Local Shock Velocity Equation Solution

STEP 0: Pre-Calculation Summary
Formula Used
Local Shock Velocity = Speed of Sound*(Mach Number-Mach Number ahead of shock)
W = cspeed*(M-M1)
This formula uses 4 Variables
Variables Used
Local Shock Velocity - (Measured in Meter per Second) - Local shock velocity, is the shock velocity after the shock wave.
Speed of Sound - (Measured in Meter per Second) - The speed of sound is defined as the dynamic propagation of sound waves.
Mach Number - Mach number is a dimensionless quantity representing the ratio of flow velocity past a boundary to the local speed of sound.
Mach Number ahead of shock - Mach Number ahead of shock is the Mach number over the body before a shockwave has occurred.
STEP 1: Convert Input(s) to Base Unit
Speed of Sound: 343 Meter per Second --> 343 Meter per Second No Conversion Required
Mach Number: 8 --> No Conversion Required
Mach Number ahead of shock: 1.5 --> No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
W = cspeed*(M-M1) --> 343*(8-1.5)
Evaluating ... ...
W = 2229.5
STEP 3: Convert Result to Output's Unit
2229.5 Meter per Second --> No Conversion Required
FINAL ANSWER
2229.5 Meter per Second <-- Local Shock Velocity
(Calculation completed in 00.020 seconds)

Credits

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Created by Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
Sanjay Krishna has created this Calculator and 300+ more calculators!
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Verified by Shikha Maurya
Indian Institute of Technology (IIT), Bombay
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10+ Shock Dynamics and Aerodynamic Shape Calculators

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​ Go Pressure Ratio = (1+((Specific Heat Ratio-1)/2)*(Induced Mass Motion/Speed of Sound))^(2*Specific Heat Ratio/(Specific Heat Ratio-1))
Ratio of New and Old Temperature
​ Go Temperature Ratio across Shock = (1+((Specific Heat Ratio-1)/2)*(Normal velocity/Old Speed of Sound))^(2)
Grid Point Calculation for Shock Waves
​ Go Grid Points = (Distance from X-Axis-Body shape in hypersonic flow)/Local Shock-detachment Distance
Mach Wave behind Shock
​ Go Mach Number behind shock = (Freestream Velocity-Local Shock Velocity for Mach Wave)/Speed of Sound
Local Shock Velocity Equation
​ Go Local Shock Velocity = Speed of Sound*(Mach Number-Mach Number ahead of shock)
Mach Wave behind Shock with Mach Infinity
​ Go Mach Number ahead of shock = Mach Number-Local Shock Velocity/Speed of Sound
Nose Radius of Cylinder-Wedge
​ Go Radius = Local Shock-detachment Distance/(0.386*exp(4.67/(Mach Number^2)))
Nose Radius of Sphere Cone
​ Go Radius = Local Shock-detachment Distance/(0.143*exp(3.24/(Mach Number^2)))
Detachment Distance of Cylinder Wedge Body Shape
​ Go Local Shock-detachment Distance = Radius*0.386*exp(4.67/(Mach Number^2))
Detachment Distance of Sphere Cone Body Shape
​ Go Local Shock-detachment Distance = Radius*0.143*exp(3.24/(Mach Number^2))

Local Shock Velocity Equation Formula

Local Shock Velocity = Speed of Sound*(Mach Number-Mach Number ahead of shock)
W = cspeed*(M-M1)

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 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 (cspeed), Mach Number (M) & 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 -> 2229.5 = 343*(8-1.5).

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 = cspeed*(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 & 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 (cspeed), Mach Number (M) & Mach Number ahead of shock (M1). With our tool, you need to enter the respective value for Speed of Sound, Mach Number & 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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