Mach Wave behind Shock with Mach Infinity Calculator

✖Mach number is a dimensionless quantity representing the ratio of flow velocity past a boundary to the local speed of sound.ⓘ Mach Number [M]			+10% -10%
✖Local shock velocity is defined as the shock velocity after the shock wave.ⓘ Local Shock Velocity [W]			+10% -10%
✖The Speed of Sound is defined as the dynamic propagation of sound waves.ⓘ Speed of Sound [c_s]			+10% -10%

✖Mach Number ahead of Shock is the Mach number over the body before a shockwave has occurred.ⓘ Mach Wave behind Shock with Mach Infinity [M₁]

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Mach Wave behind Shock with Mach Infinity Solution

STEP 0: Pre-Calculation Summary

Formula Used

Mach Number ahead of Shock = Mach Number-Local Shock Velocity/Speed of Sound
M₁ = M-W/c_s
This formula uses 4 Variables

Variables Used

Mach Number ahead of Shock - Mach Number ahead of Shock is the Mach number over the body before a shockwave has occurred.
Mach Number - Mach number is a dimensionless quantity representing the ratio of flow velocity past a boundary to the local speed of sound.
Local Shock Velocity - (Measured in Meter per Second) - Local shock velocity is defined as 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.

STEP 1: Convert Input(s) to Base Unit

Mach Number: 8 --> No Conversion Required
Local Shock Velocity: 2229.5 Meter per Second --> 2229.5 Meter per Second No Conversion Required
Speed of Sound: 343 Meter per Second --> 343 Meter per Second No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

M₁ = M-W/c_s --> 8-2229.5/343

Evaluating ... ...

M₁ = 1.5

STEP 3: Convert Result to Output's Unit

1.5 --> No Conversion Required

FINAL ANSWER

1.5 <-- Mach Number ahead of Shock

(Calculation completed in 00.004 seconds)

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Created by Sanjay Krishna

Amrita School of Engineering (ASE), Vallikavu

Sanjay Krishna has created this Calculator and 300+ more calculators!

Verified by Shikha Maurya

Indian Institute of Technology (IIT), Bombay

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< Shock Dynamics and Aerodynamic Shape Calculators

Grid Point Calculation for Shock Waves

LaTeX Go Grid Points = (Distance from X-Axis-Body Shape in Hypersonic Flow)/Local Shock-Detachment Distance

Mach Wave behind Shock

LaTeX Go Mach Number behind Shock = (Freestream Velocity-Local Shock Velocity for Mach Wave)/Speed of Sound

Local Shock Velocity Equation

LaTeX Go Local Shock Velocity = Speed of Sound*(Mach Number-Mach Number ahead of Shock)

Mach Wave behind Shock with Mach Infinity

LaTeX Go Mach Number ahead of Shock = Mach Number-Local Shock Velocity/Speed of Sound

Mach Wave behind Shock with Mach Infinity Formula

LaTeX Go

Mach Number ahead of Shock = Mach Number-Local Shock Velocity/Speed of Sound
M₁ = M-W/c_s

what is 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 Shock with Mach Infinity?

Mach Wave behind 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 Shock with Mach Infinity formula is defined as a measure of the shock wave that forms behind an object moving at hypersonic speeds, typically in excess of Mach 5, in an inviscid flow, where the shock wave's properties are affected by the object's speed and the surrounding fluid's properties. Mach Number ahead of Shock is denoted by M₁ symbol.

How to calculate Mach Wave behind Shock with Mach Infinity using this online calculator? To use this online calculator for Mach Wave behind Shock with Mach Infinity, enter Mach Number (M), Local Shock Velocity (W) & Speed of Sound (c_s) and hit the calculate button. Here is how the Mach Wave behind Shock with Mach Infinity calculation can be explained with given input values -> 5.137026 = 8-2229.5/343.

FAQ

What is Mach Wave behind Shock with Mach Infinity?

The Mach Wave behind Shock with Mach Infinity formula is defined as a measure of the shock wave that forms behind an object moving at hypersonic speeds, typically in excess of Mach 5, in an inviscid flow, where the shock wave's properties are affected by the object's speed and the surrounding fluid's properties and is represented as M₁ = M-W/c_s 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 defined as the shock velocity after the shock wave & The Speed of Sound is defined as the dynamic propagation of sound waves.

How to calculate Mach Wave behind Shock with Mach Infinity?

The Mach Wave behind Shock with Mach Infinity formula is defined as a measure of the shock wave that forms behind an object moving at hypersonic speeds, typically in excess of Mach 5, in an inviscid flow, where the shock wave's properties are affected by the object's speed and the surrounding fluid's properties is calculated using Mach Number ahead of Shock = Mach Number-Local Shock Velocity/Speed of Sound. To calculate Mach Wave behind Shock with Mach Infinity, you need Mach Number (M), Local Shock Velocity (W) & Speed of Sound (c_s). With our tool, you need to enter the respective value for Mach Number, Local Shock Velocity & 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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