Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
Sanjay Krishna has created this Calculator and 300+ 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

Mach Number behind the shock
Mach Number behind shock=((2+(Specific heat ratio*(Mach Number ahead of shock^2))-(Mach Number ahead of shock^2))/((2*Specific heat ratio*(Mach Number ahead of shock^2))-Specific heat ratio+1))^(1/2) GO
Velocity behind a normal shock
Velocity downstream of shock=Velocity upstream of shock/((Specific heat ratio+1)/((Specific heat ratio-1)+(2/(Mach Number ahead of shock^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
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
Component of Upstream Mach normal to oblique shock
Component of upstream mach normal to oblique shock=Mach Number ahead of shock*sin(Oblique shock angle) GO
Shock strength
Shock Strength=(2*Specific heat ratio/(1+Specific heat ratio))*((Mach Number ahead of shock^2)-1) GO
Ratio of Stagnation and Static Temperature
Stagnation to Static Temperature=1+(((Specific Heat Ratio-1)/2)*(Mach Number^2)) GO
Mach Number
Mach Number=Speed of a body/Speed of Sound GO
Mach Angle
Mach Angle=asin(1/Mach Number) GO

Local shock velocity equation Formula

local shock velocity=Speed of Sound*(Mach Number-Mach Number ahead of shock)
W=𝒶*(M-M<sub>1</sub>)
More formulas
Grid point calculation for shock waves GO
Mach wave behind the shock GO
Mach wave behind the shock with mach infinity 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 Local shock velocity equation?

Local shock velocity equation calculator uses local shock velocity=Speed of Sound*(Mach Number-Mach Number ahead of shock) to calculate the local shock velocity, The Local shock velocity equation formula is defined as the product of sound at mach infinity and the subtraction of mach number at infinity and mach number after shock formation. local shock velocity and is denoted by W symbol.

How to calculate Local shock velocity equation using this online calculator? To use this online calculator for Local shock velocity equation, enter Speed of Sound (𝒶), Mach Number (M) and Mach Number ahead of shock (M1) and hit the calculate button. Here is how the Local shock velocity equation calculation can be explained with given input values -> -50 = 100*(1-1.5).

FAQ

What is Local shock velocity equation?
The Local shock velocity equation formula is defined as the product of sound at mach infinity and the subtraction of mach number at infinity and mach number after shock formation and is represented as W=𝒶*(M-M1) or local shock velocity=Speed of Sound*(Mach Number-Mach Number ahead of shock). The speed of sound is defined as the dynamic propagation of sound waves, Mach number is a dimensionless quantity representing the ratio of flow velocity past a boundary to the local speed of sound and Mach Number ahead of shock is the Mach number over the body before a shockwave has occurred .
How to calculate Local shock velocity equation?
The Local shock velocity equation formula is defined as the product of sound at mach infinity and the subtraction of mach number at infinity and mach number after shock formation is calculated using local shock velocity=Speed of Sound*(Mach Number-Mach Number ahead of shock). To calculate Local shock velocity equation, you need Speed of Sound (𝒶), Mach Number (M) and Mach Number ahead of shock (M1). With our tool, you need to enter the respective value for Speed of Sound, Mach Number and Mach Number ahead of shock 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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