Ax_xiom
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Alright, thanks!Frabjous said:Give me a day or two.
Alright, thanks!Frabjous said:Give me a day or two.
Frabjous said:Kinney and Graham "Explosive Shocks in Air" 1985
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Do you mean compare overpressure to the mach number of the shockwave?Frabjous said:What does the mach number comparison look like?
Isn't that what I did when I got the result I'm currently testing? I took the result for ##\frac{dz}{dt}## and changed it to an expression of the mach number, then used that expression to calculate the pressure (and overpressure)Frabjous said:Try to follow the analysis in the paper.
It starts with z vs t
Then comes mach number.
Then comes pressure.
You want to see where the disagreement starts. Then you try to figure out the discrepancy there.Ax_xiom said:Isn't that what I did when I got the result I'm currently testing? I took the result for ##\frac{dz}{dt}## and changed it to an expression of the mach number, then used that expression to calculate the pressure (and overpressure)
So plot overpressure against mach number?Frabjous said:You want to see where the disagreement starts. Then you try to figure out the discrepancy there.
I mean, the definition of a blast wave requires it to be supersonic. It will eventually weaken into an acoustic wave. So that was pretty silly by said poster.renormalize said:Thanks for citing the Diaz & Rigby paper. We had a poster some time back who vehemently insisted that a blast-wave shock-front could propagate at the speed-of-sound ##c## and cited data from the 2020 Beirut chemical explosion to back his claim. But the analysis in this paper clearly demonstrates that the Beirut shock front traveled supersonically and only approached ##c## ("acoustic wave") as ##t\rightarrow\infty##:
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