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Non-Dimensional Pressure for High Mach Number Formula

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Non Dimensionalized Pressure For High Mech Number is the technique which can ease the analysis of the problem at hand and reduce the number of free parameters. Check FAQs

p mech = 2 \cdot \frac{{(\sin (β))}^{2}}{γ + 1}

p_mech - Non Dimensionalized Pressure For High Mech Number?β - Wave Angle?γ - Specific Heat Ratio?

Non-Dimensional Pressure for High Mach Number Example

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Here is how the Non-Dimensional Pressure for High Mach Number equation looks like with Values.

Here is how the Non-Dimensional Pressure for High Mach Number equation looks like with Units.

Here is how the Non-Dimensional Pressure for High Mach Number equation looks like.

0.0612 = 2 \cdot \frac{{(\sin (0.286))}^{2}}{1.6 + 1}

0.0612 = 2 \cdot \frac{{(\sin (0.286rad))}^{2}}{1.6 + 1}

0.0612 = 2 \cdot \frac{{(\sin (0.286))}^{2}}{1.6 + 1}

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Non-Dimensional Pressure for High Mach Number Solution

Follow our step by step solution on how to calculate Non-Dimensional Pressure for High Mach Number?

FIRST Step Consider the formula

p mech = 2 \cdot \frac{{(\sin (β))}^{2}}{γ + 1}

Next Step Substitute values of Variables

∴

p mech = 2 \cdot \frac{{(\sin (0.286rad))}^{2}}{1.6 + 1}

Next Step Prepare to Evaluate

∴

p mech = 2 \cdot \frac{{(\sin (0.286))}^{2}}{1.6 + 1}

Next Step Evaluate

∴

p mech = 0.061223066160415

LAST Step Rounding Answer

∴

p mech = 0.0612

Non-Dimensional Pressure for High Mach Number Formula Elements

Variables

Functions

Non Dimensionalized Pressure For High Mech Number

Non Dimensionalized Pressure For High Mech Number is the technique which can ease the analysis of the problem at hand and reduce the number of free parameters.

Symbol: p_mech

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Non Dimensionalized Pressure For High Mech Number

Wave Angle

Wave Angle is the shock angle created by the oblique shock, this is not similar to the mach angle.

Symbol: β

Measurement: AngleUnit: rad

Note: Value should be greater than 0.

Formulas to find Wave Angle

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 should be greater than 0.

Formulas to find Specific Heat Ratio

sin

Sine is a trigonometric function that describes the ratio of the length of the opposite side of a right triangle to the length of the hypotenuse.

Syntax: sin(Angle)

Other formulas in Approximate Methods of Hypersonic Inviscid Flowfields category

Go Non-Dimensional Pressure

p - = \frac{P}{ρ \cdot {V ∞}^{2}}

Go Non-Dimensional Density

ρ - = \frac{ρ}{ρ liq}

Go Non-Dimensional Density for High Mach Number

ρ - = \frac{γ + 1}{γ - 1}

Go Non-Dimensional Perpendicular Velocity Component for High Mach Number

v - = \frac{\sin (2 \cdot β)}{γ - 1}

How to Evaluate Non-Dimensional Pressure for High Mach Number?

Non-Dimensional Pressure for High Mach Number evaluator uses Non Dimensionalized Pressure For High Mech Number = 2*(sin(Wave Angle))^2/(Specific Heat Ratio+1) to evaluate the Non Dimensionalized Pressure For High Mech Number, Non-Dimensional Pressure for High Mach Number is a dimensionless quantity used in aerodynamics to characterize the pressure distribution on a body moving at high speeds, typically at Mach numbers greater than 0.3. It is defined as the ratio of the actual pressure to the dynamic pressure, and it helps in analyzing compressible flow phenomena. Non Dimensionalized Pressure For High Mech Number is denoted by p_mech symbol.

How to evaluate Non-Dimensional Pressure for High Mach Number using this online evaluator? To use this online evaluator for Non-Dimensional Pressure for High Mach Number, enter Wave Angle (β) & Specific Heat Ratio (γ) and hit the calculate button.

FAQs on Non-Dimensional Pressure for High Mach Number

What is the formula to find Non-Dimensional Pressure for High Mach Number?

The formula of Non-Dimensional Pressure for High Mach Number is expressed as Non Dimensionalized Pressure For High Mech Number = 2*(sin(Wave Angle))^2/(Specific Heat Ratio+1). Here is an example- 0.061223 = 2*(sin(0.286))^2/(1.6+1).

How to calculate Non-Dimensional Pressure for High Mach Number?

With Wave Angle (β) & Specific Heat Ratio (γ) we can find Non-Dimensional Pressure for High Mach Number using the formula - Non Dimensionalized Pressure For High Mech Number = 2*(sin(Wave Angle))^2/(Specific Heat Ratio+1). This formula also uses Sine (sin) function(s).

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Non-Dimensional Pressure for High Mach Number Formula

Non-Dimensional Pressure for High Mach Number Example

Non-Dimensional Pressure for High Mach Number Solution

Non-Dimensional Pressure for High Mach Number Formula Elements

Other formulas in Approximate Methods of Hypersonic Inviscid Flowfields category

How to Evaluate Non-Dimensional Pressure for High Mach Number?

FAQs on Non-Dimensional Pressure for High Mach Number

Variable Name