Speed of a sound wave (compressibe flow)

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Discussion Overview

The discussion revolves around the speed of sound waves in compressible flow, particularly how the flow velocity affects the perceived speed of sound. Participants explore concepts related to sound propagation in moving media and the implications of Mach number on sound wave behavior.

Discussion Character

  • Exploratory
  • Technical explanation
  • Conceptual clarification
  • Debate/contested

Main Points Raised

  • One participant questions whether the resultant velocity of a sound wave in a flow is 'c + U' when traveling in the same direction as the flow and 'c - U' when traveling against it, and seeks clarification on the propagation speed of sound waves relative to the flow velocity.
  • Another participant asserts that all motion is relative, prompting a broader consideration of how sound behaves in different frames of reference.
  • A participant explains that a sonic boom is experienced by an observer when a sound source, such as a jet, moves at Mach 1, while the medium through which the sound travels is not moving at that speed.
  • Responses confirm the initial participant's understanding of sound wave propagation speeds and clarify that at Mach 1, the speed of sound is not zero, but rather zero relative to the sound source, which leads to the stacking of sound waves.
  • Another participant emphasizes that sound travels at speed 'c' relative to the air, and that this must be considered when evaluating wave speed from a stationary observer's perspective.

Areas of Agreement / Disagreement

Participants generally agree on the relative nature of sound speed and the implications of Mach number, but there are nuances in understanding how these concepts apply in different contexts, particularly regarding the speed of sound relative to moving sources and observers.

Contextual Notes

There are unresolved aspects regarding the definitions of speed in different frames of reference and the implications of relative motion on sound propagation, which may depend on specific conditions or assumptions not fully articulated in the discussion.

Who May Find This Useful

This discussion may be useful for students and professionals interested in fluid dynamics, acoustics, and the behavior of sound in moving media, particularly in contexts involving compressible flow and Mach number considerations.

xJJx
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Hi, there is no particular question that I need help on, just something my lecturer told us in lesson which I couldn't quite understand so i'd like to check my understanding on this. I know that the speed of a soundwave is 'c' in undisturbed flow. Suppose the flow velocity is 'U'. If the soundwave is convected by the flow, would the resultant velocity of the soundwave be 'c + U' if the wave is traveling in the same direction as flow, and would it be 'c - U' (vector sum) if the wave is traveling in the opposite direction to the flow? Does the centre of the sound wave travel at a speed of U whilst the ripples propagate at speed c?
Also, my teacher said that at Mach 1, the speed of the sound wave is exactly 0, which is why the soundwaves stop and compile to form a shockwave. I don't understand how the speed can be 0 when U=c at mach 1.
thank you!
 
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All motion is relative. The Earth is moving through space as you speak. How do you handle that. When you talk on an airplane, how do you handle that?
 
The "Sonic boom" is experienced by an outside observer. The source of the sound (a jet plane, for example) is moving at Mach 1. The medium (air) through which the sound travels is not moving at Mach 1
 
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xJJx said:
would the resultant velocity of the soundwave be 'c + U' if the wave is traveling in the same direction as flow, and would it be 'c - U' (vector sum) if the wave is traveling in the opposite direction to the flow?
Yes.
xJJx said:
Does the centre of the sound wave travel at a speed of U whilst the ripples propagate at speed c?
Yes.
xJJx said:
Also, my teacher said that at Mach 1, the speed of the sound wave is exactly 0, which is why the soundwaves stop and compile to form a shockwave. I don't understand how the speed can be 0 when U=c at mach 1.
The speed is not zero. It is zero relative to the sound source since they travel at the same velocity (only considering the moving direction of the sound source). So, as soon as the sounds source emits a sound wave, it "follows" it since they travel at the same velocity. When the sound source emits another sound wave, it therefore "stacks" on the previous sound wave.

speed%2Bof%2Bsound.jpg
 

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The bottom line is you just have to remember that sound travels at the speed of sound ##c## (sometimes written as ##a## as well) relative to the air, so if the air is moving, you have to take that into account if you are looking at the wave speed relative to a stationary observer.
 
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jack action said:
Yes.

Yes.

The speed is not zero. It is zero relative to the sound source since they travel at the same velocity (only considering the moving direction of the sound source). So, as soon as the sounds source emits a sound wave, it "follows" it since they travel at the same velocity. When the sound source emits another sound wave, it therefore "stacks" on the previous sound wave.

Thank you so much! this was very helpful. It creeps up a lot in exam questions so it's worth knowing
 
boneh3ad said:
The bottom line is you just have to remember that sound travels at the speed of sound ##c## (sometimes written as ##a## as well) relative to the air, so if the air is moving, you have to take that into account if you are looking at the wave speed relative to a stationary observer.
thank you!
 

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