What is the difference between Mach cone and shock wave in aerodynamics?

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SUMMARY

The discussion clarifies the distinction between a Mach cone and a shock wave in aerodynamics. The Mach cone represents the area where sound waves converge, while the shock wave is the result of an object traveling faster than the speed of sound, creating a distinct boundary. The confusion arises from the visual representation of these phenomena, as some authors incorrectly equate the Mach cone with the shock wave. The analogy of a bow wave from a boat is used to illustrate how shock waves propagate similarly to sound waves.

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TimeRip496
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Is mach cone the area of the shock wave or the wave front of the Mach wave?
Usually the diagram for mach cone is this,
upload_2018-1-8_16-28-27.png


However I still see some author states that the Mach cone is the shock wave. Shouldn't the shock wave be at the intersection(between the circles) and if the Mach cone is about the shock wave, shouldn't the diagram be like this instead?
upload_2018-1-8_16-33-35.png
 

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TimeRip496 said:
However I still see some author states that the Mach cone is the shock wave. Shouldn't the shock wave be at the intersection(between the circles)
Imagine there are not just 3, but many more circles (the sound is generated continuously). Where would their intersection lie?
 
Try drawing a thousand circles in your cone. Where is the intersection now? Unless of course, sound is only generated a three intervals:wink:.
 
Take a look at the bow wave on a boat. It extends out in a v shape just like the shock wave of an aircraft. The resulting wave eventually reaches the bank where it appears to move along the water's edge in much the same way that a shock wave passes over the ground.

The circles on the drawings of a shock wave don't really exist because the process is continuous.
 

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