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Non-Dimensional Perpendicular Velocity Component for High Mach Number Formula

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Non Dimensionalized Velocity is the non dimensional form of the components of the flow velocity behind the shock wave perpendicular to the upstream flow velocity behind the shock wave. Check FAQs

v - = \frac{\sin (2 \cdot β)}{γ - 1}

v_- - Non Dimensionalized Velocity?β - Wave Angle?γ - Specific Heat Ratio?

Non-Dimensional Perpendicular Velocity Component for High Mach Number Example

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

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

Here is how the Non-Dimensional Perpendicular Velocity Component for High Mach Number equation looks like.

0.9022 = \frac{\sin (2 \cdot 0.286)}{1.6 - 1}

0.9022 = \frac{\sin (2 \cdot 0.286rad)}{1.6 - 1}

0.9022 = \frac{\sin (2 \cdot 0.286)}{1.6 - 1}

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Non-Dimensional Perpendicular Velocity Component for High Mach Number Solution

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

FIRST Step Consider the formula

v - = \frac{\sin (2 \cdot β)}{γ - 1}

Next Step Substitute values of Variables

∴

v - = \frac{\sin (2 \cdot 0.286rad)}{1.6 - 1}

Next Step Prepare to Evaluate

∴

v - = \frac{\sin (2 \cdot 0.286)}{1.6 - 1}

Next Step Evaluate

∴

v - = 0.902191283830036

LAST Step Rounding Answer

∴

v - = 0.9022

Non-Dimensional Perpendicular Velocity Component for High Mach Number Formula Elements

Variables

Functions

Non Dimensionalized Velocity

Non Dimensionalized Velocity is the non dimensional form of the components of the flow velocity behind the shock wave perpendicular to the upstream flow velocity behind the shock wave.

Symbol: v_-

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Non Dimensionalized Velocity

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 Pressure for High Mach Number

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

Go Non-Dimensional Density for High Mach Number

ρ - = \frac{γ + 1}{γ - 1}

How to Evaluate Non-Dimensional Perpendicular Velocity Component for High Mach Number?

Non-Dimensional Perpendicular Velocity Component for High Mach Number evaluator uses Non Dimensionalized Velocity = (sin(2*Wave Angle))/(Specific Heat Ratio-1) to evaluate the Non Dimensionalized Velocity, The Non-dimensional perpendicular velocity component for high mach number formula is defined as perpendicular component of the flow velocity after oblique shock occurs and Mach is infinite. Non Dimensionalized Velocity is denoted by v_- symbol.

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

FAQs on Non-Dimensional Perpendicular Velocity Component for High Mach Number

What is the formula to find Non-Dimensional Perpendicular Velocity Component for High Mach Number?

The formula of Non-Dimensional Perpendicular Velocity Component for High Mach Number is expressed as Non Dimensionalized Velocity = (sin(2*Wave Angle))/(Specific Heat Ratio-1). Here is an example- 0.902191 = (sin(2*0.286))/(1.6-1).

How to calculate Non-Dimensional Perpendicular Velocity Component for High Mach Number?

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

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Non-Dimensional Perpendicular Velocity Component for High Mach Number Formula

Non-Dimensional Perpendicular Velocity Component for High Mach Number Example

Non-Dimensional Perpendicular Velocity Component for High Mach Number Solution

Non-Dimensional Perpendicular Velocity Component for High Mach Number Formula Elements

Other formulas in Approximate Methods of Hypersonic Inviscid Flowfields category

How to Evaluate Non-Dimensional Perpendicular Velocity Component for High Mach Number?

FAQs on Non-Dimensional Perpendicular Velocity Component for High Mach Number

Variable Name