Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
Sanjay Krishna has created this Calculator and 200+ more calculators!
Shikha Maurya
Indian Institute of Technology (IIT), Bombay
Shikha Maurya has verified this Calculator and 100+ 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
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
Mach Number
Mach Number=Speed of a body/Speed of Sound GO
Mach Angle
Mach Angle=asin(1/Mach Number) GO

Mach wave behind the shock with mach infinity Formula

Mach Number ahead of shock=Mach Number-(local shock velocity/Speed of Sound)
M<sub>1</sub>=M-(W/𝒶)
More formulas
Grid point calculation for shock waves GO
Mach wave behind the shock GO
Local shock velocity equation GO
Pressure ratio for unsteady waves GO
Pressure ratio for unsteady waves with subtracted induced mass motion for expansion waves GO
Temperature ratio for unsteady compression waves GO
Temperature ratio for unsteady expansion wave GO
New pressure after the shock formation for compression wave GO
New pressure after the shock formation, subtracted to velocity for expansion wave GO
Density before shock formation for compression wave GO
Density before the shock formation for expansion wave GO
Ratio of new and old temperature GO
Ratio of new and old temperature for expansion waves GO
Detachment distance of sphere cone GO
Nose radius of sphere cone GO
Detachment distance of cylinder-wedge GO
Nose radius of cylinder-wedge GO

what is a shock wave

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 Mach wave behind the shock with mach infinity?

Mach wave behind the shock with mach infinity calculator uses Mach Number ahead of shock=Mach Number-(local shock velocity/Speed of Sound) to calculate the Mach Number ahead of shock, The Mach wave behind the shock with mach infinity formula is defined as the interrelation between mach no at infinity, local shock velocity and speed of sound at mach infinity. Mach Number ahead of shock and is denoted by M1 symbol.

How to calculate Mach wave behind the shock with mach infinity using this online calculator? To use this online calculator for Mach wave behind the shock with mach infinity, enter Mach Number (M), local shock velocity (W) and Speed of Sound (𝒶) and hit the calculate button. Here is how the Mach wave behind the shock with mach infinity calculation can be explained with given input values -> -9 = 1-(1000/100).

FAQ

What is Mach wave behind the shock with mach infinity?
The Mach wave behind the shock with mach infinity formula is defined as the interrelation between mach no at infinity, local shock velocity and speed of sound at mach infinity and is represented as M1=M-(W/𝒶) or Mach Number ahead of shock=Mach Number-(local shock velocity/Speed of Sound). Mach number is a dimensionless quantity representing the ratio of flow velocity past a boundary to the local speed of sound, local shock velocity, is the shock velocity after the shock wave and The speed of sound is defined as the dynamic propagation of sound waves.
How to calculate Mach wave behind the shock with mach infinity?
The Mach wave behind the shock with mach infinity formula is defined as the interrelation between mach no at infinity, local shock velocity and speed of sound at mach infinity is calculated using Mach Number ahead of shock=Mach Number-(local shock velocity/Speed of Sound). To calculate Mach wave behind the shock with mach infinity, you need Mach Number (M), local shock velocity (W) and Speed of Sound (𝒶). With our tool, you need to enter the respective value for Mach Number, local shock velocity and Speed of Sound and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
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