Looking for Equation that can describe both scenarios

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SUMMARY

The discussion centers on the search for a common equation that describes both rocket exhaust shock waves and traffic jam patterns. It highlights that both phenomena exhibit oscillating patterns, despite their differing contexts—supersonic flow versus vehicular movement. A reference is made to the article "On the Propagation of Shock Waves in Regions of Non-Uniform Density" by C. W. Jones, published in the Proceedings of the Royal Society of London, which may provide insights into the governing equations relevant to these scenarios. The inquiry emphasizes the challenge of finding a unifying equation for these seemingly unrelated phenomena.

PREREQUISITES
  • Understanding of fluid dynamics, particularly shock wave theory.
  • Familiarity with traffic flow theory and its mathematical modeling.
  • Knowledge of oscillatory behavior in physical systems.
  • Access to academic resources, such as JSTOR, for research articles.
NEXT STEPS
  • Research the governing equations of shock waves in fluid dynamics.
  • Explore traffic flow models, specifically those addressing non-uniform flows.
  • Study the mathematical principles behind oscillatory patterns in physics.
  • Read the article "On the Propagation of Shock Waves in Regions of Non-Uniform Density" by C. W. Jones for detailed insights.
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Researchers in fluid dynamics, traffic engineers, physicists studying wave phenomena, and anyone interested in the mathematical modeling of complex systems.

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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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