Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
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Rushi Shah
K J Somaiya College of Engineering (K J Somaiya), Mumbai
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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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