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?
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Aindependent of shear stress
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Ba universal constant
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Czero at the pipe wall
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Dindependent of radial distance from the pipe axis
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Emaximum right at the wall
Answer
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