shear Stress at Wall

𝜏 = 0.5 \cdot C f \cdot ρ e \cdot {u e}^{2}

Go Static Density Equation using Skin Friction Coefficient

ρ e = \frac{2 \cdot 𝜏}{C f \cdot {u e}^{2}}

Go Static Velocity Equation using Skin Friction Coefficient

u e = \sqrt{\frac{2 \cdot 𝜏}{C f \cdot ρ e}}

How to Evaluate Static Viscosity Relation using Temperature of Wall?

Static Viscosity Relation using Temperature of Wall evaluator uses Static Viscosity = Dynamic Viscosity/(Wall Temperature/Static Temperature)^(Constant n) to evaluate the Static Viscosity, Static Viscosity Relation using Temperature of Wall formula is defined as a measure of the dynamic viscosity of a fluid in relation to the temperature of the wall in a hypersonic flow, which is essential in understanding the boundary layer equations and its effects on the flow. Static Viscosity is denoted by μ_e symbol.

How to evaluate Static Viscosity Relation using Temperature of Wall using this online evaluator? To use this online evaluator for Static Viscosity Relation using Temperature of Wall, enter Dynamic Viscosity (μ_viscosity), Wall Temperature (Tw), Static Temperature (T_static) & Constant n (n) and hit the calculate button.

FAQs on Static Viscosity Relation using Temperature of Wall

What is the formula to find Static Viscosity Relation using Temperature of Wall?

The formula of Static Viscosity Relation using Temperature of Wall is expressed as Static Viscosity = Dynamic Viscosity/(Wall Temperature/Static Temperature)^(Constant n). Here is an example- 102.3218 = 1.02/(15/350)^(0.001).

How to calculate Static Viscosity Relation using Temperature of Wall?

With Dynamic Viscosity (μ_viscosity), Wall Temperature (Tw), Static Temperature (T_static) & Constant n (n) we can find Static Viscosity Relation using Temperature of Wall using the formula - Static Viscosity = Dynamic Viscosity/(Wall Temperature/Static Temperature)^(Constant n).

Can the Static Viscosity Relation using Temperature of Wall be negative?

No, the Static Viscosity Relation using Temperature of Wall, measured in Dynamic Viscosity cannot be negative.

Which unit is used to measure Static Viscosity Relation using Temperature of Wall?

Static Viscosity Relation using Temperature of Wall 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 Relation using Temperature of Wall can be measured.

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Static Viscosity Relation using Temperature of Wall Formula

Static Viscosity Relation using Temperature of Wall Example

Static Viscosity Relation using Temperature of Wall Solution

Static Viscosity Relation using Temperature of Wall Formula Elements

Other formulas in Hypersonic Flow Parameters category

How to Evaluate Static Viscosity Relation using Temperature of Wall?

FAQs on Static Viscosity Relation using Temperature of Wall

Variable Name