Resolving the Low Reynolds Number Paradox: Wake Formation

In summary, at low Reynolds numbers, the flow may or may not have a wake depending on the presence of a viscous flow. This can be seen in the example of a convex surface, where a boundary layer may be laminar at low Reynolds numbers and cause separation, but can be made thinner by triggering turbulent flow with turbulator strips, reducing overall drag. This is particularly important for gliders, where energy conservation is crucial.
  • #1
Cosmossos
100
0
The wake is made because the inertia forces in the system ,right? So if i have low Reynolds number the inertia forces are negligible and the flow doesn't separate ,right?
So In every low Reynolds number the flow doesn't separate (no wake) but low Reynolds number also indicate a viscous flow which in it there is a wake.
So we get that for low Reynolds numbers we can get a wake or not which it isn't possible.

please help me resolve this paradox.
 
Physics news on Phys.org
  • #2
A turbulent wake from a convex surface occurs because of viscosity and inertia issues. If there was very little viscosity, you'd have a huge near stagnant "boundary layer" to fill in what would otherwise be a void if the fluid doesn't follow a convex surface because of inertia issues.

In the real world, on a convex surface, there's a boundary layer that gets effectively thicker and separates with distance from leading edge of the surface. That boundary layer may be nearly laminar at low Reynolds numbers. Although the flow is laminar, the effective boundary layer separates and ends up thicker that it would if it was turbulent, so some low Reynolds number air foils deliberatly trip up the boundary later to trigger turbulent flow, which costs energy at the trigger point, but reduces the effective profile drag by making the effective boundary later thinner. This is mostly an issue for gliders, which rough up the surface of a wing or use turbulator strips.

Although the wiki article diagram shows the turbulent portion of the boundary layer to be thicker, the over thickness would be smaller if the transition to a turbulent boundary layer occurred sooner (reducing separation which isn't shown, since the diagram is of a flat surface):

http://en.wikipedia.org/wiki/Boundary_layer

As mentioned some gliders either rough up the surface of a wing or use turbulator strips:

http://en.wikipedia.org/wiki/Turbulator
 
Last edited:

FAQ: Resolving the Low Reynolds Number Paradox: Wake Formation

1. What is the Low Reynolds Number Paradox?

The Low Reynolds Number Paradox is a phenomenon in fluid mechanics where the flow of a fluid around a solid object at low Reynolds numbers (less than 100) results in a symmetric flow pattern, despite the presence of asymmetry in the object's shape. This contradicts the expectation that the flow should be asymmetric due to the shape of the object.

2. Why is it important to resolve the Low Reynolds Number Paradox?

The Low Reynolds Number Paradox has significant implications in various fields, such as aerodynamics, biofluid dynamics, and microfluidics. Understanding and resolving this paradox can help in designing more efficient and accurate models for predicting fluid flow behavior, which is crucial in many engineering and scientific applications.

3. What is the role of wake formation in the Low Reynolds Number Paradox?

Wake formation is the formation of a region of disturbed flow behind a solid object in a fluid. In the context of the Low Reynolds Number Paradox, wake formation plays a crucial role in understanding why the flow remains symmetric despite the asymmetry of the object. Resolving the paradox involves understanding the mechanisms behind wake formation and its effects on the flow behavior.

4. How have scientists attempted to resolve the Low Reynolds Number Paradox?

Scientists have used various approaches, such as experimental studies, theoretical analyses, and computational simulations, to resolve the Low Reynolds Number Paradox. These methods have helped in identifying and understanding the various factors that contribute to the paradox, such as boundary layer separation, viscous effects, and vortex shedding.

5. What are some potential applications of resolving the Low Reynolds Number Paradox?

Resolving the Low Reynolds Number Paradox can have significant practical applications, such as improving the design of microfluidic devices, enhancing the performance of small-scale aerial vehicles, and optimizing the efficiency of marine propulsion systems. It can also lead to a better understanding of biological fluid dynamics, which can have implications in fields such as medicine and biology.

Similar threads

Back
Top