For turbulent flow in circular pipes, which statement about Prandtl’s mixing length is correct with respect to its variation near the wall and across the radius?

Difficulty: Easy

Correct Answer: zero at the pipe wall

Explanation:


Introduction / Context:
Prandtl’s mixing length hypothesis models turbulent momentum exchange by analogy with molecular diffusion, introducing a characteristic length scale l that represents the average distance over which eddies transport momentum before losing identity. Understanding how l varies in wall-bounded flows like pipes is essential for velocity profile modeling and shear stress estimation.


Given Data / Assumptions:

  • Flow: steady, fully developed turbulent flow in a smooth circular pipe.
  • We consider the qualitative behavior of mixing length l across the radius.
  • Wall effects dominate near the boundary; core flow differs.


Concept / Approach:

In wall-bounded turbulence, mixing length increases with distance from the wall: l ≈ κ * y in the log-law region, where y is the wall-normal distance and κ is the von Kármán constant (~0.4). At the wall itself, fluctuations are suppressed and l → 0. Therefore, l is not a universal constant and certainly not independent of radius. While shear stress informs velocity gradients, the canonical variation of l is tied to position, not fixed by a single shear value.


Step-by-Step Solution:

Recognize boundary-layer behavior → l grows with y away from the wall.At y = 0 (the pipe wall), l must vanish due to the no-slip boundary condition.Conclude the correct qualitative statement: l is zero at the pipe wall.


Verification / Alternative check:

Empirical velocity profiles (log-law) and eddy viscosity models (νt = l^2 |du/dy|) both require l = 0 at the wall to avoid non-physical finite turbulent shear right at the boundary.


Why Other Options Are Wrong:

  • Universal constant/independent of radius: Contradicts position dependence (l ∝ y in near-wall region).
  • Independent of shear stress: Eddy viscosity depends on gradients; l is coupled to flow structure.
  • Maximum at wall: Opposite of physical reality; turbulence production is suppressed at the wall.


Common Pitfalls:

  • Assuming l is constant across the section; that leads to unrealistic profiles.
  • Ignoring viscous sublayer where turbulence is damped and l remains small.


Final Answer:

zero at the pipe wall

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