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Static Temperature over Flat Plate under Viscous, Very High Mach Flow Formula

GoStatic Temperature over Flat Plate using Static Mach Number Formula

GoStatic Temperature of Plate using Wall Viscosity Formula

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The Static Temperature is defined as the temperature of the gas if it had no ordered motion and was not flowing. Check FAQs

T static = \frac{T w}{(\frac{γ - 1}{2}) \cdot M^{2}}

T_static - Static Temperature?T_w - Temperature of Wall in Kelvin?γ - Specific Heat Ratio?M - Mach Number?

Static Temperature over Flat Plate under Viscous, Very High Mach Flow Example

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Here is how the Static Temperature over Flat Plate under Viscous, Very High Mach Flow equation looks like with Values.

Here is how the Static Temperature over Flat Plate under Viscous, Very High Mach Flow equation looks like with Units.

Here is how the Static Temperature over Flat Plate under Viscous, Very High Mach Flow equation looks like.

132.2222 = \frac{357}{(\frac{1.6 - 1}{2}) \cdot 3^{2}}

132.2222K = \frac{357K}{(\frac{1.6 - 1}{2}) \cdot 3^{2}}

132.2222 = \frac{357}{(\frac{1.6 - 1}{2}) \cdot 3^{2}}

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Static Temperature over Flat Plate under Viscous, Very High Mach Flow Solution

Follow our step by step solution on how to calculate Static Temperature over Flat Plate under Viscous, Very High Mach Flow?

FIRST Step Consider the formula

T static = \frac{T w}{(\frac{γ - 1}{2}) \cdot M^{2}}

Next Step Substitute values of Variables

∴

T static = \frac{357K}{(\frac{1.6 - 1}{2}) \cdot 3^{2}}

Next Step Prepare to Evaluate

∴

T static = \frac{357}{(\frac{1.6 - 1}{2}) \cdot 3^{2}}

Next Step Evaluate

∴

T static = 132.222222222222K

LAST Step Rounding Answer

∴

T static = 132.2222K

Static Temperature over Flat Plate under Viscous, Very High Mach Flow Formula Elements

Variables

Static Temperature

The Static Temperature is defined as the temperature of the gas if it had no ordered motion and was not flowing.

Symbol: T_static

Measurement: TemperatureUnit: K

Note: Value should be greater than 0.

Formulas to find Static Temperature

Temperature of Wall in Kelvin

Temperature of wall in Kelvin is the wall temperature of the body under a flow.

Symbol: T_w

Measurement: TemperatureUnit: K

Note: Value should be greater than 0.

Formulas to find Temperature of Wall in Kelvin

Specific Heat Ratio

The Specific heat ratio of a gas is the ratio of the specific heat of the gas at a constant pressure to its specific heat at a constant volume.

Symbol: γ

Measurement: NAUnit: Unitless

Note: Value can be positive or negative.

Formulas to find Specific Heat Ratio

Mach Number

Mach number is a dimensionless quantity representing the ratio of flow velocity past a boundary to the local speed of sound.

Symbol: M

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Mach Number

Other Formulas to find Static Temperature

Go Static Temperature over Flat Plate using Static Mach Number

T static = \frac{Tw}{(1 + \frac{γ - 1}{2}) \cdot M^{2}}

Go Static Temperature of Plate using Wall Viscosity

T static = \frac{T w}{\frac{μ w}{μe}}

Go Static Temperature of Fluid over Flat Plate

T static = \frac{T w}{\frac{ρ e}{ρ w}}

Other formulas in Static Parameters for Hypersonic Flow category

Go Static Viscosity using Wall Temperature and Static Temperature

μe = \frac{μ w}{\frac{Tw}{T static}}

Go Static Density of Fluid over Flat Plate

ρ e = \frac{Tw}{T static} \cdot ρ w

How to Evaluate Static Temperature over Flat Plate under Viscous, Very High Mach Flow?

Static Temperature over Flat Plate under Viscous, Very High Mach Flow evaluator uses Static Temperature = Temperature of Wall in Kelvin/(((Specific Heat Ratio-1)/2)*Mach Number^2) to evaluate the Static Temperature, The Static temperature over flat plate under viscous, very high Mach flow formula is defined as the function of specific heat ratio, wall temperature, and Mach number of the flow. Static Temperature is denoted by T_static symbol.

How to evaluate Static Temperature over Flat Plate under Viscous, Very High Mach Flow using this online evaluator? To use this online evaluator for Static Temperature over Flat Plate under Viscous, Very High Mach Flow, enter Temperature of Wall in Kelvin (T_w), Specific Heat Ratio (γ) & Mach Number (M) and hit the calculate button.

FAQs on Static Temperature over Flat Plate under Viscous, Very High Mach Flow

What is the formula to find Static Temperature over Flat Plate under Viscous, Very High Mach Flow?

The formula of Static Temperature over Flat Plate under Viscous, Very High Mach Flow is expressed as Static Temperature = Temperature of Wall in Kelvin/(((Specific Heat Ratio-1)/2)*Mach Number^2). Here is an example- 132.2222 = 357/(((1.6-1)/2)*3^2).

How to calculate Static Temperature over Flat Plate under Viscous, Very High Mach Flow?

With Temperature of Wall in Kelvin (T_w), Specific Heat Ratio (γ) & Mach Number (M) we can find Static Temperature over Flat Plate under Viscous, Very High Mach Flow using the formula - Static Temperature = Temperature of Wall in Kelvin/(((Specific Heat Ratio-1)/2)*Mach Number^2).

What are the other ways to Calculate Static Temperature?

Here are the different ways to Calculate Static Temperature-

Static Temperature=Wall Temperature/((1+(Specific Heat Ratio-1)/2)*Mach Number^2)
Static Temperature=Temperature of Wall in Kelvin/(Wall Viscosity/Static Viscosity)
Static Temperature=Temperature of Wall in Kelvin/(Static Density/Wall Density)

Can the Static Temperature over Flat Plate under Viscous, Very High Mach Flow be negative?

No, the Static Temperature over Flat Plate under Viscous, Very High Mach Flow, measured in Temperature cannot be negative.

Which unit is used to measure Static Temperature over Flat Plate under Viscous, Very High Mach Flow?

Static Temperature over Flat Plate under Viscous, Very High Mach Flow is usually measured using the Kelvin[K] for Temperature. Celsius[K], Fahrenheit[K], Rankine[K] are the few other units in which Static Temperature over Flat Plate under Viscous, Very High Mach Flow can be measured.

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Static Temperature over Flat Plate under Viscous, Very High Mach Flow Formula

​GoStatic Temperature over Flat Plate using Static Mach Number Formula

​GoStatic Temperature of Plate using Wall Viscosity Formula

Static Temperature over Flat Plate under Viscous, Very High Mach Flow Example

Static Temperature over Flat Plate under Viscous, Very High Mach Flow Solution

Static Temperature over Flat Plate under Viscous, Very High Mach Flow Formula Elements

Other Formulas to find Static Temperature

Other formulas in Static Parameters for Hypersonic Flow category

How to Evaluate Static Temperature over Flat Plate under Viscous, Very High Mach Flow?

FAQs on Static Temperature over Flat Plate under Viscous, Very High Mach Flow

Variable Name

GoStatic Temperature over Flat Plate using Static Mach Number Formula

GoStatic Temperature of Plate using Wall Viscosity Formula