Laminar Boundary Layer Thickness Calculator

Laminar Boundary Layer Thickness Calculator

Here’s a comprehensive table summarizing all you need to know about laminar boundary layer thickness:

AspectDetails
DefinitionThe distance from the wall to the point where the velocity is 99% of the free-stream velocity12
Symbolδ (delta)
Blasius Solutionδ ≈ 5.0√(νx/u₀) = 5.0x/√Re_x1
Formula for Flat Plateδ = 5x/√Re_x, where Re_x is the local Reynolds number based on distance from leading edge
Proportionalityδ ∝ x^(1/2), thickness increases with the square root of distance along the plate3
Factors Affecting GrowthIncreases as: fluid particle velocity decreases, surface roughness increases, fluid viscosity increases5
Flow CharacteristicsSmooth and steady flow, characterized by layers sliding past each other
Reynolds Number RangeLaminar boundary layers are found only at small Reynolds numbers6
Velocity ProfileGradual increase in velocity from wall to free stream6
Growth RateSmaller compared to turbulent boundary layers6
Wall Shear StressLower compared to turbulent boundary layers6
Heat TransferLower rates compared to turbulent boundary layers6

Key Points

  1. Calculation: The Blasius solution is commonly used for calculating laminar boundary layer thickness over a flat plate.
  2. Reynolds Number: The local Reynolds number (Re_x) is crucial in determining the boundary layer thickness.
  3. Growth: The thickness increases with distance from the leading edge, but at a decreasing rate (square root relationship).
  4. Transition: At higher Reynolds numbers, the laminar boundary layer may transition to turbulent, changing its characteristics significantly.
  5. Importance: Understanding laminar boundary layer thickness is crucial in fluid dynamics, affecting drag, heat transfer, and other flow properties in various engineering applications.

This table provides a concise overview of the key aspects of laminar boundary layer thickness, including its definition, calculation methods, influencing factors, and characteristics compared to turbulent boundary layers.

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