Inverse of density for hypersonic flow Calculator

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Engineering	Mechanical ↺
Mechanical	Fluid Mechanics ↺
Fluid-Mechanics	Hypersonic Flow ↺
Hypersonic-Flow	Hypersonic Small-Disturbance Equations ↺

✖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 ]

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Inverse of density for hypersonic flow

Sanjay Krishna

Amrita School of Engineering (ASE), Vallikavu

Sanjay Krishna has created this Calculator and 200+ more calculators!

Rushi Shah

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

Rushi Shah has verified this Calculator and 100+ more calculators!

< 11 Other formulas that you can solve using the same Inputs

Stanton Number (using basic fluid properties)

Stanton Number=External convection heat transfer coefficient/(Specific Heat Capacity*Fluid Velocity*Density) GO

Reynolds Number for Non-Circular Tubes

Reynolds Number=Density*Fluid Velocity*Characteristic Length/Dynamic viscosity GO

Thermal Diffusivity

Thermal Diffusivity=Thermal Conductivity/(Density*Specific Heat Capacity) GO

Reynolds Number for Circular Tubes

Reynolds Number=Density*Fluid Velocity*Diameter /Dynamic viscosity GO

Inertial Force Per Unit Area

Inertial Force per unit area=(Fluid Velocity^2)*Density GO

Pressure when density and height are given

Pressure=Density*Acceleration Due To Gravity*Height GO

Turbulence

Turbulence=Density*Dynamic viscosity*Fluid Velocity GO

Molar Volume

Molar Volume=(Atomic Weight*Molar Mass)/Density GO

Momentum Diffusivity

Momentum diffusivity=Dynamic viscosity/Density GO

Number of atomic sites

Number of atomic sites=Density/Atomic Mass GO

Relative Density

Relative Density=Density/Water Density GO

< 1 Other formulas that calculate the same Output

Inverse of density for hypersonic flow using mach number

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)) GO

Inverse of density for hypersonic flow Formula

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

More formulas

Change in velocity for hypersonic flow in x direction GO

Similarity constant equation with slenderness ratio GO

Density ratio with similarity constant having slenderness ratio GO

Non dimensional Change in hypersonic disturbance velocity in x direction GO

Non dimensional Change in hypersonic disturbance velocity in y direction GO

Non dimensional pressure equation with slenderness ratio GO

Non dimensional Velocity disturbance in y direction in hypersonic flow GO

Coefficient of pressure with slenderness ratio GO

Coefficient of pressure with slenderness ratio and similarity constant GO

Similarity constant equation using the wave angle GO

Rasmussen closed-form expression for the shock-wave angle GO

Doty and Rasmussen - normal-force coefficient GO

Inverse of density for hypersonic flow using mach number GO

Constant g used for finding the location of perturbed shock GO

Non- dimensionalised time GO

Distance from tip of the leading edge to the base GO

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, The Inverse of density for hypersonic flow formula is defined as the inverse of product of the density of the flow and wave angle created by shock . Inverse of density and 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) and 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 -> 0.005747 = 1/(997*0.1745329251994).

FAQ

What is Inverse of density for hypersonic flow?

The Inverse of density for hypersonic flow formula is defined as the inverse of product of the density of the flow and wave angle created by shock 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. and 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?

The Inverse of density for hypersonic flow formula is defined as the inverse of product of the density of the flow and wave angle created by shock is calculated using Inverse of density=1/(Density*Wave angle). To calculate Inverse of density for hypersonic flow, you need Density (ρ) and Wave angle (β). With our tool, you need to enter the respective value for Density and 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 and 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))

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