How fast does a blastwave travel?

In summary, a blast wave typically travels at supersonic speeds, often exceeding the speed of sound which is approximately 343 meters per second (1,125 feet per second) in air at sea level. The speed can vary depending on the explosive material, the medium through which it travels, and environmental conditions, with some blasts reaching speeds of several kilometers per second. The intensity and effects of a blast wave decrease with distance from the explosion.
  • #211
It is not your prerogative to invalidate the literature of science, by demanding your personal terminology replace that employed for the last century.
 
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  • #212
Squizzie said:
I suggest that the term 'detonation phase' be reserved for the brief, supersonic 'Hugoniot' phase, while 'blast wave' is more appropriately used for the extended sonic 'Friedlander phase' due to these distinctions.
With just a few minutes of googling, I easily find references (with my emphasis added) that directly contradict your "appropriate distinctions".

https://en.wikipedia.org/wiki/Blast_wave:
Blast Wave 1.png

https://apps.dtic.mil/sti/pdfs/AD0608861.pdf:
Blast Wave 2.png

https://onlinelibrary.wiley.com/doi/abs/10.1002/prep.201400042:
Blast Wave 3.png

Can you cite any reference that supports your "distinction", i.e., one that explicitly and unequivocally states that a "blast wave" travels only at the speed of sound (or less)? If not, you're simply espousing a personal theory that contradicts the literature.
 
  • #213
Squizzie said:
I suggest that the term 'detonation phase' be reserved for the brief, supersonic 'Hugoniot' phase, while 'blast wave' is more appropriately used for the extended sonic 'Friedlander phase' due to these distinctions.
I see no reason to do this, especially since the term 'phase' can be and is used to mark the distinctions. The term 'blast wave' appears to be a more general term for how the resulting shock wave and field flow is generated, with the aforementioned phases used to describe the different parts of the blast wave.

Please use the standard terminology in discussing this topic.
 
  • #214
Drakkith said:
I see no reason to do this, especially since the term 'phase' can be and is used to mark the distinctions. The term 'blast wave' appears to be a more general term for how the resulting shock wave and field flow is generated, with the aforementioned phases used to describe the different parts of the blast wave.

Please use the standard terminology in discussing this topic.
While the term 'blast wave' is commonly used to describe the entire phenomenon, it's important to recognize that the blast wave actually consists of two distinct phases, each with its own unique characteristics of propagation speed and pressure profile.
The first phase is characterised by a very high initial propagation speed which decays within milliseconds to the speed of sound, with an abrupt pressure rise, while the second phase exhibits a slower, more gradual decay in pressure and a constant propagation speed.

Unfortunately, a standardised terminology for each of these phases is lacking, introducing challenges into discussions about the speed of a blast wave.
 
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  • #215
Squizzie said:
While the term 'blast wave' is commonly used to describe the entire phenomenon, it's important to recognize that the blast wave actually consists of two distinct phases, each with its own unique characteristics of propagation speed and pressure profile.
The first phase is characterised by a very high initial propagation speed which decays within milliseconds to the speed of sound, with an abrupt pressure rise, while the second phase exhibits a slower, more gradual decay in pressure and a constant propagation speed.
You keep claiming this but you haven't answered my request from post #212. Again I implore you: please support your claim by posting references that explicitly define this "second phase" of a blast wave and explicitly state that the propagation velocity of a blast wave rapidly decays to, and then continues to propagate at, a constant speed of Mach 1. Or is this really just a personal interpretation of what you've read?
 
  • #216
renormalize said:
You keep claiming this but you haven't answered my request from post #212. Again I implore you: please support your claim by posting references that explicitly define this "second phase" of a blast wave and explicitly state that the propagation velocity of a blast wave rapidly decays to, and then continues to propagate at, a constant speed of Mach 1. Or is this really just a personal interpretation of what you've read?
May I direct your attention to my post #206, where I presented a plot featuring data sets from three reputable sources? I have adopted a log scale for both axes in order to accommodate the vast scale range of the two co-ordinates.
In that log/log scale, constant speeds can be represented by parallel lines as indicated by the dotted lines.
The plot illustrates the position of the shock front over time and distance from the detonation. In all three plots, a discernible transition between two phases is evident.
During the initial phase, the shock front speed undergoes a decay from an initial hypersonic speed to a consistent speed of approximately 340 m/s (Mach 1.0 at NTP).
In the second phase, it travels at that constant speed (340 m/s) to the remainder of the data.
 
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  • #217
Squizzie said:
I suggest that the term 'detonation phase' be reserved for the brief, supersonic 'Hugoniot' phase, while 'blast wave' is more appropriately used for the extended sonic 'Friedlander phase' due to these distinctions.
The Rankine–Hugoniot conditions, describe and model the pressure step transition at one point, only as the shock front pressure rises. The blast-wave air-movement that follows the shock front, is not covered by that analysis.

Friedlander models the pressure at one place, near the explosion, over time. It covers the period from the shock front passing that place, right through to the relaxation at the end of the negative phase in that place. Friedlander models the pressure against time, NOT against distance.

After the event, examination of blast damage, does NOT identify the presence of a shock front. The sum of all damage, caused by the pressure changes, or the
blast wave winds, is all undifferentiated blast damage.

The detonation front, or detonation wave, already refers to the progress of the chemical reaction through the explosive material. The atmosphere certainly does NOT detonate, as a shock front passes.

Your choice of terms to be redefined and reallocated, seem inappropriate, and selected to cause maximum possible confusion in the literature. I cannot help thinking that, to consider such a change, you must be equally confused in your understanding.
 
  • #218
Squizzie said:
May I direct your attention to my post #206, where I presented a plot featuring data sets from three reputable sources? I have adopted a log scale for both axes in order to accommodate the vast scale range of the two co-ordinates.
That's a plot you made. I ask for the original references, not filtered through your personal interpretation, that explicitly state that 1) there are two phases of blast waves and 2) the second phase propagates at a constant Mach 1.
 
  • #219
Squizzie said:
Unfortunately, a standardised terminology for each of these phases is lacking, introducing challenges into discussions about the speed of a blast wave.
Look, I don't really care what else you call it, but trying to use 'blast wave' to describe only one part of the process, when it is commonly used to describe the entire thing from creation to dissipation, is only going to generate confusion.

renormalize said:
You keep claiming this but you haven't answered my request from post #212. Again I implore you: please support your claim by posting references that explicitly define this "second phase" of a blast wave and explicitly state that the propagation velocity of a blast wave rapidly decays to, and then continues to propagate at, a constant speed of Mach 1. Or is this really just a personal interpretation of what you've read?
From my reading, the blast wave quickly decays to the speed of sound in the (unheated, uncompressed) medium. You can check the links I posted previously in post #90.

I'd also like to remind people that communication is a two-way street. Describing and explaining phenomena is often difficult, even with the proper terminology readily available, and it is often more beneficial to take the time to try to understand what someone is trying to say versus taking what they typed out at literal value. Also, there is no harm in agreeing on a 'temporary' set of terms to use for a discussion if such a thing is warranted.
 
  • #220
Drakkith said:
From my reading, the blast wave quickly decays to the speed of sound in the (unheated, uncompressed) medium. You can check the links I posted previously in post #90.
I agree, except that, according to the quotes in post #212, a propagating atmospheric disturbance is not called a "blast wave" once it slows to the ambient speed of sound. It's no longer a "blast wave" because it is no longer accompanied by significant pressure excursions, else it wouldn't be in "ambient conditions". The disturbance becomes an ordinary high-amplitude sound wave. That's why I ask @Squizzie to cite some references that uses "blast wave" to label a sonic-speed disturbance in ambient conditions.
 
  • #221
Drakkith said:
Look, I don't really care what else you call it, but trying to use 'blast wave' to describe only one part of the process, when it is commonly used to describe the entire thing from creation to dissipation, is only going to generate confusion.

From my reading, the blast wave quickly decays to the speed of sound in the (unheated, uncompressed) medium. You can check the links I posted previously in post #90.

I'd also like to remind people that communication is a two-way street. Describing and explaining phenomena is often difficult, even with the proper terminology readily available, and it is often more beneficial to take the time to try to understand what someone is trying to say versus taking what they typed out at literal value. Also, there is no harm in agreeing on a 'temporary' set of terms to use for a discussion if such a thing is warranted.
Yes, you are correct, but in the absence of any other terminology, my approach has been to restrict my use of "blast wave" it to the much longer phase once it has decayed to the speed of sound. It is that phase that Kinney & Graham discuss in Ch 6. "Blast Waves".
After all this is the phase that lasts for many seconds whereas the earlier phase (which I have clumsily identified as the "detonation phase") only lasts milliseconds (but does most of the damage) .
I would welcome the opportunity to discuss alternate temporary set of terms.
 
  • #222
renormalize said:
I agree, except that, according to the quotes in post #212, a propagating atmospheric disturbance is not called a "blast wave" once it slows to the ambient speed of sound. It's no longer a "blast wave" because it is no longer accompanied by significant pressure excursions, else it wouldn't be in "ambient conditions". The disturbance becomes an ordinary high-amplitude sound wave. That's why I ask @Squizzie to cite some references that uses "blast wave" to label a sonic-speed disturbance in ambient conditions.
The blast wave appears to undergo an exponential decay towards the speed of sound, and I'm wondering if the shock front is sustained for a significant amount of time very close to the speed of sound before finally transitioning to a regular sound wave. I have yet to see anything in any of the sources I've read in this thread seen anything about when/where/how this transition occurs. That leads me to believe that the blast wave remains a blast wave for a pretty long time/distance and the transition to a sound wave is not particularly important. But that's a guess on my part.

Squizzie said:
Yes, you are correct, but in the absence of any other terminology, my approach has been to restrict my use of "blast wave" it to the much longer phase once it has decayed to the speed of sound. It is that phase that Kinney & Graham discuss in Ch 6. "Blast Waves".
I have yet to see anything that made any effort to use 'blast wave' differently in the two phases, so I would highly recommend not doing that. If you really need to label the two phases, perhaps 'early' and 'late' phases would be do, or "supersonic' and 'near-sonic', or something similar.
 
  • #223
Drakkith said:
The blast wave appears to undergo an exponential decay towards the speed of sound, and I'm wondering if the shock front is sustained for a significant amount of time very close to the speed of sound before finally transitioning to a regular sound wave.
The shock front decays exponentially as it heats air, at the same time as it is attenuated by the inverse square law.

Gilbert F. Kinney and Kenneth J. Graham - Explosive Shocks in Air. 2'nd Edn. 1985.
Table XI, page 254, shows one kilogram of TNT as being supersonic to beyond 500 metres. From 100 m to 500 m, the velocity falls by only 0.2%.

Drakkith said:
I have yet to see anything in any of the sources I've read in this thread seen anything about when/where/how this transition occurs.
There is no clear point where the transition occurs. The two velocity modes are feathered together. I would expect reflections to make the transition quite patchy near the ground.
 
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  • #224
Baluncore said:
Gilbert F. Kinney and Kenneth J. Graham - Explosive Shocks in Air. 2'nd Edn. 1985.
Table XI, page 254, shows one kilogram of TNT as being supersonic to beyond 500 metres. From 100 m to 500 m, the velocity falls by only 0.2%.
By computing the speed between each pair of data points using Vi = (Zi - Zi-1) / (ti- ti-1) with the provided data, you will observe a consistent interval speed of 340 m/s from 70 metres to 500 metres.
1700950766192.png
Could you please provide more details about the meaning and implications of the "only 0.2%?"
 
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  • #225
Squizzie said:
By computing the speed between each pair of data points using Vi = (Zi - Zi-1) / (ti- ti-1) with the provided data, you will observe a consistent interval speed of 340 m/s from 70 metres to 500 metres.
I do not understand why you are differentiating the data when the Mach number is given.

I've plotted the 1 kg HE data from Kinney. I plotted the full range of the Mach Number and a limited range of the Mach Number as a function of distance.
Graph3.jpg

Please identify where you would start your "blast regime” given that the propagation speed is asymptoting to the sound speed.

Fun fact, the pressure of the last point is about 140 dB.
 
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  • #226
Squizzie said:
Could you please provide more details about the meaning and implications of the "only 0.2%" ?
They give the accurate velocity as a Mack number in the Mx column.
Z = 100 m; Mx = 1.003
Z = 500 m; Mx = 1.001
The difference is only 0.2%, but it is still supersonic at 500 m.

You are seeing numerical round-off noise from the tabulated data in your unnecessary re-computation. That explains why your graph jumps up and down about the speed of sound, while the shock front remains supersonic throughout.
 
  • #227
Baluncore said:
They give the accurate velocity as a Mack number in the Mx column.
Z = 100 m; Mx = 1.003
Z = 500 m; Mx = 1.001
The difference is only 0.2%, but it is still supersonic at 500 m.

You are seeing numerical round-off noise from the tabulated data in your unnecessary re-computation. That explains why your graph jumps up and down about the speed of sound, while the shock front remains supersonic throughout.
But the difference between Mach 1.003 (at Z=100 m) and Mach 1 ( ~340 m/sec) is 1.02 metres per second. A few degrees of temperature or hectopascals of atmospheric pressure could easily account for those differences in the data.
I'm not convinced that this evidence is sufficient to support the conclusion that the shock front was moving at anything other than Mach 1.
 
  • #228
Squizzie said:
I'm not convinced that this evidence is sufficient to support the conclusion that the shock front was moving at anything other than Mach 1.
Then you will be unable to work as a scientist in this field.
The data says it is doing Mx = 1.001, not Mx = 1.000
How can it be a shock front if it is not moving faster than Mach 1.
 
  • #229
Squizzie said:
But the difference between Mach 1.003 (at Z=100 m) and Mach 1 ( ~340 m/sec) is 1.02 metres per second. A few degrees of temperature or hectopascals of atmospheric pressure could easily account for those differences in the data.
I'm not convinced that this evidence is sufficient to support the conclusion that the shock front was moving at anything other than Mach 1.
Well, there is also the theory, and I would also say that my plot of the data supports the conclusion.
 
  • #230
Baluncore said:
How can it be a shock front if it is not moving faster than Mach 1.
I think we are both correctly interpreting the data in table XI as it relates to the progress of the shock front as explained on p. 96 of Chapter 6 "Blast Waves":
" the peak overpressure values of Table XI also uniquely define the time required for that shock front to travel out to various distances. "
And I have previously identified p. 88 of the same chapter:
"Each individual portion of this pulse moves outward at its own speed, which also is the speed of sound in its own immediate medium. "
So I'm not convinced that your evidence is sufficient to support your contrary conclusion that the shock front was propagating at anything other than steadily at Mach 1 by 100 metres and 280 ms.
 
  • #231
Squizzie said:
I think we are both correctly interpreting the data in table XI as it relates to the progress of the shock front as explained on p. 96 of Chapter 6 "Blast Waves":
" the peak overpressure values of Table XI also uniquely define the time required for that shock front to travel out to various distances. "
And I have previously identified p. 88 of the same chapter:
"Each individual portion of this pulse moves outward at its own speed, which also is the speed of sound in its own immediate medium. "
So I'm not convinced that your evidence is sufficient to support your contrary conclusion that the shock front was propagating at anything other than steadily at Mach 1 by 100 metres and 280 ms.
No. You are proposing the nonstandard interpretation. The responsibility is on your end.
 
  • #232
Frabjous said:
No. You are proposing the nonstandard interpretation. The responsibility is on your end.
Is not Kinney and Graham, from whom I'm drawing my reference, the standard text?
 
  • #233
Squizzie said:
Is not Kinney and Graham, from whom I'm drawing my reference, the standard text?
Yes, and you are saying that the data they present is wrong. You did not know about it when you started this thread, and now you believe that you can correct it.
 
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  • #234
Squizzie said:
So I'm not convinced that your evidence is sufficient to support your contrary conclusion that the shock front was propagating at anything other than steadily at Mach 1 by 100 metres and 280 ms.
But a shock front is a pressure step that heats the air. It propagates faster in the heated air, so it maintains the step. The shock front must be propagating marginally above Mach 1, to remain as a step.

All things are relative. Small variations in local air pressure or temperature, do not influence the differential step height of the pressure or temperature shock.

You would find the distinct 'crack' of any shock front to be an uncomfortable noise, no matter how small it was.

You cannot round; Mx > 1, down to; Mx = 1, while the shock front remains a step, which the data shows it does, to beyond 500 metres.

By definition, NO shock front ever propagates at Mach 1.
 
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  • #235
Frabjous said:
Yes, and you are saying that the data they present is wrong.
If you are suggesting that I am contradicting the data in Table XI, I should point out that the"δ(m/s)" and "Mx" values reported in Table XI represent the average speed (Z(m)/ ta), not the interval speed.

I attach a screenshot of my working, highlighting the detail that the δ(m/s) values in the table are in fact the average values that can be deduced from the data, not the interval values.
1700968307792.png
Since the speed is decreasing from an initially very high value, the average speed values will approach asymptotically to Mach 1, obscuring the fact that, as my post #224 above clearly shows, the interval, or instantaneous speed of Mach 1 is achieved after about 50 metres from the blast.
 
  • #236
@Squizzie
Way back, about 200 posts ago, in post #24, you believed that you had estimated a shock front velocity to be about Mach 1. What you had actually estimated, was the phase velocity of the condensation cloud formation, in the inertially pulled depression that followed the explosion. At the time, that was one of the several things you did not know existed.

If you do not know what you are doing, you must be prepared to learn. There are early false beliefs, that you must dispel. One of those is your belief that a shock front propagates at Mach 1, which actually contradicts the definition of a shock wave. Maybe you would get a better perspective if you first studied the Dunning-Kruger effect.

Rather than study, accept, and work in the field, you deny and contradict the science, then like an authoritarian barbarian, a dictator, you persistently try to crush the science.
 
  • #237
I think that's it for this thread.
@Squizzie Without any clear statement to the contrary from the references on the topic, I'm inclined to believe that the blast wave continues to travel just above the speed of sound until the energy dissipates. Even if only barely above the speed of sound.

If anyone finds a reference that clearly states otherwise, please feel free to PM myself or another mentor and we can discuss reopening the thread. Until then, thread locked.
 
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