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Vinay Mishra
Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune
Vinay Mishra has created this Calculator and 300+ more calculators!
Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
Sanjay Krishna 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
Relation between Characteristic Mach number and Mach number
Characteristic Mach number=((Specific heat ratio+1)/((Specific heat ratio-1)+(2/(Mach Number^2))))^0.5 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
Exact relation for pressure coefficient behind an oblique shock wave
Pressure coefficient=(4/(Specific Heat Ratio+1))*(((sin(Wave angle))^2)-(1/Mach Number^2)) GO
Ratio of Stagnation and Static Temperature
Stagnation to Static Temperature=1+(((Specific Heat Ratio-1)/2)*(Mach Number^2)) GO
Dynamic pressure for given specific heat ratio and Mach number
Dynamic Pressure=Specific heat ratio*Static pressure*(Mach Number^2)/2 GO
Hypersonic similarity parameter
Hypersonic similarity parameter=Mach Number*Flow Deflection angle GO

1 Other formulas that calculate the same Output

Mach angle for the compressible fluid flow
Mach Angle=asin(velocity of sound wave/Fluid Velocity) GO

Mach Angle Formula

Mach Angle=asin(1/Mach Number)
μ=asin(1/M)
More formulas
Speed of Sound GO
Mach Number GO
Mayer's formula GO
Stagnation Temperature GO
Thermal resistance for conduction through 2 resistances in parallel GO
Isentropic compressibility for given density and speed of sound GO

What is the Mach cone?

Mach cone is defined as the conical pressure wavefront produced by a body moving at a speed greater than that of sound.

How to Calculate Mach Angle?

Mach Angle calculator uses Mach Angle=asin(1/Mach Number) to calculate the Mach Angle, The Mach Angle depends only on the Mach number and is equal to the inverse sin of one over the Mach number. Mach Angle and is denoted by μ symbol.

How to calculate Mach Angle using this online calculator? To use this online calculator for Mach Angle, enter Mach Number (M) and hit the calculate button. Here is how the Mach Angle calculation can be explained with given input values -> 1.570796 = asin(1/1).

FAQ

What is Mach Angle?
The Mach Angle depends only on the Mach number and is equal to the inverse sin of one over the Mach number and is represented as μ=asin(1/M) or Mach Angle=asin(1/Mach Number). Mach number is a dimensionless quantity representing the ratio of flow velocity past a boundary to the local speed of sound.
How to calculate Mach Angle?
The Mach Angle depends only on the Mach number and is equal to the inverse sin of one over the Mach number is calculated using Mach Angle=asin(1/Mach Number). To calculate Mach Angle, you need Mach Number (M). With our tool, you need to enter the respective value for Mach Number 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 Mach Angle?
In this formula, Mach Angle uses Mach Number. We can use 1 other way(s) to calculate the same, which is/are as follows -
  • Mach Angle=asin(velocity of sound wave/Fluid Velocity)
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