Boundary layer thickness in partial air vacuum

In summary, the boundary layer thickness is unaffected by changes in pressure, as it is primarily dependent on Reynolds number and viscosity. While pressure may indirectly influence the boundary layer through changes in temperature and density, it is not a direct factor in determining its thickness. Furthermore, in low pressures, kinematic viscosity may increase while dynamic viscosity remains constant, potentially leading to changes in density and air velocity. However, these changes are highly dependent on other factors such as temperature, making it difficult to predict their exact effects on the boundary layer.
  • #1
GT1
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How does low ambient pressure effect on the thickness of the boundary layer for given flow conditions of gas?

In absolute vacuum the thickness of the boundary layer is 0 of course, but it seems that all the boundary layer thickness correlations use the Reynolds number, which doesn’t change much vs pressure for given flow conditions (the kinematic viscosity of air is roughly independent of pressure).

How can we explain it?
 
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  • #2
Bird, Stewart, and Lightfoot, Transport Phenomena has a derivation for the viscosity of gases based on molecular considerations. It is in Chapter 1.
 
  • #3
As pressure decreases, the gas flow decreases because it is the result of ΔP. Consequently, Reynolds number decreases and the boundary layer's thickness tends to be zero when pressure tends to be zero.
 
  • #4
DoItForYourself said:
As pressure decreases, the gas flow decreases because it is the result of ΔP. Consequently, Reynolds number decreases and the boundary layer's thickness tends to be zero when pressure tends to be zero.

And if we have an electric car driving at partial vacuum? -the Reynolds number stays the same. and what about the boundary layer thickness?
 
  • #5
In such low pressures (this happens also in higher pressures), kinematic viscosity increases when pressure decreases. Dynamic viscosity does not change significantly but density decreases due to less molecules of air.

I am not sure if the air velocity will be the same in this case, but I think it will decrease.
 
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  • #6
I don't know why you are being advised that a decrease in pressure has any bearing on boundary-layer thickness (##\delta##). The only real dependence ##\delta## has is on ##Re##, which does not depend on pressure. Viscosity also does not depend on pressure; it depends on temperature. Density depends on pressure, but also temperature. So, absent additional constraints, the answer is that ##\delta## does not depend explicitly or directly on pressure.
 
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  • #7
As pressure becomes lower, density becomes lower too (gas flow) and so does Reynolds number ( ##Re = \frac {uDd} {μ} ## ).

So, if all conditions remain constant except pressure, the boundary layer thickness will be influenced.
 
  • #8
However, when you lower pressure, it is unusual for temperature to also be constant such that only density changes. Consider an ideal gas:
[tex]p = \rho R T\to\rho = \dfrac{p}{RT}.[/tex]
Also consider viscosity. Since we are talking gases, it has a relationship to temperature such that
[tex]\mu\propto \sqrt{T}.[/tex]
So,
[tex]Re\propto \dfrac{\rho}{\mu}\propto\dfrac{p}{T^{3/2}}.[/tex]
So if temperature is held constant, then sure, but temperature is rarely constant like that.

The bottom line is that the boundary layer does not directly depend on pressure, and depending on other constraints, notably on temperature, the boundary layer might do a number of things.
 

1. What is a boundary layer thickness?

The boundary layer thickness refers to the distance from a solid surface where the flow of a fluid (such as air) experiences a significant change in velocity due to the influence of the surface. In other words, it is the region near the surface where the effects of viscosity, or the resistance of the fluid to flow, are important.

2. Why is boundary layer thickness important in a partial air vacuum?

In a partial air vacuum, the pressure is lower than that of the surrounding environment. This can significantly affect the behavior of the boundary layer, as the lower pressure can cause the fluid to flow faster and the boundary layer to become thinner. Understanding the boundary layer thickness in a vacuum is important for various applications, such as aerodynamics and heat transfer.

3. How is the boundary layer thickness affected by the presence of a solid surface?

The presence of a solid surface greatly affects the boundary layer thickness. As the fluid flows over the surface, it experiences friction and viscosity, which causes the velocity of the fluid to decrease near the surface. This results in a thicker boundary layer. The type of surface, such as its smoothness or roughness, can also impact the boundary layer thickness.

4. What factors influence the boundary layer thickness?

The boundary layer thickness is influenced by several factors, including the fluid properties (such as viscosity and density), the velocity of the fluid, and the geometry of the surface. Additionally, the type of flow (such as laminar or turbulent) and the presence of external forces, such as gravity or pressure gradients, can also affect the boundary layer thickness.

5. How is the boundary layer thickness measured?

There are various methods for measuring the boundary layer thickness, including direct measurement techniques (such as using a hot-wire anemometer) and indirect methods (such as pressure measurements). The choice of measurement method depends on the specific application and the desired accuracy of the results.

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