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How is the Nominal Thickness of the Boundary Layer Defined When the Velocity Reaches the Velocity of the Free Stream?

Published in Fluid Mechanics 3 mins read

The nominal thickness of the boundary layer, often denoted as δ, is conventionally defined as the distance from the wall to the point where the flow velocity reaches 99% of the free stream velocity (U). While theoretically the boundary layer extends to infinity where the fluid reaches the free stream velocity, in practical terms, defining it at 99% offers a more usable and consistent measure.

Here's a breakdown:

  • What is a Boundary Layer? A boundary layer is the thin layer of fluid immediately adjacent to a solid surface where the flow velocity ranges from zero at the wall (due to the no-slip condition) to the free stream velocity as you move away from the wall.

  • Why Not 100%? The velocity asymptotically approaches the free stream velocity. Reaching exactly 100% would theoretically occur at an infinite distance from the wall. Using 99% provides a finite and practical value for the boundary layer thickness.

  • Nominal Thickness (δ): This is the most common definition of boundary layer thickness. Mathematically, it can be expressed as:

    • y = δ when u(y) = 0.99 * U

    Where:

    • y is the distance from the wall
    • δ is the boundary layer thickness
    • u(y) is the flow velocity at distance y from the wall
    • U is the free stream velocity
  • Alternative Definitions: It's important to note that other definitions of boundary layer thickness exist, although they are less common than the 99% definition:

    • *Displacement Thickness (δ):** This represents the distance the solid surface would have to be displaced outward into the free stream to account for the reduction in mass flow rate caused by the boundary layer.

    • Momentum Thickness (θ): This represents the distance the solid surface would have to be displaced outward to account for the reduction in momentum caused by the boundary layer.

  • Importance: Defining the boundary layer thickness is crucial for various engineering applications, including:

    • Estimating drag on aerodynamic surfaces
    • Designing efficient heat exchangers
    • Analyzing flow separation
    • Predicting the performance of pumps and turbines

In summary, while conceptually the boundary layer blends into the free stream, for practical engineering calculations, its thickness is typically defined as the distance from the wall where the fluid velocity reaches 99% of the free stream velocity. This convention provides a tangible and useful measure for analyzing and predicting fluid behavior.

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