Mach Angle Solution

STEP 0: Pre-Calculation Summary
Formula Used
Mach Angle = asin(1/Mach Number)
μ = asin(1/M)
This formula uses 2 Functions, 2 Variables
Functions Used
sin - Sine is a trigonometric function that describes the ratio of the length of the opposite side of a right triangle to the length of the hypotenuse., sin(Angle)
asin - The inverse sine function, is a trigonometric function that takes a ratio of two sides of a right triangle and outputs the angle opposite the side with the given ratio., asin(Number)
Variables Used
Mach Angle - (Measured in Radian) - Mach Angle is defined as the angle between the Mach line and the direction of motion of the body.
Mach Number - Mach Number is a dimensionless quantity representing the ratio of flow velocity past a boundary to the local speed of sound.
STEP 1: Convert Input(s) to Base Unit
Mach Number: 2 --> No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
μ = asin(1/M) --> asin(1/2)
Evaluating ... ...
μ = 0.523598775598299
STEP 3: Convert Result to Output's Unit
0.523598775598299 Radian -->30.0000000000056 Degree (Check conversion ​here)
FINAL ANSWER
30.0000000000056 30 Degree <-- Mach Angle
(Calculation completed in 00.004 seconds)

Credits

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Created by Vinay Mishra
Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune
Vinay Mishra has created this Calculator and 300+ more calculators!
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Verified by Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
Sanjay Krishna has verified this Calculator and 200+ more calculators!

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​ LaTeX ​ Go Specific Gas Constant = Specific Heat Capacity at Constant Pressure-Specific Heat Capacity at Constant Volume
Mach Number
​ LaTeX ​ Go Mach Number = Speed of Object/Speed of Sound
Mach Angle
​ LaTeX ​ Go Mach Angle = asin(1/Mach Number)

Mach Angle Formula

​LaTeX ​Go
Mach Angle = asin(1/Mach Number)
μ = asin(1/M)

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, Mach Angle formula is defined as the angle formed between the direction of a supersonic flow and the direction of the wavefront. It is crucial in understanding shock waves and their behavior in compressible flow scenarios. Mach Angle 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 -> 1718.873 = asin(1/2).

FAQ

What is Mach Angle?
Mach Angle formula is defined as the angle formed between the direction of a supersonic flow and the direction of the wavefront. It is crucial in understanding shock waves and their behavior in compressible flow scenarios 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?
Mach Angle formula is defined as the angle formed between the direction of a supersonic flow and the direction of the wavefront. It is crucial in understanding shock waves and their behavior in compressible flow scenarios 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.
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