Validity of Navier-Stokes at Extreme Mach Nos. (M = 100,000)

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Discussion Overview

The discussion centers on the validity of the Navier-Stokes equations at extreme Mach numbers, specifically at Mach 100,000, and the implications for fluid dynamics in such conditions. Participants explore theoretical limits, potential corrections to the equations, and alternative modeling approaches for high-velocity flows.

Discussion Character

  • Exploratory
  • Technical explanation
  • Debate/contested

Main Points Raised

  • One participant questions at what point the Navier-Stokes equations lose validity when applied to extreme Mach numbers and suggests the need for corrections to the equations.
  • Another participant provides a reference to a paper discussing the limitations and extensions of the Navier-Stokes equations.
  • A different participant emphasizes the need to consider small-scale phenomena at high velocities, suggesting there is a limit to the applicability of continuum flow mechanics.
  • One participant explains that at very high supersonic speeds, continuum flow mechanics break down, transitioning to free molecular flow, particularly during atmospheric re-entry of space vehicles.
  • Another participant introduces the concept of relativistic fluid dynamics and mentions the Boltzmann equation as a necessary tool for high Knudsen numbers, indicating it may generalize the Navier-Stokes equations.

Areas of Agreement / Disagreement

Participants express differing views on the applicability of the Navier-Stokes equations at extreme velocities, with some suggesting corrections may be needed while others highlight the transition to free molecular flow. The discussion remains unresolved regarding the exact limits and conditions under which the Navier-Stokes equations may fail.

Contextual Notes

Participants mention various factors such as temperature and pressure changes across shock boundaries and the implications of relativistic effects, indicating that assumptions about flow conditions and scales are critical to the discussion.

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So, speaking theoretically, if you could accelerate a fluid to extreme Mach number at sea level, then at what point does the Navier Stokes number lose its validity? What equations would you then use to model this potentially extreme momentum?

I presume based on the fact that Newton's Law's are an approximation to the classical world that only really fail at extreme velocities approaching the speed of light, how close to those velocities do we need to be before we need to worry about the validity of the equations and can we apply corrections to N-S to correct for this?

Finally, is it theoretically possible to collect a group of neutrino's for instance, compact them so that they can regarded as a continuum (very low Knudsen number) and therefore model this from using what we've just discussed?
 
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That is more to do with small scale phenomena. I was looking more specifically at extreme velocity. But you are correct in thinking that inevitably at higher velocities, smaller scales must be found. There must surely be a limit to this though.
 
Navier–Stokes equations balance momentum in the flow, and are utilized in the "continuum flow" regime. At very high supersonic speeds for high altitudes continuum flow mechanics start to break down and are replaced by "free molecular" flow due to reduced collisions between gas molecules. I'm by no means an expert in this area, but I know a practical example of free molecular flow is the a space vehicle re-entering the atmosphere.

My feeling is at very high hypersonic speeds and low altitudes continuum flow equations will start to break down due to the temperature and pressure delta across the shock boundary (if that boundary is hot enough to "induce" free molecular flow-like conditions in the shock's wake). It might be Navier-Stokes works if utilized in concert with some "creative" boundary conditions, but when you're talking M > 100,000 it's anyone's guess as to what's going on there... The speed you're describing is over 1/10 the speed of light, my guess is travel through an atmosphere at that speed would be like setting off a nuclear bomb in front of the vehicle.
 
Here is a nice introduction to relativistic fluid dynamics. Practical applications are I think mainly in the area of plasma physics:

http://mathreview.uwaterloo.ca/archive/voli/2/olsthoorn.pdf

For high Knudsen numbers, you need to solve the Boltzmann equation, I think you can derive the Navier-Stokes equations from it, so you can see it as a generalization of the N-S equations.
 

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