Looking for Equation that can describe both scenarios

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The discussion explores the possibility of a single equation describing both rocket exhaust shock waves and traffic jams, highlighting their shared oscillating patterns. It emphasizes the complexity of relating supersonic flow phenomena to traffic dynamics, despite their apparent differences. A reference is made to an article by C. W. Jones that connects shock wave behavior in non-uniform flows to traffic patterns. The inquiry seeks guidance on relevant topics or equations that could bridge these two scenarios. The conversation reflects skepticism about the feasibility of a unified equation for such distinct phenomena.
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Scenario 1: Rocket Exhaust Shock Waves
A wave pattern forms on an exhaust plume. The wave is reflected back and forth between the fluid jet boundary, forming oblique shocks which resemble diamonds.

Scenario 2: Traffic Jams on an open highway
While driving on the interstate traffic comes to a halt or a slow down, then it picks up again, then slows back down. Forming a pattern. ----- - - ----- - - ----- - - (something like that, I would imagine).

I was told these two patterns can be found using the same equation or explained using the same equation (not necessarily found). And I cannot for the life of me locate what equation these could be.

Any help on what topic to look under or the equation itself would be nice.
 
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It seems quite ridiculous that a single equation would be capable of properly describing those two completely different phenomenea. One is supersonic flow, the other is traffic patterns; the only shared relationship between the two is they have some form of oscillating pattern.
 
Yes is does seem ridiculous. A colleague of mine said that they read it in a science magazine on an airplane and cannot recall which magazine or the basis of the comparison. I have tried to find any similarities possible, maybe some sort of fluids equation?
 
You may find the following article of interest. If you don't have a subscription that covers it, please let me know.

Ultimately it attempts to relate the governing equations for the behaviour of shocks when meeting a shear layer (such as at wing tips) to the travel of shock waves in traffic in non uniform flows.

On the Propagation of Shock Waves in Regions of Non-Uniform Density
C. W. Jones

Proceedings of the Royal Society of London. Series A, Mathematical and Physical Sciences, Vol. 228, No. 1172 (Feb. 15, 1955), pp. 82-99

http://www.jstor.org/stable/99477
 
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