What Are Shock Cones and How Do They Relate to Mach Numbers?

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A shock cone is formed when a sound source travels faster than the speed of sound, creating a cone of sound wave-fronts that angles back from the source. Mach numbers, such as Mach II or Mach III, indicate the speed of an object relative to the speed of sound, with Mach II being twice that speed. To solve problems involving shock cones, understanding the relationship between the speed of the source and the speed of sound is crucial. The cone angle can be determined by analyzing the motion of both the sound waves and the source. Clarifying these concepts will aid in tackling related problems effectively.
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My teacher gave us a worksheet to prepare for the test tomorrow, and we never discussed anything about problems 10 to 14. I'm not asking for answers . . . just clarifications.

1.) What is a shock cone, anyway?
2.) What does Mach II, Mach III, etc. mean?
3.) Are there certain equations that I have to use when solving problems about shock cones?

I would really like to not post the questions on here, because I want to figure them out myself. Just answer my above questions for me as best as you can, and I'm hoping that will help me figure these out. Thanks!
 
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If you don't have a textbook ...
When a sound source travels faster than the sound,
the forward motion of the sound can't keep up.
The sideways moving sound that was made "t" ago has traveled
y = v_sound t , while the source has moved forward x = v_source t .
There's a cone of sound wave-front that angles back from the source
to the y-coordinate above.
Can you draw this? Can you fingure what the tangent of the cone angle is?
(The cone angle is measured from the path that the source has taken)
 
Mach (X) means that the velocity of that particle is X times the speed of sound.

So mach II would be twice the speed of sound.
 
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