Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
Sanjay Krishna has created this Calculator and 300+ more calculators!
Maiarutselvan V
PSG College of Technology (PSGCT), Coimbatore
Maiarutselvan V has verified this Calculator and 200+ more calculators!

11 Other formulas that you can solve using the same Inputs

Exact Density Ratio
Density ratio=((Specific Heat Ratio+1)*((Mach Number*(sin(Wave angle)))^2))/((Specific Heat Ratio-1)*((Mach Number*(sin(Wave angle)))^2)+2) GO
Temperature ratio when Mach becomes infinite
Temperature Ratio=(2*Specific Heat Ratio*(Specific Heat Ratio-1))*((Mach Number*sin(Wave angle))^2)/(Specific Heat Ratio+1)^2 GO
Ratio of stagnation and static pressure
Stagnation to Static Pressure=(1+(((Specific Heat Ratio-1)/2)*(Mach Number^2)))^(Specific Heat Ratio/(Specific Heat Ratio-1)) GO
Ratio of Stagnation and Static Density
Stagnation to Static Density=(1+(((Specific Heat Ratio-1)/2)*(Mach Number^2)))^(1/(Specific Heat Ratio-1)) GO
Deflection angle
deflection angle=(2/(Specific Heat Ratio-1))*((1/Mach Number ahead of shock)-(1/Mach Number behind shock)) GO
Exact pressure ratio
pressure ratio=1+(2*Specific Heat Ratio/(Specific Heat Ratio+1))*(((Mach Number*sin(Wave angle))^2)-1) GO
Pressure ratio when Mach becomes infinite
pressure ratio=(2*Specific Heat Ratio/(Specific Heat Ratio+1))*((Mach Number*sin(Wave angle))^2) GO
Mach number
Mach Number=Fluid Velocity/(sqrt(Specific Heat Ratio*Universal Gas Constant*final temp.)) GO
Ratio of Stagnation and Static Temperature
Stagnation to Static Temperature=1+(((Specific Heat Ratio-1)/2)*(Mach Number^2)) GO
Speed of Sound
Speed of Sound=sqrt(Specific Heat Ratio*[R-Dry-Air]*Temperature of Gas) GO
Density ratio when Mach become infinite
Density ratio=(Specific Heat Ratio+1)/(Specific Heat Ratio-1) GO

2 Other formulas that calculate the same Output

Non dimensional pressure equation with slenderness ratio
Non-dimensionalized Pressure=Pressure/(Specific Heat Ratio*(Mach Number^2)*(Slenderness Ratio^2)*Free stream Pressure) GO
Non-dimensional pressure
Non-dimensionalized Pressure=Pressure/(Density*(Freestream Velocity)^2) GO

Non-dimensional pressure for high mach number Formula

Non-dimensionalized Pressure=(2*(sin(Wave angle)^2))/(Specific Heat Ratio+1)
p-=(2*(sin(β)^2))/(γ+1)
More formulas
Non-dimensional pressure GO
Non-dimensional density GO
Non-dimensional density for high mach number GO
Non-dimensional parallel velocity component for high mach number GO
Non-dimensional perpendicular velocity component for high mach number GO
Coefficient of pressure with slenderness ratio GO
Non dimensional radius for hypersonic vehicles GO
Transformed conical variable GO
Transformed conical variable with wave angle GO
Slenderness ratio with cone radius for hypersonic vehicle GO
Transformed conical variable with cone angle in hypersonic flow GO

What is Non-dimensionalization ?

n fluid mechanics, non-dimensionalization of the Navier–Stokes equations is the conversion of the Navier–Stokes equation to a nondimensional form. This technique can ease the analysis of the problem at hand, and reduce the number of free parameters

How to Calculate Non-dimensional pressure for high mach number?

Non-dimensional pressure for high mach number calculator uses Non-dimensionalized Pressure=(2*(sin(Wave angle)^2))/(Specific Heat Ratio+1) to calculate the Non-dimensionalized Pressure, The Non-dimensional pressure for high mach number formula is defined as the ratio of double the square of wave angle to the specific heat ratio. Non-dimensionalized Pressure and is denoted by p- symbol.

How to calculate Non-dimensional pressure for high mach number using this online calculator? To use this online calculator for Non-dimensional pressure for high mach number, enter Wave angle (β) and Specific Heat Ratio (γ) and hit the calculate button. Here is how the Non-dimensional pressure for high mach number calculation can be explained with given input values -> 0.023195 = (2*(sin(10)^2))/(1.6+1).

FAQ

What is Non-dimensional pressure for high mach number?
The Non-dimensional pressure for high mach number formula is defined as the ratio of double the square of wave angle to the specific heat ratio and is represented as p-=(2*(sin(β)^2))/(γ+1) or Non-dimensionalized Pressure=(2*(sin(Wave angle)^2))/(Specific Heat Ratio+1). Wave angle is the shock angle created by the oblique shock, this is not similar to the mach angle and 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.
How to calculate Non-dimensional pressure for high mach number?
The Non-dimensional pressure for high mach number formula is defined as the ratio of double the square of wave angle to the specific heat ratio is calculated using Non-dimensionalized Pressure=(2*(sin(Wave angle)^2))/(Specific Heat Ratio+1). To calculate Non-dimensional pressure for high mach number, you need Wave angle (β) and Specific Heat Ratio (γ). With our tool, you need to enter the respective value for Wave angle and Specific Heat Ratio 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 Non-dimensionalized Pressure?
In this formula, Non-dimensionalized Pressure uses Wave angle and Specific Heat Ratio. We can use 2 other way(s) to calculate the same, which is/are as follows -
  • Non-dimensionalized Pressure=Pressure/(Density*(Freestream Velocity)^2)
  • Non-dimensionalized Pressure=Pressure/(Specific Heat Ratio*(Mach Number^2)*(Slenderness Ratio^2)*Free stream Pressure)
Share Image
Let Others Know
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!