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?

Civil Engineering GATE Exam Questions Difficulty: Easy
Choose an option
  • A
    independent of shear stress
  • B
    a universal constant
  • C
    zero at the pipe wall
  • D
    independent of radial distance from the pipe axis
  • E
    maximum 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

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