Inverse of Density for Hypersonic Flow Calculator

✖The Density of a material shows the denseness of that material in a specific given area. This is taken as mass per unit volume of a given object.ⓘ Density [ρ]			+10% -10%
✖Wave Angle is the shock angle created by the oblique shock, this is not similar to the mach angle.ⓘ Wave Angle [β]			+10% -10%

✖Inverse of Density is the variable used for simplifying the equation.ⓘ Inverse of Density for Hypersonic Flow [ϵ]

⎘ Copy

👎

Formula

LaTeX

Reset

👍

Download Hypersonic Flow and Disturbances Formulas PDF PDF Image

Inverse of Density for Hypersonic Flow Solution

STEP 0: Pre-Calculation Summary

Formula Used

Inverse of Density = 1/(Density*Wave Angle)
ϵ = 1/(ρ*β)
This formula uses 3 Variables

Variables Used

Inverse of Density - (Measured in Cubic Meter per Kilogram) - Inverse of Density is the variable used for simplifying the equation.
Density - (Measured in Kilogram per Cubic Meter) - The Density of a material shows the denseness of that material in a specific given area. This is taken as mass per unit volume of a given object.
Wave Angle - (Measured in Radian) - Wave Angle is the shock angle created by the oblique shock, this is not similar to the mach angle.

STEP 1: Convert Input(s) to Base Unit

Density: 997 Kilogram per Cubic Meter --> 997 Kilogram per Cubic Meter No Conversion Required
Wave Angle: 0.286 Radian --> 0.286 Radian No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

ϵ = 1/(ρ*β) --> 1/(997*0.286)

Evaluating ... ...

ϵ = 0.00350702457021414

STEP 3: Convert Result to Output's Unit

0.00350702457021414 Cubic Meter per Kilogram --> No Conversion Required

FINAL ANSWER

0.00350702457021414 ≈ 0.003507 Cubic Meter per Kilogram <-- Inverse of Density

(Calculation completed in 00.004 seconds)

You are here -

Home » Engineering » Mechanical » Fluid Mechanics » Hypersonic Flow » Hypersonic Flow and Disturbances » Inverse of Density for Hypersonic Flow

Credits

Created by Sanjay Krishna

Amrita School of Engineering (ASE), Vallikavu

Sanjay Krishna has created this Calculator and 300+ more calculators!

Verified by Rushi Shah

K J Somaiya College of Engineering (K J Somaiya), Mumbai

Rushi Shah has verified this Calculator and 200+ more calculators!

< Hypersonic Flow and Disturbances Calculators

Coefficient of Pressure with Slenderness Ratio

LaTeX Go Pressure Coefficient = 2/Specific Heat Ratio*Mach Number^2*(Non Dimensionalized Pressure*Specific Heat Ratio*Mach Number^2*Slenderness Ratio^2-1)

Density Ratio with Similarity Constant having Slenderness Ratio

LaTeX Go Density Ratio = ((Specific Heat Ratio+1)/(Specific Heat Ratio-1))*(1/(1+2/((Specific Heat Ratio-1)*Hypersonic Similarity Parameter^2)))

Change in Velocity for Hypersonic Flow in X Direction

LaTeX Go Change in Velocity for Hypersonic Flow = Fluid Velocity-Freestream Velocity Normal

Similarity Constant Equation with Slenderness Ratio

LaTeX Go Hypersonic Similarity Parameter = Mach Number*Slenderness Ratio

Inverse of Density for Hypersonic Flow Formula

LaTeX Go

Inverse of Density = 1/(Density*Wave Angle)
ϵ = 1/(ρ*β)

What is a shock?

Shock wave, strong pressure wave in any elastic medium such as air, water, or a solid substance, produced by supersonic aircraft, explosions, lightning, or other phenomena that create violent changes in pressure

How to Calculate Inverse of Density for Hypersonic Flow?

Inverse of Density for Hypersonic Flow calculator uses Inverse of Density = 1/(Density*Wave Angle) to calculate the Inverse of Density, Inverse of Density for Hypersonic Flow formula is defined as a measure of the inverse of the product of air density and compressibility factor in hypersonic flow, which is essential in understanding the behavior of air at high speeds and its interaction with objects. Inverse of Density is denoted by ϵ symbol.

How to calculate Inverse of Density for Hypersonic Flow using this online calculator? To use this online calculator for Inverse of Density for Hypersonic Flow, enter Density (ρ) & Wave Angle (β) and hit the calculate button. Here is how the Inverse of Density for Hypersonic Flow calculation can be explained with given input values -> 0.003507 = 1/(997*0.286).

FAQ

What is Inverse of Density for Hypersonic Flow?

Inverse of Density for Hypersonic Flow formula is defined as a measure of the inverse of the product of air density and compressibility factor in hypersonic flow, which is essential in understanding the behavior of air at high speeds and its interaction with objects and is represented as ϵ = 1/(ρ*β) or Inverse of Density = 1/(Density*Wave Angle). The Density of a material shows the denseness of that material in a specific given area. This is taken as mass per unit volume of a given object & Wave Angle is the shock angle created by the oblique shock, this is not similar to the mach angle.

How to calculate Inverse of Density for Hypersonic Flow?

Inverse of Density for Hypersonic Flow formula is defined as a measure of the inverse of the product of air density and compressibility factor in hypersonic flow, which is essential in understanding the behavior of air at high speeds and its interaction with objects is calculated using Inverse of Density = 1/(Density*Wave Angle). To calculate Inverse of Density for Hypersonic Flow, you need Density (ρ) & Wave Angle (β). With our tool, you need to enter the respective value for Density & Wave Angle and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

How many ways are there to calculate Inverse of Density?

In this formula, Inverse of Density uses Density & Wave Angle. We can use 1 other way(s) to calculate the same, which is/are as follows -

Inverse of Density = (2+(Specific Heat Ratio-1)*Mach Number^2*sin(Deflection Angle)^2)/(2+(Specific Heat Ratio+1)*Mach Number^2*sin(Deflection Angle)^2)

Home

FREE PDFs

🔍 Search